.

DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
WASHINGTON, D.C.

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

APPROVED BY :

_____________________
GENE HARTMAN, CHAIRMAN
FLIGHT OPERATIONS EVALUATION BOARD

Federal Aviation Administration

Flight Standards Division
LONG BEACH AIRCRAFT EVALUATION GROUP (LGB-AEG)
3960 PARAMOUNT BLVD. SUITE 100
LAKEWOOD, CA 90712-4137
TELEPHONE: (562) 627-5317
FAX:
(562) 627-5281
www.faa.gov/about/office_org/field_offices/aeg/lgb_aeg

Revision: 18
Date: 07/09/2012

FEDERAL AVIATION ADMINISTRATION

Page: I
Revision: 18
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Table of Contents
SYSTEM NO.

21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
38
45
46
49
52
73
74
76
77
78
79
80

SYSTEM

PAGE

Table of Contents
Log of Revisions
Control Page
Highlights of Change
Definition
Preamble

I, II
III, IV, V, VI, VII, VIII
IX, X, XI, XII, XIII, XIV
XV THRU XXVIII
XXIX THRU XXXIV
XXXV, XXXVI

Air Conditioning
Auto Flight
Communications
Electrical Power
Equipment/Furnishings
Fire Protection
Flight Controls
Fuel
Hydraulic Power
Ice and Rain Protection
Indicating/Recording Systems
Landing Gear
Lights
Navigation
Oxygen
Pneumatic
Water/Waste
Central Maintenance Computer
Information Systems
Airborne Auxiliary Power
Doors
Engine Fuel & Control
Ignition
Engine Controls
Engine Indicating
Engine Exhaust
Engine Oil
Starting

21-1
22-1
23-1
24-1
25-1
26-1
27-1
28-1
29-1
30-1
31-1
32-1
33-1
34-1
35-1
36-1
38-1
45-1
46-1
49-1
52-1
73-1
74-1
76-1
77-1
78-1
79-1
80-1

THRU 21-34
THRU 22-4
THRU 23-12
THRU 24-10
THRU 25-14
THRU 26-8
THRU 27-12
THRU 28-16
THRU 29-6
THRU 30-12
THRU 31-4
THRU 32-8
THRU 33-18
THRU 34-10
THRU 35-4
THRU 36-12
THRU 38-2
THRU 45-2
THRU 46-2
THRU 49-6
THRU 52-8
THRU 73-2
THRU 74-2
THRU 76-2
THRU 77-2
THRU 78-2
THRU 79-2
THRU 80-2

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Table of Contents
(contd)

THIS PAGE IS INTENTIONALLY LEFT BLANK

Page: II
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Page: III
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Log of Revisions
REV NO.

DATE

PAGE NUMBERS

0a

05/27/1993

HIGHLIGHTS OF REV., DEFINITIONS,

21-1,21-2,21-3,21-4,22-1,22-2,23-1,23-2,23-3,
24-1,24-2,24-3,25-1,25-2,25-3,25-4,26-1,26-2,
26-3,27-1,28-1,28-2,29-1,29-2,30-1,30-2,30-3,
30-4,30-5,30-6,30-7,31-1,32-1,33-1,33-2,33-3,
33-4,33-5,34-1,34-2,34-3,35-1,35-2,36-1,49-1,
52-1,73-1,74-1,76-1,77-1,78-1,79-1,80-1

07/12/1993

HIGHLIGHTS OF REV.,
30-1,30-2,30-3,30-4,30-5,30-6,30-7

01/10/1994

HIGHLIGHTS OF REV.,
21-1,21-2,21-3,21-4,21-5,22-1,22-2,23-1,23-2,
23-3,24-1,24-2,24-3,24-4,24-5,24-6,25-1,25-2,
25-3,25-4,26-1,26-2,26-3,27-1,27-2,28-1,28-2,
28-3,28-4,29-1,29-2,30-1,30-2,30-3,30-4,30-5,
30-6,30-7,30-8,31-1,31-2,32-1,33-1,33-2,33-3,
33-4,33-5,34-1,34-2,34-3,34-4,35-1,35-2,35-3,
36-1,36-2,49-1,52-1,52-2,73-1,74-1,76-1,77-1,
78-1,79-1,80-1

2a

04/28/1994

HIGHLIGHTS OF REV.,
34-1,34-2,34-4

2b

08/09/1995

HIGHLIGHTS OF REV., DEFINITIONS,

22-2,22-3

2c

04/15/1996

HIGHLIGHTS OF REV., DEFINITIONS,

34-1,34-2,34-3

06/18/1996

HIGHLIGHTS OF REV., DEFINITIONS,

21-1,21-2,21-3,21-4,21-5,21-6,21-7,21-8,22-3,
23-1,23-2,23-3,23-4,24-1,24-2,24-3,24-4,24-5,
24-6,24-7,25-1,25-2,25-3,25-4,25-5,25-6,26-1,
26-2,26-3,26-4,27-2,27-3,28-1,28-2,28-3,28-4,
28-5,28-6,29-1,29-2,30-1,30-2,30-3,30-4,30-5,
30-6,30-7,30-8,30-9,31-2,32-1,32-2,32-3,33-1,
33-2,33-3,33-4,33-5,33-6,34-1,34-2,34-3,34-4,
34-5,36-1,36-2,73-1,74-1

11/27/1996

HIGHLIGHTS OF REV., DEFINITIONS,

24-1,24-3,24-4,24-5,31-1,31-2

INITIALS

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Log of Revisions
(contd)
REV NO.

DATE

PAGE NUMBERS

05/01/2000

HIGHLIGHTS OF REV.,
21-1,21-2,21-3,21-4,21-5,21-6,21-7,21-8,21-9,
21-10,21-11,22-1,22-2,22-3,22-4,23-1,23-2,23-3,
23-4,23-5,24-1,24-2,24-3,24-4,24-5,24-6,24-7,
24-8,24-9,24-10,25-1,25-2,25-3,25-4,25-5,25-6,
26-1,26-2,26-3,26-4,26-5,26-6,27-1,27-2,27-3,
27-4,27-5,27-6,28-1,28-2,28-3,28-4,28-5,28-6,
28-7,28-8,28-9,29-1,29-2,29-3,30-1,30-2,30-3,
30-4,30-5,30-6,30-7,30-8,30-9,30-10,31-1,31-2,
31-3,32-1,32-2,32-3,32-4,33-1,33-2,33-3,33-4,
33-5,33-6,34-1,34-2,34-3,34-4,34-5,34-6,35-1,
35-2,35-3,35-4,36-1,36-2,38-1,45-1,49-1,49-2,
49-3,52-1,52-2,52-3,52-4,73-1,74-1,74-2,76-1,
77-1,78-1,79-1,80-1

05/25/2000

HIGHLIGHTS OF REV., DEFINITIONS,

24-1,24-2,24-3,24-4,24-5,24-6,24-7,24-8,24-9,
24-10,30-1,30-2,30-3,30-4,30-5,30-6,30-7,30-8,
30-10,52-1,52-2,52-3

04/30/2001

HIGHLIGHTS OF REV., DEFINITIONS,

21-1,21-2,21-3,21-4,21-5,21-6,21-7,21-8,21-9,
21-10,21-11,21-12,21-13,21-14,21-15,21-16,
21-17,21-18,21-19,21-20,21-21,21-22,21-23,
21-24,21-25,22-1,22-2,22-3,22-4,23-1,23-2,23-3,
23-4,23-5,23-6,23-7,23-8,24-1,24-2,24-3,24-4,
24-5,24-6,24-7,24-8,24-9,24-10,25-1,25-2,25-3,
25-4,25-5,25-6,25-7,25-8,25-9,25-10,25-11,
25-12,26-1,26-2,26-3,26-4,26-5,26-6 26-7,26-8,
26-9,26-10,27-1,27-2,27-3,27-4,27-5,27-6,28-1,
28-2,28-3,28-4,28-5,28-6,28-7,28-8,28-9,28-10,
28-11,28-12,28-13,28-14,28-15,28-16,28-17,29-1,
29-2,29-3,30-1,30-2,30-3,30-4,30-5,30-6,30-7,
30-8,30-9,30-10,30-11,30-12,31-1,31-2,31-3,
31-4,32-1,32-2,32-3,32-4,33-1,33-2,33-3,33-4,
33-5,33-6,33-7,33-8,34-1,34-2,34-3,34-4,34-5,
34-6,34-7,34-8,34-9,34-10,35-1,35-2,35-3,35-4,
36-1,36-2,36-3,36-4,38-1,38-2,49-1,49-2,49-3,
49-4,49-5,52-1,52-2,52-3,52-4,52-5,73-1,74-1,
74-2,76-1,77-1,78-1,79-1,80-1

08/28/2001

HIGHLIGHTS OF REV., DEFINITIONS,

24-1,24-2,24-3,24-4,24-5,24-6,24-7,24-8,24-9,
30-1,30-2,30-3,30-4,30-5,30-6,30-7,30-8,30-9,
30-10,30-11,30-12,33-1,33-2,33-3,33-4,33-5,
33-6,33-7,33-8,33-9,36-1,36-2,36-3,36-4,49-1,
49-2,49-3,49-4,49-5

01/24/2002

HIGHLIGHTS OF REV., DEFINITIONS,

26-1,26-6,73-1,73-2

INITIALS

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Log of Revisions
(contd)
REV NO.

DATE

PAGE NUMBERS

10

12/04/2002

HIGHLIGHTS OF REV., DEFINITIONS,

21-1,21-2,21-3,21-4,21-5,21-6,21-7,21-8,21-9,
21-10,21-11,21-12,21-13,21-14,21-15,21-16,
21-17,21-18,21-19,21-20,21-21,21-22,21-23,
21-24,21-25,21-26,21-27,21-28,21-29,21-30,
21-31,21-32,21-33,21-34,21-35,21-36,21-37,22-2,
22-3,22-4,23-1,23-2,23-3,23-4,23-5,23-6,23-7,
23-8,24-1,24-2,24-3,24-4,24-5,24-6,24-7,24-8,
24-9,24-10,24-11,24-12,24-13,24-14,24-15,24-16,
25-1,25-2,25-3,25-4,25-5,25-6,25-7,25-8,25-9,
25-10,25-11,25-12,25-13,25-14,26-1,26-2,26-3,
26-4,26-5,26-6,26-7,26-8,26-9,26-10,26-11,
26-12,27-1,27-2,27-3,27-4,27-5,27-6,27-7,27-8,
27-9,27-10,27-11,28-1,28-2,28-3,28-4,28-5,28-6,
28-7,28-8,28-9,28-10,28-11,28-12,28-13,28-14,
28-15,28-16,28-17,28-18,28-19,28-20,28-21,29-1,
29-2,30-1,30-2,30-3,30-4,30-5,30-6,30-7,30-8,
30-9,30-10,30-11,30-12,30-13,31-1,31-2,31-3,
31-4,31-5,32-1,32-2,32-3,32-4,32-5,32-6,32-7,
33-1,33-2,33-3,33-4,33-5,33-6,33-7,33-8,33-9,
34-1,34-2,34-3,34-4,34-5,34-6,34-7,34-8,34-9,
34-10,35-1,35-2,35-3,35-4,36-1,36-2,36-3,36-4,
36-5,36-6,36-7,36-8,36-9,38-1,38-2,49-1,49-2,
49-3,49-4,49-5,49-6,52-1,52-2,52-3,52-4,52-5,
52-6,52-7,73-1,73-2,74-1,74-2,76-1,77-1,78-1,
79-1,80-1

11

09/22/2003

HIGHLIGHTS OF REV., DEFINITIONS,

21-1,21-2,21-3,21-5,21-6,21-8,21-9,21-10,21-11,
21-13,21-14,21-15,21-16,21-17,21-18,21-19,
21-20,21-21,21-22,21-23,21-24,21-25,21-26,
21-27,21-28,21-29,21-30,21-31,21-32,21-33,
21-34,21-35,21-36,21-37,21-38,21-39,21-40,
21-41,21-42,21-43,21-44,21-45,21-46,22-2,22-3,
22-4,25-1,25-10,25-11,25-12,25-13,25-14,27-1,
27-2,27-3,27-4,27-5,27-6,27-7,27-8,27-9,27-10,
27-11,27-12,27-13,27-14,27-15,29-1,29-2,29-3,
31-1,31-2,31-3,31-4,31-5,32-1,32-2,32-3,32-4,
32-5,32-6,32-7,32-8,33-1,33-2,33-3,33-4,33-5,
33-6,33-7,33-8,33-9,33-10,36-1,36-2,36-3,36-4,
36-5,36-6,36-7,36-8,36-9,36-10,36-11,36-12,
36-13,36-14,36-15,36-16,49-1,49-2,49-3,49-4,
49-5,49-6,52-1,52-2,52-3,52-4,52-5,52-6,52-7,
52-8,74-2,78-1

INITIALS

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Log of Revisions
(contd)
REV NO.

DATE

PAGE NUMBERS

12

04/20/2004

HIGHLIGHTS OF REV., DEFINITIONS,

21-1,21-2,21-6,21-7,21-8,21-9,21-10,21-11,
21-12,21-13,21-14,21-15,21-16,21-17,21-18,
21-19,21-20,21-21,21-22,21-23,21-24,21-25,
21-26,21-27,21-28,21-29,21-30,21-31,21-32,
21-33,21-34,21-35,21-36,21-37,21-38,21-39,
21-40,21-41,21-42,21-43,21-44,21-45,21-46,22-2,
22-3,2-4,22-5,23-1,23-2,23-3,3-4,23-5,23-6,
23-7,23-8,23-9,23-10,23-11,23-12,24-1,24-2,
25-3,25-4,25-5,25-6,25-7,25-8,25-9,25-10,25-11,
25-12,25-13,25-14,25-15,25-16,25-17,26-4,27-1,
27-2,27-3,27-4,27-5,27-6,27-7,27-8,27-9,27-10,
27-11,27-12,27-13,27-14,27-15,27-16,27-17,28-3,
28-4,28-5,28-6,28-10,28-11,28-12,28-15,28-18,
28-21,29-1,29-2,29-3,29-4,30-1,30-2,30-3,30-4,
30-5,30-6,30-7,30-8,30-9,30-10,30-11,30-12,
30-13,30-14,30-15,30-16,30-17,31-1,32-2,32-3,
32-4,32-5,32-6,32-7,32-8,33-1,33-2,33-3,33-5,
33-6,33-8,33-9,33-10,34-1,34-4,34-5,34-7,34-9,
35-1,36-1,36-2,36-3,36-4,36-6,36-7,36-11,36-13,
36-14,49-1,49-2,49-3,49-4,49-5,49-6,52-1,52-2,
52-3,74-2,77-1,78-1,80-1

13

09/28/2004

HIGHLIGHTS OF REV., DEFINITIONS,

33-2,33-3,33-4,33-5,33-6,33-7,33-8,33-9,33-10,
33-11,33-12,33-13,33-14,33-15,33-16,34-3,34-4,
34-5,34-7,34-8,34-9,34-10

13a

11/30/2004

HIGHLIGHTS OF REV., DEFINITIONS,

33-10,34-3,34-4,34-5,34-7,34-8,34-10

14

11/23/2005

All

15

09/07/2006

TABLE OF CONTENTS, HIGHLIGHTS OF REV., DEFINITIONS

21-6, 23-1, 23-8, 23-9, 24-1, 24-3, 24-4, 24-13, 25-3, 25-8,
25-9, 25-11, 25-12, 25-13, 25-14, 27-4, 27-8, 28-2, 28-3, 28-4
28-5, 28-6, 28-7, 28-8, 28-9, 28-10, 28-11, 28-12, 28-13,
28-14, 28-15, 28-16, 29-5, 30-12, 31-2, 33-8, 33-16, 34-8,
35-1, 49-1, 49-2, 73-1, 74-1, 79-1

15a

03/07/2007

HIGHLIGHTS OF REV.,
28-9

15b

03/14/2007

HIGHLIGHTS OF REV.,
21-3

INITIALS

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Log of Revisions
(contd)
REV NO.

DATE

PAGE NUMBERS

16

02/25/2008

HIGHLIGHTS OF REV.,
21-5, 21-6, 21-8, 21-27, 23-10, 24-4, 24-5, 24-13, 25-4, 25-6,
25-11, 25-13, 25-14, 27-1, 27-4, 27-6, 27-7,
28-1, 28-2, 28-8, 28-9, 28-11, 28-12, 28-13,
29-1, 29-4, 32-5, 33-3, 33-4, 49-1, 49-2, 49-3,
52-7, 73-2, 74-1, 74-2

16a

06/10/2008

HIGHTLIGHTS OF REV.,
27-4, 29-1, 32-5, 32-6, 34-5, 49-2, 49-3

16b

07/13/2009

TABLE OF CONTENTS, HIGHLIGHTS OF REV.,

23-10, 23-11, 23-12, 24-1, 24-2, 27-3, 27-4, 27-5

17

04/21/2010

HIGHLIGHTS OF REV.,
21-8, 21-9, 21-23, 21-26, 22-3, 23-6, 23-7, 24-1, 24-2, 24-3,
24-4, 24-13, 25-2, 25-3, 25-4, 25-5, 25-6, 25-7, 25-8, 25-13,
25-14, 26-1, 26-2, 26-3, 27-1, 27-4, 27-10, 28-11, 28-15, 29-1,
29-4, 30-5, 30-10, 32-6, 34-1, 34-3, 34-8, 34-9, 35-1, 36-5,
46-1, 49-1, 49-2, 49-3,52-7, 74-2, 78-1, 79-1

18

07/09/2012

All

INITIALS

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Control Page
SYSTEM

PAGE

REV NO

CURRENT DATE

Cover Page
Table of Contents

NO NUMBER
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II
III
IV
V
VI
VII
VIII
IX
X
XI
XII
XIII
XIV
XV
XVI
XVII
XVIII
XIX
XX
XXI
XXII
XXIII
XXIV
XXV
XXVI
XXVII
XXVIII
XXIX
XXX
XXXI
XXXII
XXXIII
XXXIV
XXXV
XXXVI

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18
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9
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07/05/2005
07/05/2005
07/05/2005
07/05/2005
09/07/2006
09/07/2006
06/14/1989
06/14/1989

21-1
21-2
21-3
21-4
21-5
21-6
21-7
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Log of Revisions

Control Page

Highlights of Change

Definitions

Preamble

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FEDERAL AVIATION ADMINISTRATION

Page: X
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

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FEDERAL AVIATION ADMINISTRATION

Page: XI
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

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(contd)
SYSTEM

PAGE

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CURRENT DATE

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FEDERAL AVIATION ADMINISTRATION

Page: XII
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

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(contd)
SYSTEM

PAGE

REV NO

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FEDERAL AVIATION ADMINISTRATION

Page: XIII
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

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(contd)
SYSTEM

PAGE

REV NO

CURRENT DATE

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FEDERAL AVIATION ADMINISTRATION

Page: XIV
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Control Page
(contd)
SYSTEM

PAGE

REV NO

CURRENT DATE

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FEDERAL AVIATION ADMINISTRATION

Page: XV
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
The purpose of this revision is to introduce technical and editorial changes.
Also, the revision 18 introduces the model CL-600-2E25.

SUMMARY OF TECHNICAL AND EDITORIAL CHANGES

Item No.

Type of
change

21-22-01

Technical

The model 600-2E25 is introduced in this item and typo correction.

21-23-01

Technical

The model 600-2E25 is introduced in this item.

21-23-02

Technical

The model 600-2E25 is introduced in this item.

21-24-02

Technical

The model 600-2E25 is introduced in this item.

21-24-03

Technical

The model 600-2E25 is introduced in this item.

21-24-07

Technical

The model 600-2E25 is introduced in this item.

21-31-01

Technical

The model 600-2E25 is introduced in this item.

21-31-02

Technical

The model 600-2E25 is introduced in this item.

21-31-03

Technical

The model 600-2E25 is introduced in this item.

21-32-01

Technical

The model 600-2E25 is introduced in this item.

21-33-01

Technical

The model 600-2E25 is introduced in this item.

21-40-01

Technical

The new ModSums 670T82406 (production) and 670T040476 (in-service) are

introduced for the CL-600-2C10/-2D15/-2D24 models.
The model 600-2E25 is introduced in this item.

Highlights of changes

21-50-01

Technical

The model 600-2E25 is introduced in this item.

21-51-01

Technical

The model 600-2E25 is introduced in this item.

21-51-02

Technical

The model 600-2E25 is introduced in this item.

Order of provisos change c) & d)

21-51-03

Technical

The model 600-2E25 is introduced in this item.

21-51-04

Technical

The model 600-2E25 is introduced in this item.

21-51-05

Technical

The note is modified to address the various failure modes of pressure transducer
such as output drift.

21-52-01

Technical

The model 600-2E25 is introduced in this item.

FEDERAL AVIATION ADMINISTRATION

Page: XVI
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

21-52-02

Technical

The model 600-2E25 is introduced in this item.

21-52-03

Technical

The model 600-2E25 is introduced in this item..

21-55-03

Technical

The model 600-2E25 is introduced in this item.

21-55-04

Technical

The model 600-2E25 is introduced in this item.

21-55-05

Technical

The model 600-2E25 is introduced in this item.

21-61-01

Technical

The model 600-2E25 is introduced in this item.

21-61-04

Technical

The model 600-2E25 is introduced in this item.

22-10-01

Technical

The model 600-2E25 is introduced in this item.

22-10-02

Technical

The note for T/O CONFIG OK is addressed in the relief.

The model 600-2E25 is introduced in this item.

22-11-01

Technical

The model 600-2E25 is introduced in this item.

22-11-02

Technical

The model 600-2E25 is introduced in this item.

22-11-03

Technical

The model 600-2E25 is introduced in this item.

22-12-01

Technical

The model 600-2E25 is introduced in this item.

22-12-02

Technical

The model 600-2E25 is introduced in this item.

22-21-01

Technical

The model 600-2E25 is introduced in this item.

22-22-01

Technical

The model 600-2E25 is introduced in this item.

22-30-01

Technical

New item is introduced for the model 600-2B19 for Auto-throttle System installed as
per the STC# SA8191NM-D

23-11-01

Technical

The model 600-2E25 is introduced in this item.

23-12-01

Technical

The model 600-2E25 is introduced in this item.

23-21-01

Technical

The model 600-2E25 is introduced in this item.

23-22-01

Technical

A note is added to both sets of provisos.

The model 600-2E25 is introduced in this item.

23-22-02

Technical

A note is added to the item.

The model 600-2E25 is introduced in this item.

23-22-03

Technical

The model 600-2E25 is introduced in this item.

Highlights of changes

FEDERAL AVIATION ADMINISTRATION

Page: XVII
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

23-31-01

Technical

The model 600-2E25 is introduced in this item.

23-31-02

Technical

The model 600-2E25 is introduced in this item.

23-32-01

Technical

The model 600-2E25 is introduced in this item.

23-40-01

Technical

The model 600-2E25 is introduced in this item.

23-51-01

Technical

The model 600-2E25 is introduced in this item.

23-51-02

Technical

The model 600-2E25 is introduced in this item.

23-51-03

Technical

The model 600-2E25 is introduced in this item.

23-51-04

Technical

The model 600-2E25 is introduced in this item.

23-51-05

Technical

The model 600-2E25 is introduced in this item.

23-51-06

Technical

The model 600-2E25 is introduced in this item.

23-71-01

Technical

The model 600-2E25 is introduced in this item.

23-81-01

Technical

The model 600-2E25 is introduced in this item.

24-11-01

Editorial

Technical

Provisos e) of sub-item 1) and d) of sub-item 3) is modified to bring in line with the

changed item 24-32-03 description.
The model 600-2E25 is introduced in this item.

24-11-02

Technical

The model 600-2E25 is introduced in this item.

24-22-01

Technical

The model 600-2E25 is introduced in this item.

24-23-01

Technical

The model 600-2E25 is introduced in this item.

24-24-01

Technical

The model 600-2E25 is introduced in this item.

24-31-01

Technical

The model 600-2E25 is introduced in this item.

24-31-02

Technical

The model 600-2E25 is introduced in this item.

24-32-01

Editorial
Technical

Item description is changed to Main Battery and Main Battery Charger System.
Item is reintroduced to combine with Main Battery Charger and remove redundant
limitations.
The wordings of provisos are changed accordingly.
The model 600-2E25 is introduced in this item.

Combined with item 24-32-01.

24-32-02

Technical

Highlights of changes

FEDERAL AVIATION ADMINISTRATION

Page: XVIII
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

24-32-03

Editorial
Technical

Highlights of changes

Item description is changed to APU Battery and APU Battery Charger System.
Item is reintroduced to combine with APU Battery Charger and remove redundant
limitations.
The wordings of provisos are changed accordingly.

24-32-04

Technical

Combined with item 24-32-03.

24-41-01

Technical

The model 600-2E25 is introduced in this item.

24-41-02

Technical

The model 600-2E25 is introduced in this item.

24-41-03

Technical

The model 600-2E25 is introduced in this item.

24-50-03

Technical

The model 600-2E25 is introduced in this item.

24-51-01

Technical

The model 600-2E25 is introduced in this item.

24-61-02

Technical

The model 600-2E25 is introduced in this item.

25-00-01

Technical

The model 600-2E25 is introduced in this item.

25-11-01

Technical

The model 600-2E25 is introduced in this item.

25-12-01

Technical

The model 600-2E25 is introduced in this item.

25-18-01

Technical

The model 600-2E25 is introduced in this item.

25-18-02

Technical

The model 600-2E25 is introduced in this item.

25-21-01

Technical

The model 600-2E25 is introduced in this item.

25-22-01

Technical

The model 600-2E25 is introduced in this item.

25-23-01

Technical

The model 600-2E25 is introduced in this item.

25-32-01

Technical

The model 600-2E25 is introduced in this item.

25-40-01

Technical

The model 600-2E25 is introduced in this item.

25-40-02

Technical

The model 600-2E25 is introduced in this item.

25-42-01

Technical

The model 600-2E25 is introduced in this item.

25-51-01

Technical

The model 600-2E25 is introduced in this item.

25-51-02

Technical

The model 600-2E25 is introduced in this item.

25-51-03

Technical

The model 600-2E25 is introduced in this item.

FEDERAL AVIATION ADMINISTRATION

Page: XIX
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

25-51-04

Technical

The model 600-2E25 is introduced in this item.

25-52-01

Editorial
Technical

For the proviso b), the requirement to empty cargo made specific to affected cargo
compartment.
The model 600-2E25 is introduced in this item.

Highlights of changes

25-61-01

Technical

The model 600-2E25 is introduced in this item.

25-61-02

Technical

The model 600-2E25 is introduced in this item.

25-61-04

Technical

25-62-01

Technical

The model 600-2E25 is introduced in this item.

25-64-01

Technical

The model 600-2E25 is introduced in this item.

25-70-01

Technical

The model 600-2E25 is introduced in this item.

26-00-01

Technical

26-00-02

Technical

The model 600-2E25 is introduced in this item and wording is replaced with
commonly accepted prior to each flight.

26-12-01

Technical

The model 600-2E25 is introduced in this item.

26-14-01

Technical

The model 600-2E25 is introduced in this item.

26-15-01

Editorial
Technical

For FWD Cargo Smoke Detectors, the note is modified address dual smoke
detector failures indicated by the FIRE SYS FAULT status message shown.
The model 600-2E25 is introduced in this item.

The model 600-2E25 is introduced in this item.

The model 600-2E25 is introduced in this item.

26-16-01

Technical

The model 600-2E25 is introduced in this item.

26-22-01

Technical

The model 600-2E25 is introduced in this item.

26-23-01

Technical

The model 600-2E25 is introduced in this item.

26-25-01

Technical

The model 600-2E25 is introduced in this item.

26-25-02

Technical

In the sub-item 1), the wording before each departure is replaced with commonly
accepted prior to each flight.
The model 600-2E25 is introduced in this item.

26-26-01

Technical

The model 600-2E25 is introduced in this item.

27-12-01

Technical

The model 600-2E25 is introduced in this item.

27-15-02

Technical

The model 600-2E25 is introduced in this item.

FEDERAL AVIATION ADMINISTRATION

Page: XX
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

27-21-01

Technical

New item is introduced for the model 600-2E25.

27-24-02

Technical

The model 600-2E25 is introduced in this item.

27-35-01

Technical

The model 600-2E25 is introduced in this item.

27-51-02

Technical

The model 600-2E25 is introduced in this item.

27-51-04

Technical

27-51-05

Technical

New proviso to inspect slat disconnect if 0g or less encountered in last flight is

introduced for models 600-2C10/2D15/2D24.
The model 600-2E25 is introduced in this item.
The model 600-2E25 is introduced in this item.

27-53-01

Technical

New item is introduced for the model 600-2B19 for Flap Actuator Heater System
installed as per the STC# ST03032NY.

27-60-01

Technical

The model 600-2E25 is introduced in this item.

27-65-01

Technical

The model 600-2E25 is introduced in this item.

27-65-02

Technical

The model 600-2E25 is introduced in this item.

28-13-01

Technical

The model 600-2E25 is introduced in this item.

28-13-02

Technical

The model 600-2E25 is introduced in this item.

28-13-03

Technical

The model 600-2E25 is introduced in this item.

28-13-04

Technical

The model 600-2E25 is introduced in this item.

28-13-07

Technical

The model 600-2E25 is introduced in this item.

In the provisos 1a) & 2a), the wording at departure is replaced with commonly
accepted prior to each flight.
The redundant proviso 2b) Fuel imbalance between wing tanks is less than 300 lbs
at dispatch is removed due to AFM Limitation precedence.

Highlights of changes

28-13-08

Technical

The model 600-2E25 is introduced in this item.

In the provisos 1a) & 2a), the wording at departure is replaced with commonly
accepted prior to each flight.
The redundant proviso 2c) Fuel imbalance between wing tanks is less than 300 lbs
at dispatch is removed due to AFM Limitation precedence.

28-13-10

Technical

The model 600-2E25 is introduced in this item.

28-23-01

Technical

The model 600-2E25 is introduced in this item.

28-23-02

Technical

The model 600-2E25 is introduced in this item.

FEDERAL AVIATION ADMINISTRATION

Page: XXI
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

Highlights of changes

28-24-01

Editorial

Provisos e) and f) are combined to bring in line with the changed item 24-32-03
description.

28-24-03

Technical

The model 600-2E25 is introduced in this item.

28-24-04

Technical

The model 600-2E25 is introduced in this item.

28-25-01

Technical

The model 600-2E25 is introduced in this item.

28-25-02

Technical

The model 600-2E25 is introduced in this item.

28-25-03

Technical

The model 600-2E25 is introduced in this item.

28-25-04

Technical

New set of provisos for manual refueling is introduced for the CL-600-2C10/2D15/2D24.
The model 600-2E25 is introduced in this item.

28-25-05

Technical

The model 600-2E25 is introduced in this item.

28-40-01

Technical

The model 600-2E25 is introduced in this item.

28-41-01

Technical

The model 600-2E25 is introduced in this item.

28-41-02

Technical

The model 600-2E25 is introduced in this item.

28-41-03

Technical

The model 600-2E25 is introduced in this item.

28-41-04

Technical

The model 600-2E25 is introduced in this item.

28-41-05

Technical

The model 600-2E25 is introduced in this item.

29-11-01

Technical

The model 600-2E25 is introduced in this item.

The NOTE in the sub-item 1 is modified by adding the term system to bring in line
with the 24-11-01 item description.

29-11-03

Technical

The model 600-2E25 is introduced in this item.

29-11-04

Technical

The model 600-2E25 is introduced in this item.

29-11-05

Technical

The model 600-2E25 is introduced in this item.

29-11-06

Technical

The model 600-2E25 is introduced in this item.

29-11-08

Technical

The model 600-2E25 is introduced in this item.

29-12-01

Technical

In sub-item 3), the new proviso d) for operations to conduct per AFM Supplement is
added for 600-2D15/-2D24 models.
The model 600-2E25 is introduced in this item.
Note changed for standardization

FEDERAL AVIATION ADMINISTRATION

Page: XXII
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

29-32-01
29-32-01

Editorial
Technical

Aircraft designations were revised accordingly

The model 600-2E25 is introduced in this item.
The wording before each departure is replaced with commonly accepted prior to
each flight.

29-34-01

Technical

The model 600-2E25 is introduced in this item.

30-12-01

Technical

The model 600-2E25 is introduced in this item.

30-12-04

Editorial
Technical

In the Sub-item 3), the symbol (O) is added to correct typo error.
The model 600-2E25 is introduced in this item.

30-12-05

Technical

Provisos a) for both sub-items 1) and 2) are changed to secure Wing Cross Bleed
Valve OPEN.
The model 600-2E25 is introduced in this item.

Highlights of changes

30-12-06

Technical

The model 600-2E25 is introduced in this item.

30-22-01

Technical

The model 600-2E25 is introduced in this item.

30-22-03

Technical

The model 600-2E25 is introduced in this item.

30-31-01

Technical

The model 600-2E25 is introduced in this item.

30-31-02

Technical

The model 600-2E25 is introduced in this item.

30-41-01

Technical

The item description is changed from Windshield and Side Window Anti-Ice
Controllers to Windshield and Side Window Anti-Ice Systems to include any other
system parts failures.
Proviso a) for affected anti-ice controller to deactivate is added for both sets of
provisos.
The model 600-2E25 is introduced in this item.

30-42-01

Technical

The model 600-2E25 is introduced in this item.

30-71-02

Technical

The model 600-2E25 is introduced in this item.

30-81-01

Technical

The model 600-2E25 is introduced in this item.

31-14-01

Technical

The model 600-2E25 is introduced in this item.

31-14-02

Technical

The model 600-2E25 is introduced in this item.

31-21-01

Technical

The model 600-2E25 is introduced in this item.

31-31-01

Technical
Editorial

The model 600-2E25 is introduced in this item.

In the second set of provisos, the wording prior takeoff is modified to prior to
takeoff.

FEDERAL AVIATION ADMINISTRATION

Page: XXIII
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

31-31-02

Technical

The model 600-2E25 is introduced in this item.

31-41-01

Technical

The model 600-2E25 is introduced in this item.

31-41-02

Technical

The model 600-2E25 is introduced in this item.

31-41-03

Technical

The model 600-2E25 is introduced in this item.

31-41-04

Technical

The model 600-2E25 is introduced in this item.

31-41-05

Technical

The model 600-2E25 is introduced in this item.

31-61-01

Technical

The model 600-2E25 is introduced in this item.

32-30-01

Technical

In the sub-item 2), the wording of proviso d) is modified to include the Computerized
In-Flight Performance (CIFP).
The model 600-2E25 is introduced in this item.

Highlights of changes

32-31-01

Technical

The model 600-2E25 is introduced in this item.

32-40-01

Technical

The model 600-2E25 is introduced in this item.

32-43-01

Technical

The model 600-2E25 is introduced in this item.

32-44-01

Technical

The model 600-2E25 is introduced in this item.

32-45-01

Technical

The model 600-2E25 is introduced in this item.

32-46-01

Technical

The model 600-2E25 is introduced in this item.

32-46-02

Technical

The model 600-2E25 is introduced in this item.

32-47-01

Technical

The model 600-2E25 is introduced in this item.

32-50-01

Technical

In sub-item 2), the wording of proviso d) is changed,

The model 600-2E25 is introduced in this item.

32-60-01

Technical

New item is introduced for the models 600-2C10/-2D15/-2D24/-2E25.

33-11-01

Technical

The model 600-2E25 is introduced in this item.

33-13-01

Technical

The model 600-2E25 is introduced in this item.

33-21-01

Technical

The model 600-2E25 is introduced in this item.

1b) and 1 c) editorial changes

33-21-02

Technical

The model 600-2E25 is introduced in this item.

33-23-02

Technical

The model 600-2E25 is introduced in this item.

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

33-24-01

Technical

The model 600-2E25 is introduced in this item.

33-31-01

Technical

The model 600-2E25 is introduced in this item.

33-32-01

Technical

The model 600-2E25 is introduced in this item.

33-41-01

Technical

The model 600-2E25 is introduced in this item.

33-41-02

Technical

The model 600-2E25 is introduced in this item.

33-42-01

Technical

The model 600-2E25 is introduced in this item.

33-43-01

Technical

The model 600-2E25 is introduced in this item.

33-44-01

Technical

The model 600-2E25 is introduced in this item.

33-44-02

Technical

The model 600-2E25 is introduced in this item.

33-45-01

Technical

The model 600-2E25 is introduced in this item.

33-46-01

Technical

The model 600-2E25 is introduced in this item.

33-51-01

Technical

The model 600-2E25 is introduced in this item.

1 h) Editorial changes

33-51-02

Technical

The model 600-2E25 is introduced in this item.

34-12-01

Technical

The model 600-2E25 is introduced in this item.

34-14-01

Technical

The model 600-2E25 is introduced in this item.

34-21-01

Technical

The model 600-2E25 is introduced in this item.

34-22-01

Technical

The model 600-2E25 is introduced in this item.

34-25-01

Technical

The model 600-2E25 is introduced in this item.

34-32-01

Technical

The model 600-2E25 is introduced in this item.

34-41-01

Technical

The model 600-2E25 is introduced in this item.

34-41-02

Technical

The model 600-2E25 is introduced in this item.

34-42-01

Technical

The model 600-2E25 is introduced in this item.

34-42-02

Technical

The model 600-2E25 is introduced in this item.

34-42-03

Technical

The model 600-2E25 is introduced in this item.

Highlights of changes

Page: XXIV
Revision: 18
Date: 07/09/2012

FEDERAL AVIATION ADMINISTRATION

Page: XXV
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

34-43-01

Technical

The model 600-2E25 is introduced in this item.

34-44-01

Technical

The model 600-2E25 is introduced in this item.

34-44-02

Technical

The model 600-2E25 is introduced in this item.

34-45-01

Technical

The model 600-2E25 is introduced in this item.

34-50-01

Technical

The model 600-2E25 is introduced in this item.

34-51-01

Technical

The model 600-2E25 is introduced in this item.

34-51-02

Technical

The model 600-2E25 is introduced in this item.

34-52-01

Technical

The model 600-2E25 is introduced in this item.

34-53-01

Technical

The model 600-2E25 is introduced in this item.

34-54-01

Technical

The model 600-2E25 is introduced in this item.

34-61-01

Technical

The model 600-2E25 is introduced in this item.

34-61-02

Technical

The model 600-2E25 is introduced in this item.

35-10-01

Technical

The model 600-2E25 is introduced in this item.

35-10-02

Technical

The model 600-2E25 is introduced in this item.

35-11-02

Technical

The model 600-2E25 is introduced in this item.

35-12-01

Technical

The model 600-2E25 is introduced in this item.

35-12-02

Technical

The model 600-2E25 is introduced in this item.

35-20-01

Technical

New set of provisos introduced for the Passenger Oxygen System.

The model 600-2E25 is introduced in this item.

35-20-02

Technical

The model 600-2E25 is introduced in this item.

35-20-03

Technical

The model 600-2E25 is introduced in this item.

35-31-01

Technical

The model 600-2E25 is introduced in this item.

35-31-02

Technical

The model 600-2E25 is introduced in this item.

36-11-02

Technical

The model 600-2E25 is introduced in this item.

1) and 2) Editorial changes

Highlights of changes

FEDERAL AVIATION ADMINISTRATION

Page: XXVI
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

36-11-03

Technical

The model 600-2E25 is introduced in this item.

1) and 2) Editorial changes

36-11-04

Technical

Typo correction; sensors should be in plural.

The model 600-2E25 is introduced in this item.

36-12-02

Technical

The model 600-2E25 is introduced in this item.

36-21-06

Technical

The model 600-2E25 is introduced in this item.

38-10-01

Technical

The model 600-2E25 is introduced in this item.

38-30-01

Technical

The model 600-2E25 is introduced in this item.

38-30-02

Technical

The model 600-2E25 is introduced in this item.

45-45-01

Technical

The model 600-2E25 is introduced in this item.

45-45-02

Technical

The model 600-2E25 is introduced in this item.

46-20-01

Technical

The model 600-2E25 is introduced in this item.

49-10-01

Technical

The model 600-2E25 is introduced in this item.

49-14-01

Technical

Proviso d) of sub-item 1) is modified to bring in line with the changed item 24-32-03
description.
In sub-item 2), the symbol (O) and Operational procedure is added for the models
600-2C10/-2D15/-2D24 to address provisions for speed limitations, AFM
performance corrections.
The model 600-2E25 is introduced in this item.

Highlights of changes

49-43-01

Technical

The model 600-2E25 is introduced in this item.

49-51-01

Technical

The model 600-2E25 is introduced in this item.

49-51-02

Technical

The model 600-2E25 is introduced in this item.

49-61-01

Technical

The model 600-2E25 is introduced in this item.

49-61-02

Technical

New sub-item 7) Time Totalizing Meter introduced.

The model 600-2E25 is introduced in this item.

52-11-01

Technical

Item is reintroduced as the Door Assist System with the Power Assist Sub-system
and Counterbalance Sub-system.
The NOTE is replaced with the proviso to establish and use alternate procedures for
door operations.
The model 600-2E25 is introduced in this item.

The model 600-2E25 is introduced in this item.

52-11-05

Technical

FEDERAL AVIATION ADMINISTRATION

Page: XXVII
Revision: 18
Date: 07/09/2012

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

52-11-06

Technical

The model 600-2E25 is introduced in this item.

52-21-01

Technical

The model 600-2E25 is introduced in this item.

52-31-01

Technical

The model 600-2E25 is introduced in this item.

52-35-01

Technical

The model 600-2E25 is introduced in this item.

52-51-01

Technical

The model 600-2E25 is introduced in this item.

52-70-01

Technical

The model 600-2E25 is introduced in this item.

52-70-02

Technical

The model 600-2E25 is introduced in this item.

52-70-03

Technical

The model 600-2E25 is introduced in this item.

52-70-04

Technical

The model 600-2E25 is introduced in this item.

52-70-05

Technical

The model 600-2E25 is introduced in this item.

73-21-01

Technical

The model 600-2E25 is introduced in this item.

73-31-04

Technical

The model 600-2E25 is introduced in this item.

74-11-01

Technical

The model 600-2E25 is introduced in this item.

74-30-02

Technical

The model 600-2E25 is introduced in this item.

76-10-01

Technical

The model 600-2E25 is introduced in this item.

76-11-03

Technical

The model 600-2E25 is introduced in this item.

77-31-01

Technical

The model 600-2E25 is introduced in this item.

78-30-01

Technical

The model 600-2E25 is introduced in this item.

79-12-01

Technical

The model 600-2E25 is introduced in this item.

79-21-01

Editorial
Technical

The word approved is change to alternate.

The word in between is change to interval(s).
A Pre and a Post SB configuration for the CRJ 200 are introduced.
To support this MMEL a new DDG procedure is introduced.
The model 600-2E25 is introduced in this item.

79-30-01

Technical

The model 600-2E25 is introduced in this item.

79-30-03

Technical

The model 600-2E25 is introduced in this item.

80-10-01

Technical

The model 600-2E25 is introduced in this item.

Highlights of changes

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Highlights of Change
Item No.

Type of
change

80-10-02

Technical

The model 600-2E25 is introduced in this item.

80-11-01

Technical

The model 600-2E25 is introduced in this item.

Highlights of changes

Please retain these sheets until the next revision has been issued.

Page: XXVIII
Revision: 18
Date: 07/09/2012

FEDERAL AVIATION ADMINISTRATION

Page: XXIX
Revision: 9
Date: 07/05/2005

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Definitions
1. System Definitions.
System numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are
numbered sequentially.
a.

"Item" (Column 1) means the equipment, system, component, or function listed in the "Item" column.

b.

"Number Installed" (Column 2) is the number (quantity) of items normally installed in the aircraft. This
number represents the aircraft configuration considered in developing this MMEL. Should the number
be a variable (e.g., passenger cabin items), a number is not required.

c.

"Number Required for Dispatch" (Column 3) is the minimum number (quantity) of items required for
operation provided the conditions specified in Column 4 are met.

NOTE: Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number
required for dispatch or an alternate means of configuration control approved by the Administrator.
d.

"Remarks or Exceptions" (Column 4) in this column includes a statement either prohibiting or

permitting operation with a specific number of items inoperative, provisos (conditions and limitations)
for such operation, and appropriate notes.

e.

A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text
for the current revision of that page only. The change bar is dropped at the next revision of that page.

2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type certification and approved by
the responsible FAA Aircraft Certification Office. The FAA approved AFM/RFM for the specific aircraft is listed on
the applicable Type Certificate Data Sheet.
3. "As required by FAR" means that the listed item is subject to certain provisions (restrictive or permissive)
expressed in the Federal Aviation Regulations operating rules. The number of items required by the FAR must be
operative. When the listed item is not required by FAR it may be inoperative for time specified by repair category.
4. Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel
of the equipment condition.
NOTE: To the extent practical, placards should be located adjacent to the control or indicator for the item affected;
however, unless otherwise specified, placard wording and location will be determined by the operator.
5. "-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed.
6. "Deleted" in the remarks column after a sequence item indicates that the item was previously listed but is now
required to be operative if installed in the aircraft.
7. "ER" refers to extended range operations of a two-engine airplane (ETOPS) which has a type design approval
for ER operations (ETOPS) and complies with the provisions of Advisory Circular 120-42A.
8. "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal Aviation Act and Federal
Aviation Regulations.
9. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or
local time, as established by the operator, during which at least one flight is initiated for the affected aircraft.

FEDERAL AVIATION ADMINISTRATION

Page: XXX
Revision: 9
Date: 07/05/2005

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Definitions
(contd)
10. "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft or in the
engine(s).
11. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for
operation with the listed item inoperative.
12. "Inoperative" means a system and/or component malfunction to the extent that it does not accomplish
its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or
tolerance(s).
13. "Notes:" in Column 4 provides additional information for crewmember or maintenance consideration. Notes
are used to identify applicable material which is intended to assist with compliance, but do not relieve the operator
of the responsibility for compliance with all applicable requirements. Notes are not a part of the provisos.
14. Inoperative components of an inoperative system:
Inoperative items which are components of a system which is inoperative are usually considered components
directly associated with and having no other function than to support that system.
(Warning/caution systems associated with the inoperative system must be operative unless relief is specifically
authorized per the MMEL).
15. "(M)" symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior
to operation with the listed item inoperative. Normally these procedures are accomplished by maintenance
personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures
requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by
maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who
performs them, is the responsibility of the operator. Appropriate procedures are required to be published as part of
the operator's manual or MEL.
16. "(O)" symbol indicates a requirement for a specific operations procedure which must be accomplished in
planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by the
flight crew; however, other personnel may be qualified and authorized to perform certain functions. The
satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the
operator. Appropriate procedures are required to be published as a part of the operator's manual or MEL.
NOTE: The (M) and (O) symbols are required in the operator's MEL unless otherwise authorized by the
Administrator.
17. "Deactivated" and "Secured" means that the specified component must be put into an acceptable condition for
safe flight. An acceptable method of securing or deactivating will be established by the operator.
18. "Visual Flight Rules" (VFR) is as defined in FAR Part 91. This precludes a pilot from filing an Instrument Flight
Rules (IFR) flight plan.
19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such that would allow a
flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under
Instrument Flight Rules.
20. "Visible Moisture" means an atmospheric environment containing water in any form that can be seen in natural
or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.
21. "Passenger Convenience Items" means those items related to passenger convenience, comfort or
entertainment such as, but not limited to, galley equipment, movie equipment, ash trays, stereo equipment,
overhead reading lamps, etc.

FEDERAL AVIATION ADMINISTRATION

Page: XXXI
Revision: 9
Date: 07/05/2005

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Definitions
(contd)
22. Repair Intervals: All users of an MEL approved under FAR 121, 125, 129 and 135 must effect repairs of
inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times
established by the following letter designators:
Category A. Items in this category shall be repaired within the time interval specified in the remarks column
of the operator's approved MEL.
Category B. Items in this category shall be repaired within three (3) consecutive calendar days (72 hours),
excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were
recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and end at midnight
the 29th.
Category C. Items in this category shall be repaired within ten (10) consecutive calendar days (240 hours),
excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were
recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight
February 5th.
Category D. Items in this category shall be repaired within one hundred and twenty (120) consecutive
calendar days (2880 hours), excluding the day the malfunction was recorded in the aircraft maintenance log and/or
record.
The letter designators are inserted adjacent to Column 2.
23. Electronic fault alerting system - General
New generation aircraft display system fault indications to the flight crew by use of computerized display systems.
Each aircraft manufacturer has incorporated individual design philosophies in determining the data that would be
represented. The following are customized definitions (specific to each manufacturer) to help determine the level
of messages affecting the aircraft's dispatch status. When preparing the MEL document, operators are to select
the proper Definition No. 23 for their aircraft, if appropriate.
a. BOEING (B-757/767, B-747-400, B-777)
Boeing airplanes equipped with Engine Indicating and Crew Alerting Systems (EICAS), provide different priority
levels of system messages (WARNING, CAUTION, ADVISORY, STATUS and MAINTENANCE). Any message
that affects airplane dispatch status will be displayed at a STATUS message level or higher. The absence of an
EICAS STATUS or higher level (WARNING, CAUTION, ADVISORY) indicates that the system/component is
operating within its approved operating limits or tolerances.
System conditions that result only in a maintenance level message, i.e. no correlation with a higher level EICAS
message, do not affect dispatch and do not require action other than as addressed within an operators standard
maintenance program.
b. BOEING (B-717, MD-10, MD-11)
These aircraft are equipped with an alerting function, which is a subsystem within the Electronic Instrument
System (EIS). The alerting function provides various levels of system condition alerts (WARNING, CAUTION,
ADVISORY, MAINTENANCE and STATUS). Alerts that affect aircraft dispatch will include WARNING, CAUTION,
STATUS or MAINTENANCE level. MAINTENANCE alerts are displayed on the status page of the EIS display
panel under the maintenance heading. A MAINTENANCE alert on the EIS indicates the presence of a system
fault, which can be identified by the Central Fault Display System (CFDS) interrogation. The systems are designed
to be fault tolerant, however, for any MAINTENANCE alert, the MEL must be verified for dispatch purposes.

FEDERAL AVIATION ADMINISTRATION

Page: XXXII
Revision: 9
Date: 07/05/2005

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Definitions
(contd)
c. AIRBUS (A-300-600, A-310, A-318/319/320/321, A-330, A-340)
Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide different levels of system
condition messages (WARNING, CAUTION, STATUS, and ADVISORY). A-318/319/320/321, A-330, and A-340
also provide MAINTENANCE status messages.
Any message that affects airplane dispatchability will normally be at the WARNING, CAUTION or STATUS level.
MAINTENANCE messages (A-318/319/320/321, A-330, and A-340 only) are also indicated on ECAM Status Page
below the white Maintenance label.
A MAINTENANCE status (Class II) message on ECAM indicates the presence of a system fault, which can be
identified by CFDS (A-318/319/320/321) or CMS (A-330/A-340) interrogation. The systems are designed to be
fault tolerant. For A-318/319/320/321, MAINTENENACE status (Class II) do not affect dispatch but are listed in
the MMEL. Dispatch is allowed without specific conditions except for: BLUE RSVR MAINTENANCE status: If
applicable, and AIR BLEED MAINTENANCE status: As applicable. For the A-330 and A-340, MAINTENANCE
status messages do not affect dispatch.
d. FOKKER (FK-100)
Fokker aircraft are equipped with Multi Function Display System (MFDS), which provides electronic message
referring to the different priority levels of system information (WARNING (red), CAUTION (amber), AWARENESS
(cyan) AND STATUS (white). Any message that affects aircraft dispatch will be at the WARNING, CAUTION or
AWARENESS level. In these cases, the MEL must be verified for dispatch capability and maintenance may be
required.
System conditions that only require maintenance are not presented on the flight deck. These maintenance
indications/messages may be presented on the Maintenance & Test Panel (MAP) or the Centralized Fault Display
Unit (CFDU) and by dedicated Built In Test Evaluation (BITE) of systems.
e. CANADAIR (CL-65, CL-604)
Canadair aircraft equipped with Engine Indication and Crew Alerting Systems (EICAS) provide four classes of
messages (WARNING, CAUTION, ADVISORY, and STATUS). Any message that affects aircraft dispatch will be
at the WARNING, CAUTION, or STATUS level. System conditions that only require maintenance are not visible to
the flight crew. These maintenance indications/messages are only activated by maintenance personnel using the
Maintenance Diagnostics Computer.
f. EMBRAER (EMB-135/145, ERJ-170 Series)
The EMB-135/145 and ERJ-170/190 are equipped with an Engine Indicating and Crew Alerting System (EICAS)
that provides three different message levels: WARNING, CAUTION, and ADVISORY. The ERJ-170/190 Series
add STATUS messages. Failures that effect dispatchability are presented to the flight crew at one of these levels.
Other failures may be presented only to the maintenance personnel on the Multi Function Display (MFD)
maintenance pages or through the download of the Central Maintenance Computer (CMC). System conditions
that result only in a maintenance level message, i.e. no correlation with a higher level EICAS message, do not
affect dispatch and do not require action other than as addressed within an operator's standard maintenance
program.

FEDERAL AVIATION ADMINISTRATION

Page: XXXIII
Revision: 15
Date: 09/07/2006

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Definitions
(contd)
g. GULFSTREAM (G-IV, G-V, GV-SP, and GIV-X)
Gulfstream airplanes equipped with EICAS provide different priority levels of system messages: WARNING (red),
CAUTION (amber), ADVISORY, STATUS and MAINTENANCE (cyan or blue). Any WARNING or CAUTION
message affects airplane dispatch status and requires that the Airplane Flight Manual or the MEL be used to
determine dispatch capability. STATUS messages which indicate a system failure (e.g., FMS 1 fail) require that
the Airplane Flight Manual or the MEL be used to determine dispatch capability. MAINTENANCE messages do
not affect airplane dispatch status. They indicate the presence of a system fault which can be identified by
Maintenance Data Acquisition Unit (MDAU on the G-V) interrogation, Central Maintenance Computer (CMC on the
GV-SP/GIV-X) interrogation or by reference to the Airplane Flight Manual.
h. De-HAVILLAND (DASH 8 SERIES 400)
Series 400 aircraft are equipped with a Caution/Warning Panel that annunciates all cautions and warnings.
Advisory messages are displayed by the Electronic Indication System (EIS) or individual advisory lights supplied in
the cockpit. "Class 1 failures" are failures that prevent continued operation of a specific Line Replacement Unit or
channel and are annunciated via advisory messages: caution, warning or advisory lights in the flight compartment.
Dispatch with such posted failures are to be in accordance with the MMEL. "Class 2 failures" are failures which do
not prevent continued system function. These faults will not be annunciated to the flight crew and the absence of
the higher level alert (warning, caution, advisory) indicates that the system/component is operating within its
approved operating limits or tolerances. Such faults would be evident during maintenance interrogation performed
during maintenance activities. Class 2 faults do not affect dispatch and will be listed in the Fault Isolation Manual
(FIM). Class 2 faults will be left to the discretion of the operators when these faults are to be rectified.
24. "Administrative control item" means an item listed by the operator in the MEL for tracking and informational
purposes. It may be added to an operator's MEL by approval of the Principal Operations Inspector provided no
relief is granted, or provided conditions and limitations are contained in an approved document (i.e. Structural
Repair Manual, airworthiness directive, etc.). If relief other than that granted by an approved document is sought
for an administrative control item, a request must be submitted to the Administrator. If the request results in review
and approval by the FOEB, the item becomes an MMEL item rather than an administrative control item.
25. "***" symbol in Column 1 indicates an item which is not required by regulation but which may have been
installed on some models of aircraft covered by this MMEL. This item may be included on the operator's MEL after
the approving office has determined that the item has been installed on one or more of the operator's aircraft. The
symbol, however, shall not be carried forward into the operator's MEL. It should be noted that neither this policy
nor the use of this symbol provide authority to install or remove an item from an aircraft.
26. "Excess Items" means those items that have been installed that are redundant to the requirements of the
FARs.
27. "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft
maintenance log and or record. This day is excluded from the calendar days or flight days specified in the MMEL
for the repair of an inoperative item of equipment. This provision is applicable to all MMEL items, i.e., categories
"A, B, C, and D."
28. Considered Inoperative as used in the provisos means that item must be treated for dispatch, taxi
and flight purposes as though it were inoperative. The item shall not be used or operated until the
original deferred item is repaired. Additional actions include: documenting the item on the dispatch
release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL
provisions, including any (M) and (O) procedures and observing the repair category.

FEDERAL AVIATION ADMINISTRATION

Page: XXXIV
Revision: 15
Date: 09/07/2006

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Definitions
(contd)
29. Is not used in the provisos, remarks or exceptions for an MMEL item may specify that another item
relieved in the MMEL is not used. In such cases, crewmembers should not activate, actuate, or
otherwise utilize that component or system under normal operations. It is not necessary for the
operators to accomplish the (M) procedures associated with the item. However, operational
requirements must be complied with, and an additional placard must be affixed, to the extent practical,
adjacent to the control or indicator for the item that is not used to inform crewmembers that a component
or system is not to be used under normal operations.
30. Nonessential equipment and furnishings (NEF) are those items installed on the aircraft as part of the
original certification, supplemental type certificate, or engineering order that have no effect on the safe
operation of flight and would not be required by the applicable certification rules or operational rules.
They are those items that if inoperative, damaged or missing have no effect on the aircrafts ability to be
operated safely under all operational conditions. These nonessential items may be installed in areas
including, but not limited to, the passenger compartment, flight deck area, service areas, cargo areas,
crew rest areas, lavatories, and galley areas. NEF items are not items already identified in the MEL or
CDL of the applicable aircraft. They do not include items that are functionally required to meet the
certification rule or for compliance with any operational rule. Operators NEF process shall not provide
for deferral of items within serviceable limits identified in the manufactures maintenance manual or
operators approved maintenance program such as wear limits, fuel/hydraulic leak rates, oil consumption,
etc. Cosmetic items that are fully serviceable but worn or soiled may be deferred under an operators
NEF process.

FEDERAL AVIATION ADMINISTRATION

Page: XXXV
Revision: 2
Date: 06/14/1989

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Preamble
The following is applicable for authorized certificate holders operating under Federal Aviation
Regulations (FAR) Parts 121, 125, 129, 135: The FAR require that all equipment installed on an aircraft in
compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules
also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment
requirements is not necessary in the interests of safety under all operating conditions. Experience has shown
that with the various levels of redundancy designed into aircraft, operation of every system or installed
component may not be necessary when the remaining operative equipment can provide an acceptable level of
safety.

A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation
industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for
the public. The FAA approved MMEL includes those items of equipment related to airworthiness and operating
regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an
acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items
such as wings, flaps, and rudders. The MMEL is the basis for development of individual operator MELs which
take into consideration the operator's particular aircraft equipment configuration and operational conditions.
Operator MELs, for administrative control, may include items not contained in the MMEL; however, relief for
administrative control items must be approved by the Administrator. An operator's MEL may differ in format from
the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and
authorized, permits operation of the aircraft with inoperative equipment.

Equipment not required by the operation being conducted and equipment in excess of FAR requirements
are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft
Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember
that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL
must be operative.
Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating
procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of
safety is maintained.

The MEL is intended to permit operation with inoperative items of equipment for a period of time until
repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to
maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and
conditions for operation with inoperative equipment. The MEL provides for release of the aircraft for flight with
inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an

FEDERAL AVIATION ADMINISTRATION

Page: XXXVI
Revision: 2
Date: 06/14/1989

MASTER MINIMUM EQUIPMENT LIST

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

Preamble
(contd)
entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR. The item is then either repaired or may
be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation.
MEL conditions and limitations, do not relieve the operator from determining that the aircraft is in condition for
safe operation with items of equipment inoperative.

When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook
entry, or other approved documentation is issued as prescribed by FAR. Such documentation is required prior to
operation with any item of equipment inoperative.

Operators are responsible for exercising the necessary operational control to ensure that an acceptable
level of safety is maintained. When operating with multiple inoperative items, the interrelationships between
those items and the effect on aircraft operation and crew workload will be considered.

Operators are to establish a controlled and sound repair program including the parts, personnel, facilities,
procedures, and schedules to ensure timely repair.

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS,
AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

21-1

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING

23-01

PAGE:

NUMBER INSTALLED
3.

22-01

18

4.

REMARKS OR EXCEPTIONS

Recirculation Fans
1) 600-2C10

(M) May be inoperative provided affected fan(s) is

deactivated.

2) 600-2D15,
600-2D24

(M) May be inoperative provided:

a) Affected fan(s) is deactivated,
b) Inlet Cargo Air SOV is operative or secured
CLOSED,
c) AIR CONDITIONING Cargo switch is selected
to OFF, and
d) Live animals are not carried in cargo
compartment.

3) 600-2E25

(M)(O) May be inoperative provided:

a) Affected fan(s) is deactivated, and
b) Both Air Conditioning Packs are operative.

1) Galley
(600-2B19)

(M) May be inoperative provided:

a) Fan is deactivated, and
b) AFT Exhaust Fan is considered inoperative.

2) Galley
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M) May be inoperative provided fan is deactivated.

3) Galley/Lavatory
***
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

|
|
|

FWD Exhaust Fan

|
1

(M) May be inoperative provided fan is deactivated.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

24-01

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Fan is deactivated, and
b) FWD Exhaust Fan is considered inoperative.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M) May be inoperative provided fan is deactivated.

ARINC Supply Fans

(Avionics Cooling)
(600-2B19)

|
2

(M) One may be inoperative provided:

a) Exhaust Fan (Avionics Cooling) is verified
operative, and
b) One Air Conditioning Pack is verified operative.
NOTE:

24-02

21-2

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
AFT Exhaust Fan
(Lavatory)
1) 600-2B19

07/09/2012

PAGE:

NUMBER INSTALLED
3.

23-02

18

Display Cooling
Fans
1) 600-2B19

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

Utilization of equipment in the avionics bay

without air conditioning and fans should be
avoided during ground operation.

(M) One may be inoperative provided remaining

Display Cooling Fans are verified operative.

(M)(O) One may be inoperative provided display check

valve is verified operative.
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
21-3

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
24-03

18

4.

REMARKS OR EXCEPTIONS

Exhaust Fan
(Avionics Cooling)
1) 600-2B19

(M) May be inoperative provided:

a) Both ARINC Supply Fans are verified
operative,
b) Two Display Cooling Fans are verified
operative, and
c) Both Air Conditioning Packs are verified
operative.
NOTE:

Utilization of equipment in the avionics bay

without air conditioning and fans should be
avoided during ground operation.

2) 600-2C10
with ModSum
670T10548
(Dual Fan),
600-2D15,
600-2D24,
600-2E25

24-04

Display Units
Cooling Air SOV
(600-2B19)

(M) May be inoperative provided SOV is deactivated

and secured OPEN.

24-05

Inboard Exhaust
SOV
(600-2B19)

(M) May be inoperative provided SOV is deactivated

and secured OPEN.

(M) May be inoperative provided one Air Conditioning

Pack is operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-4

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING

4.

REMARKS OR EXCEPTIONS

Overboard Exhaust
SOV
(Avionics Cooling)
(600-2B19)
1) Without

(M)(O) May be inoperative OPEN provided:

a) SOV is secured OPEN,
b) Operations are conducted unpressurized at or
below 10,000 feet MSL, and
c) Extended overwater operations are prohibited.

(M)(O) May be inoperative OPEN provided:

a) SOV is secured OPEN,
b) Operations are conducted unpressurized at or
below 10,000 feet MSL, and
c) Extended overwater operations are prohibited.

(M) May be inoperative CLOSED provided:

a) SOV is secured CLOSED,
b) Inboard exhaust SOV is secured OPEN,
c) Both Air Conditioning Packs are operative,
d) Service door locking mechanism is verified
operative,
e) Service door is CLOSED, LATCHED and
LOCKED, and
f) Passenger Door and Service Door Indication
Systems are operative.

(M) May be inoperative CLOSED.

SB 601R-52-001

(Enlarged vent
flap)

2) With
SB 601R-52-001

(Enlarged vent
flap)

3) With
SB 601R-52-001

(Enlarged vent
flap)

24-07

07/09/2012

PAGE:

NUMBER INSTALLED
3.

24-06

18

Ground Valve
(Avionics Cooling)
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

PAGE:

07/09/2012

21-5

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
31-01

18

4.

REMARKS OR EXCEPTIONS

Automatic Cabin
Pressurization
Controllers
1) 600-2B19

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

One may be inoperative provided Cabin Pressure

Acquisition Module (CPAM) of Cabin Pressure
Monitoring Sub-system is operative.

(O) May be inoperative provided:

a) Cabin Pressure Acquisition Module (CPAM) of
Cabin Pressure Monitoring Sub-system is
operative,
b) Operations are conducted unpressurized at or
below 10,000 feet MSL, and
c) Takeoffs and landings must not be conducted
on runways that may lead to imminent ditching.

(O) One may be inoperative provided:

a) Manual control system is verified operative,
and
b) Cabin Pressure Controller Panel (CPCP)
Pressure Monitoring Function of Cabin
Pressure Monitoring Sub-system is operative.

(O) Both may be inoperative provided:

a) Cabin Pressure Controller Panel (CPCP)
Pressure Monitoring Function of Cabin
Pressure Monitoring Sub-system is operative,
b) Operations are conducted unpressurized at or
below 10,000 feet MSL,
c) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits, and
d) Takeoffs and landings must not be conducted
on runways that may lead to imminent ditching.
NOTE:

Operators MELs must define which items

are approved for inclusion in the Fly Away
Kits, and which materials can be used as
ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

2) 600-2C10,
600-2D15,
600-2D24

3) 600-2E25

21-6

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
EMER DEPRESS
Switch Guard
1) 600-2B19

07/09/2012

PAGE:

NUMBER INSTALLED
3.

31-02

18

4.

REMARKS OR EXCEPTIONS

May be inoperative or missing provided:

a) Both Air Conditioning Packs are operative, and
b) Operations are conducted at or below FL 250.

(O) May be inoperative or missing provided operations

are conducted unpressurized at or below 10,000 feet
MSL.

May be inoperative or missing provided:

a) Both Air Conditioning Packs are operative, and
b) Operations are conducted at or below 15,000 ft
MSL.

(O) May be inoperative or missing provided:

a) Operations are conducted unpressurized at or
below 10,000 feet MSL, and
b) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits.
NOTE:
Operator MELs must define which items are
approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
C

1) MAN ALT
Switch

21-7

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Cabin Pressure
Control Manual
Mode
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

31-03

18

REMARKS OR EXCEPTIONS

May be inoperative provided Outflow Valve is

considered inoperative.

|
1

(O) May be inoperative provided:

a) Pressure control is not selected to MAN,
b) EMER DEPRESS switch is selected ON,
c) Operations are conducted unpressurized at or
below 10,000 feet MSL,
d) Extended overwater operations are prohibited,
and
e) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
21-8

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
32-01

18

4.

REMARKS OR EXCEPTIONS

Outflow Valves
1) 600-2B19

(M)(O) Both may be inoperative provided:

a) Affected valve(s) is secured OPEN,
b) Overboard Exhaust SOV (Avionics Cooling) is
secured OPEN,
c) Operations are conducted unpressurized at or
below 10,000 feet MSL,
d) Extended overwater operations are prohibited,
and
e) Takeoffs and landings must not be conducted
on runways that may lead to imminent ditching.

2) 600-2C10

(M)(O) May be inoperative provided:

a) Affected valve is secured OPEN,
b) Operations are conducted unpressurized at or
below 10,000 ft MSL, and
c) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits.
NOTE:

3) 600-2D15,
600-2D24,
600-2E25

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

(M)(O) May be inoperative provided:

a) Affected valve is secured OPEN,
b) Floatation Valve is checked for integrity,
c) Operations are conducted unpressurized at or
below 10,000 ft MSL, and
d) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

33-01

Cabin Pressure
Monitoring
Sub-system

21-9

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Floatation Valve
(600-2C10
with ModSum
MM670T11933)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

32-02

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided valve is removed.

1) Cabin Pressure
Acquisition
Module (CPAM)
(600-2B19)

(M) May be inoperative provided:

a) Both Automatic Cabin Pressurization
Controllers are operative, and
b) Operations are conducted at or below FL 300.

2) Cabin Pressure
Control Panel
(CPCP)
Pressure
Monitoring
Function
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(O) May be inoperative provided:

a) Both automatic Cabin Pressure Controllers are
operative,
b) Emergency depress system is verified
operative,
c) Operations are conducted at or below FL 300,
and
d) Repairs are made within one flight day.
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
C

21-10

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Galley Heating
System
(600-2B19 with
SB 601R-25-012
or
SB 601R-25-033,
and
SB 601R-25-034),
(600-2C10 without

07/09/2012

PAGE:

NUMBER INSTALLED
3.

40-01

18

REMARKS OR EXCEPTIONS

(M) May be inoperative provided system is

deactivated.

ASB 670BA-21-011,

or
600-2C10 with
ASB 670BA-21-011,

and
SB 670BA-21-013),
(600-2D15),
(600-2D24 without
ASB 670BA-21-011,
or
600-2D24 with
ASB 670BA-21-011,
and
SB 670BA-21-013)
or
(600-2C10,
600-2D15,
600-2D24 with
Modsum
670T82406 or
670T040476),
(600-2E25)

|
|
|
|
|
|
|
|

1) Fan
(600-2B19)

May be inoperative provided:

a) Galley heating fan switch is selected OFF, and
b) Galley heating #1 switch is selected OFF.

2) Heater #1
(600-2B19)

May be inoperative provided galley heating #1 switch

is selected OFF.

3) Heater #2
(600-2B19)

May be inoperative provided galley heating #2 switch

is selected OFF.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

51-01

Air Conditioning
Packs
1) 600-2B19

21-11

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Ground Air
Conditioning
Connector Cover
***

07/09/2012

PAGE:

NUMBER INSTALLED
3.

50-01

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative or missing provided:

a) Connector check valve is verified CLOSED,
b) Operations are conducted at or below FL 250,
and
c) Extended overwater operations are prohibited.

(O) RH pack may be inoperative provided:

a) RH pack is selected OFF,
b) Operations are conducted at or below FL 250,
and
c) Ram Air SOV is verified operative.

(O) LH pack may be inoperative provided:

a) LH pack is selected OFF,
b) Operations are conducted at or below FL 250,
and
c) Ram Air SOV is either verified operative or
deactivated OPEN.

(M)(O) Both may be inoperative provided:

a) Both packs are selected OFF,
b) Operations are conducted unpressurized at or
below 10,000 feet MSL,
c) Ram Air SOV is either verified operative or
deactivated OPEN,
d) EMER DEPRESS switch is selected ON,
e) Overboard Exhaust SOV (Avionics Cooling) is
secured OPEN, and
f) Extended overwater operations are prohibited.
NOTE:

Ground operations should be limited at

ambient temperatures greater than 30
degrees Celsius, to prolong service life of
avionics components.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-12

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Air Conditioning
Packs
(contd)
2) 600-2C10

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

4.

REMARKS OR EXCEPTIONS

(O) RH pack may be inoperative provided:

a) RH pack is selected OFF,
b) Operations are conducted at or below FL 310,
c) Ram Air SOV is either verified operative or
deactivated OPEN, and
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(O) LH pack may be inoperative provided:

a) LH pack is selected OFF,
b) Operations are conducted at or below FL 310,
c) Ram Air SOV is verified operative, and
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(O) Both may be inoperative provided:

a) Both packs are selected OFF,
b) Ram Air SOV is either verified operative or
deactivated OPEN,
c) Operations are conducted unpressurized at or
below 10,000 feet MSL,
d) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits, and
e) Extended overwater operations are prohibited.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-13

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Air Conditioning
Packs
(contd)
3) 600-2D15,
600-2D24

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

4.

REMARKS OR EXCEPTIONS

(O) RH pack may be inoperative provided:

a) RH pack is selected OFF,
b) Operations are conducted at or below FL 250,
c) Ram Air SOV is either verified operative or
deactivated OPEN, and
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(O) LH pack may be inoperative provided:

a) LH pack is selected OFF,
b) Operations are conducted at or below FL 250,
c) Ram Air SOV is verified operative, and
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(O) Both may be inoperative provided:

a) Both packs are selected OFF,
b) Ram Air SOV is either verified operative or
deactivated OPEN,
c) Inlet Cargo Air SOV is operative or secured
CLOSED,
d) AIR CONDITIONING Cargo switch is selected
to OFF,
e) Live animals are not carried in cargo
compartment,
f) Operations are conducted unpressurized at or
below 10,000 feet MSL,
g) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits, and
h) Extended overwater operations are prohibited.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which can be used as ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-14

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Air Conditioning
Packs
(contd)
4) 600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

4.

REMARKS OR EXCEPTIONS

(O) RH pack may be inoperative provided:

a) RH pack is selected OFF,
b) Ram Air SOV is verified operative,
c) Operations are conducted at or below FL 250,
d) Ground operation for Left Air Conditioning
Pack is conducted using APU bleed,
e) Ground operations are not conducted in known
or forecast icing conditions, and
f) Operations are conducted in accordance with
AFM Supplement (Air Conditioning Single
Pack Operation).

|
|
|
|
|
|
|
|
|
|
|

(O) RH pack may be inoperative provided:

a) RH pack is selected OFF,
b) Ram Air SOV is verified operative,
c) Operations are conducted at or below FL 250,
d) Ground operation for Left Air Conditioning
Pack is conducted using engine bleed,
e) Ground operation is limited to temperature
below ISA+10, and
f) Operations are conducted in accordance with
AFM Supplement (Air Conditioning Single
Pack Operation).

|
|
|
|
|
|
|
|
|
|
|

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-15

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Air Conditioning
Packs
(contd)
4) 600-2E25
(contd)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

4.

REMARKS OR EXCEPTIONS

(O) LH pack may be inoperative provided:

a) LH pack is selected OFF,
b) Ram Air SOV is verified operative,
c) Operations are conducted at or below FL 250,
d) Ground operation for Right Air Conditioning
Pack is conducted using APU bleed,
e) Ground operations are not conducted in known
or forecast icing conditions, and
f) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

|
|
|
|
|
|
|
|
|
|
|

(O) LH pack may be inoperative provided:

a) LH pack is selected OFF,
b) Ram Air SOV is verified operative,
c) Operations are conducted at or below FL 250,
d) Ground operation for Right Air Conditioning
Pack is conducted using engine bleed,
e) Ground operation is limited to temperature
below ISA+10, and
f) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

|
|
|
|
|
|
|
|
|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
21-16

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
51-02

18

4.

REMARKS OR EXCEPTIONS

Flow Control Valve

(FCV)
1) 600-2C10

(M)(O) RH FCV may be inoperative provided:

a) Valve is secured CLOSED,
b) RH pack is selected OFF,
c) Opposite Air Conditioning Pack is operative,
d) Operations are conducted at or below FL 310,
e) Ram Air SOV is either verified operative or
deactivated OPEN, and
f) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(M)(O) LH FCV may be inoperative provided:

a) Valve is secured CLOSED,
b) LH pack is selected OFF,
c) Opposite Air Conditioning Pack is operative,
d) Operations are conducted at or below FL 310,
e) Ram Air SOV is verified operative, and
f) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

21-17

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Flow Control Valve
(FCV)
(contd)
1) 600-2C10
(cont'd)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-02

18

REMARKS OR EXCEPTIONS

(M)(O) Both FCVs may be inoperative provided:

a) Both valves are secured CLOSED,
b) Both Air Conditioning Packs are selected OFF,
c) Ram Air SOV is either verified operative or
deactivated OPEN,
d) Operations are conducted unpressurized at or
below 10,000 feet MSL,
e) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits, and
f) Extended overwater operations are prohibited.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-18

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Flow Control Valve
(cont'd)
2) 600-2D15,
600-2D24

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-02

18

4.

REMARKS OR EXCEPTIONS

(M)(O) RH FCV may be inoperative provided:

a) Valve is secured CLOSED,
b) RH pack is selected OFF,
c) Opposite Air Conditioning Pack is operative,
d) Operations are conducted at or below FL 250,
e) Ram Air SOV is either verified operative or
deactivated OPEN, and
f) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(M)(O) LH FCV may be inoperative provided:

a) Valve is secured CLOSED,
b) LH pack is selected OFF,
c) Opposite Air Conditioning Pack is operative,
d) Operations are conducted at or below FL 250,
e) Ram Air SOV is verified operative, and
f) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

21-19

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Flow Control Valve
(FCV)
(cont'd)
2) 600-2D15,
600-2D24
(cont'd)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-02

18

REMARKS OR EXCEPTIONS

(M)(O) Both FCVs may be inoperative provided:

a) Both valves are secured CLOSED,
b) Both Air Conditioning Packs are selected OFF,
c) Ram Air SOV is either verified operative or
deactivated OPEN,
d) Inlet Cargo Air SOV is operative or secured
CLOSED,
e) AIR CONDITIONING Cargo switch is selected
to OFF,
f) Live animals are not carried in cargo
compartment,
g) Operations are conducted unpressurized at or
below 10,000 feet MSL,
h) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits, and
i) Extended overwater operations are prohibited.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-20

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Flow Control Valve
(FCV)
(cont'd)
3) 600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-02

18

4.

REMARKS OR EXCEPTIONS

(M)(O) RH FCV may be inoperative provided:

a) Valve is secured CLOSED,
b) RH pack is selected OFF,
c) Ram Air SOV is verified operative,
d) Operations are conducted at or below FL 250,
e) Ground operation for Left Air Conditioning
Pack is conducted using APU bleed,
f) Ground operations are not conducted in known
or forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplement (Air Conditioning Single
Pack Operation).

|
|
|
|
|
|
|
|
|
|
|
|

(M)(O) RH FCV may be inoperative provided:

a) Valve is secured CLOSED,
b) RH pack is selected OFF,
c) Ram Air SOV is verified operative,
d) Operations are conducted at or below FL 250,
e) Ground operation for Left Air Conditioning
Pack is conducted using engine bleed,
f) Ground operation is limited to temperature
below ISA+10, and
g) Operations are conducted in accordance with
AFM Supplement (Air Conditioning Single
Pack Operation).

|
|
|
|
|
|
|
|
|
|
|
|

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-21

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Flow Control Valve
(FCV)
(cont'd)
3) 600-2E25
(contd)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-02

18

4.

REMARKS OR EXCEPTIONS

(M)(O) LH FCV may be inoperative provided:

a) Valve is secured CLOSED,
b) LH pack is selected OFF,
c) Ram Air SOV is verified operative,
d) Operations are conducted at or below FL 250,
e) Ground operation for Right Air Conditioning
Pack is conducted using APU bleed,
f) Ground operations are not conducted in known
or forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplement (Air Conditioning Single
Pack Operation).

|
|
|
|
|
|
|
|
|
|
|
|

(M)(O) LH FCV may be inoperative provided:

a) Valve is secured CLOSED,
b) LH pack is selected OFF,
c) Ram Air SOV is verified operative,
d) Operations are conducted at or below FL 250,
e) Ground operation for Right Air Conditioning
Pack is conducted using engine bleed,
f) Ground operation is limited to temperature
below ISA+10, and
g) Operations are conducted in accordance with
AFM Supplement (Air Conditioning Single
Pack Operation).

|
|
|
|
|
|
|
|
|
|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

51-04

Air Conditioning
System
1) 600-2C10,
600-2D15,
600-2D24

4.
C

REMARKS OR EXCEPTIONS

(M) System redundancy may be degraded as indicated

by "L PACK FAULT" and/or "R PACK FAULT" status
message(s) provided:
a) Associated pack discharge pressure sensor(s)
is verified operative once each flight day, and
b) Automatic Mode of the associated
Cockpit/Cabin Temperature Control System is
operative and associated MAN mode is not
selected.
NOTE:

2) 600-2E25

21-22

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Air Conditioning
Pack "FAULT/OFF"
Switch Lights
(light function only)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-03

18

Pack Discharge Temperature Readout(s)

and/or Cockpit TEMP Readout(s) and/or
Cabin TEMP Readout(s) and/or Cockpit
SEL Readout(s) and/or Cabin SEL
Readout(s) may be replaced by amber
dashes on the EICAS ECS Synoptic Page.

(M) System redundancy may be degraded as indicated

by L PACK FAULT and/or R PACK FAULT status
message(s) provided:
a) Associated pack discharge pressure sensor(s)
is verified operative once each flight day,
b) Automatic Mode of the associated
Cockpit/Cabin Temperature Control System is
operative and associated MAN mode is not
selected, and
c) Both Air Conditioning Packs are selected ON.

|
|
|
|
|
|
|
|
|
|

NOTE:

|
|
|
|
|
|

Pack Discharge Temperature Readout(s)

and/or Cockpit TEMP Readout(s) and/or
Cabin TEMP Readout(s) and/or Cockpit
SEL Readout(s) and/or Cabin SEL
Readout(s) may be replaced by amber
dashes on the EICAS ECS Synoptic Page.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

52-01

4.

REMARKS OR EXCEPTIONS

System redundancy may be degraded as indicated by

"L PACK FAULT" and/or "R PACK FAULT" status
messages provided the associated Air Conditioning
Pack(s) is considered inoperative.

600-2E25

System redundancy may be degraded as indicated by

L PACK FAULT or R PACK FAULT status message
provided the associated Air Conditioning Pack is
considered inoperative.

|
|
|
|

Pack Supply
Pressure Indication
(600-2B19)

(O)

4)

51-05

21-23

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Air Conditioning
System
(contd)
3) 600-2C10,
600-2D15,
600-2D24

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-04

18

NOTE:

Pack Supply Pressure Readout on the

EICAS ECS Synoptic Page may show
amber dashes and the pack flowline may
show black with white outlines.

Ram Air SOV

1) 600-2B19

(M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN,
b) RH Air Conditioning Pack is operative,
c) LH Air Conditioning Pack is selected OFF, and
d) Operations are conducted at or below FL 250.
NOTE:

Ground operations should be limited at

ambient temperatures greater than 30
degrees Celsius, to prolong service life of
avionics components.
(contd)

|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

21-24

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Ram Air SOV
(contd)
1) 600-2B19
(contd)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

52-01

18

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN,
b) LH Air Conditioning Pack is selected OFF,
c) Operations are conducted unpressurized at or
below 10,000 feet MSL,
d) EMER DEPRESS switch is selected ON,
e) Overboard Exhaust SOV (Avionics Cooling) is
secured OPEN, and
f) Extended overwater operations are prohibited.
NOTE:

Ground operations should be limited at

ambient temperatures greater than 30
degrees Celsius, to prolong service life of
avionics components.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
21-25

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
52-01

18

4.

REMARKS OR EXCEPTIONS

Ram Air SOV

(contd)
2) 600-2C10

(M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN,
b) LH Air Conditioning Pack is operative,
c) RH Air Conditioning Pack is selected OFF,
d) Operations are conducted at or below FL 310,
and
e) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN,
b) RH and LH Air Conditioning Pack are selected
OFF,
c) Operations are conducted unpressurized at or
below 10,000 feet MSL,
d) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits, and
e) EMER DEPRESS switch is selected ON.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-26

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Ram Air SOV
(contd)
3) 600-2D15,
600-2D24

07/09/2012

PAGE:

NUMBER INSTALLED
3.

52-01

18

4.

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN,
b) LH Air Conditioning Pack is operative,
c) RH Air Conditioning Pack is selected OFF,
d) Operations are conducted at or below FL 250,
and
e) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN,
b) RH and LH Air Conditioning Packs are
selected OFF,
c) Inlet Cargo Air SOV is operative or secured
CLOSED,
d) AIR CONDITIONING Cargo switch is selected
to OFF,
e) Live animals are not carried in cargo
compartment,
f) Operations are conducted unpressurized at or
below 10,000 feet MSL,
g) Procedures are established and used to
ensure the cargo compartments remain empty,
or are verified to contain only empty cargo
handling equipment, ballast (ballast may be
loaded in ULDs), and/or Fly Away Kits, and
h) EMER DEPRESS switch is selected ON.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-27

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Ram Air SOV
(contd)
4) 600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

52-01

18

4.

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN,
b) LH Air Conditioning Pack is operative,
c) RH Air Conditioning Pack is selected OFF,
d) Operations are conducted at or below FL 250,
e) Ground operation for Left Air Conditioning
Pack is conducted using APU bleed,
f) Ground operations are not conducted in known
or forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplement (Air Conditioning Single
Pack Operation).

|
|
|
|
|
|
|
|
|
|
|
|

(M)(O) May be inoperative OPEN provided:

a) Ram Air SOV is deactivated OPEN,
b) LH Air Conditioning Pack is operative,
c) RH Air Conditioning Pack is selected OFF,
d) Operations are conducted at or below FL 250,
e) Ground operation for Left Air Conditioning
Pack is conducted using engine bleed,
f) Ground operation is limited to temperature
below ISA+10, and
g) Operations are conducted in accordance with
AFM Supplement (Air Conditioning Single
Pack Operation).

|
|
|
|
|
|
|
|
|
|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

52-03

Ram Air Regulating

Valve (RARV)
1) 600-2D15,
600-2D24,
600-2E25

4.
C

One may be inoperative provided associated Air

Conditioning Pack is considered inoperative.

Cargo Conditioned
Air SOV
***
(600-2B19)

Both may be inoperative provided both Air

Conditioning Packs are considered inoperative.

(M) May be inoperative CLOSED provided:

a) SOV is secured CLOSED,
b) Live animals are not carried in cargo
compartment, and
c) AIR CONDITIONING Cargo switch is selected
to OFF.

May be inoperative OPEN provided:

a) AIR CONDITIONING Cargo switch is selected
to OFF, and
b) Procedures are established and used to
ensure the cargo compartment remains empty,
or is verified to contain only empty cargo
handling equipment, ballast(ballast may be
loaded in ULDs), and/or Fly Away Kits.
NOTE:

55-02

Cargo Fan
***
(600-2B19)

REMARKS OR EXCEPTIONS

2) 600-2D15,
600-2D24
55-01

21-28

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Air Conditioning
Panel RAM AIR
"OPEN" Switch
Light
(light function only)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

52-02

18

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

(M) May be inoperative provided live animals are not

carried in cargo compartment.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
21-29

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
55-03

18

4.

REMARKS OR EXCEPTIONS

Cargo Exhaust SOV

1) 600-2B19
***

(M) May be inoperative CLOSED provided:

a) SOV is secured CLOSED,
b) Live animals are not carried in cargo
compartment, and
c) AIR CONDITIONING Cargo switch is selected
to OFF.

May be inoperative OPEN provided:

a) AIR CONDITIONING Cargo switch is selected
to OFF, and
b) Procedures are established and used to
ensure the cargo compartment remains empty,
or is verified to contain only empty cargo
handling equipment, ballast(ballast may be
loaded in ULDs), and/or Fly Away Kits.
NOTE:

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

(M) May be inoperative CLOSED provided:

a) SOV is secured CLOSED,
b) Live animals are not carried in aft cargo
compartment, and
c) AIR CONDITIONING Cargo switch is selected
to OFF.
May be inoperative OPEN provided:
a) AIR CONDITIONING Cargo switch is selected
to OFF, and
b) Procedures are established and used to
ensure the aft cargo compartment remains
empty, or is verified to contain only empty
cargo handling equipment, ballast(ballast may
be loaded in ULDs), and/or Fly Away Kits.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
21-30

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
55-04

18

4.

REMARKS OR EXCEPTIONS

Cargo Air SOV

1) Recirculated
***
(600-2B19)

(M) May be inoperative CLOSED provided:

a) SOV is secured CLOSED,
b) Live animals are not carried in cargo
compartment, and
c) AIR CONDITIONING Cargo switch is selected
to COND AIR or OFF.

May be inoperative OPEN provided:

a) AIR CONDITIONING Cargo switch is selected
to OFF, and
b) Procedures are established and used to
ensure the cargo compartment remains empty,
or is verified to contain only empty cargo
handling equipment, ballast(ballast may be
loaded in ULDs), and/or Fly Away Kits.
NOTE:

2) Inlet
(600-2C10)

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

(M) May be inoperative CLOSED provided:

a) SOV is secured CLOSED,
b) Live animals are not carried in aft cargo
compartment, and
c) AIR CONDITIONING Cargo switch is selected
to OFF.

May be inoperative OPEN provided:

a) AIR CONDITIONING Cargo switch is selected
to OFF, and
b) Procedures are established and used to
ensure the aft cargo compartment remains
empty, or is verified to contain only empty
cargo handling equipment, ballast (ballast may
be loaded in ULDs), and/or Fly Away Kits.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

21-31

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING
Cargo Air SOV
(contd)
3) Inlet
(600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

55-04

18

REMARKS OR EXCEPTIONS

(M) May be inoperative CLOSED provided:

a) SOV is secured CLOSED,
b) Live animals are not carried in aft cargo
compartment, and
c) AIR CONDITIONING Cargo switch is selected
to OFF

May be inoperative OPEN provided:

a) AIR CONDITIONING Cargo switch is selected
to OFF,
b) Both Recirculation Fans are operative,
c) Both Air Conditioning Packs are operative,
d) Both Flow Control Valves are operative,
e) Both Pressure Regulating SOVs are operative,
f) Both High Pressure Valves are operative, and
g) Procedures are established and used to
ensure the aft cargo compartment remains
empty, or is verified to contain only empty
cargo handling equipment, ballast (ballast may
be loaded in ULDs), and / or Fly Away Kits.
NOTE: Operator MELs must define which items are
approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

55-05

AFT Cargo
Compartment
Temperature
Control System
***
1) 600-2B19

May be inoperative provided:

a) Live animals are not carried in cargo
compartment, and
b) AIR CONDITIONING Cargo switch is selected
to FAN or OFF.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

May be inoperative provided:

a) Live animals are not carried in cargo
compartment, and
b) AIR CONDITIONING Cargo switch is selected
to AIR or OFF.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-32

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING

4.

REMARKS OR EXCEPTIONS

Cabin/Cockpit
Temperature
Control Systems

(O) One may be inoperative provided associated Air

Conditioning Pack is considered inoperative.

1) Automatic Mode

(M) One automatic control may be inoperative

provided:
a) Associated manual control is operative, and
b) Associated Duct Temperature Indication is
operative.

(M) Both automatic controls may be inoperative

provided:
a) Both manual controls are operative, and
b) Both Duct Temperature Indications are
operative.

(M) One manual control may be inoperative provided:

a) Associated automatic control is operative, and
b) Associated Duct Temperature Indication is
operative.

(M) Both manual controls may be inoperative provided:

a) Both automatic controls are operative, and
b) Both Duct Temperature Indications are
operative.

EICAS CABIN
TEMP Indication
(600-2B19)

1) Upper Cabin
Temperature
Sensor
(A/c with SB
601R-21-039)

May be inoperative provided indication is switched to

Lower Cabin Temperature Sensor.

2) Lower Cabin
Temperature
Sensor
(A/c with SB
601R-21-039)

May be inoperative provided indication is switched to

Upper Cabin Temperature Sensor.

2) Manual Mode

61-02

07/09/2012

PAGE:

NUMBER INSTALLED
3.

61-01

18

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
21-33

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

21 AIR CONDITIONING

4.

61-03

Duct Temperature
Indications
(COCKPIT and
CABIN)
(600-2B19)

61-04

Air Conditioning
Panel CKPT/CABIN
Temperature
Control "MAN"
Switch Lights
(light function only)

REMARKS OR EXCEPTIONS

Both may be inoperative provided associated Cockpit

and/or Cabin Automatic Temperature Control Mode is
operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

21 AIR CONDITIONING

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
21-34

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
B

07/09/2012

22-1

NUMBER REQUIRED FOR DISPATCH

22 AUTO FLIGHT
Autopilot System

PAGE:

NUMBER INSTALLED
3.

10-01

18

REMARKS OR EXCEPTIONS

Except where enroute operations or approach

procedures require its use, may be inoperative
provided Altitude Alerting system is operative.
NOTE 1: Autopilot is required for RVSM Operations.
NOTE 2: Relief for inoperative individual flight
guidance operational modes is provided by
MMEL Item 22-10-02 Flight Directors.

10-02

Flight Directors

(O) Except where enroute operations or approach

procedures require its use, may be inoperative
provided Autopilot is considered inoperative.
NOTE 1: Windshear escape guidance function will be
available from the remaining Flight Director.
NOTE 2: The TOGA switches will not be affected by
the inoperative Flight Director.

1) 600-2B19,
600-2C10,
600-2D15,
600-2D24

(O) Except where enroute operations or approach

procedures require its use, may be inoperative
provided:
a) Autopilot is considered inoperative, and
b) TOGA switches are considered inoperative.
NOTE:

2) 600-2E25

Windshear escape guidance will be

inoperative. However, all remaining
windshear functions will be available.

(O) Except where enroute operations or approach

procedures require its use, may be inoperative
provided:
a) Autopilot is considered inoperative,
b) TOGA switches are considered inoperative,
c) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative), and
d) Repairs are made within one flight day.

|
|
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|
|
|
|
|
|

NOTE:

|
|
|

Windshear escape guidance will be

inoperative. However, all remaining
windshear functions will be available.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

22-2

NUMBER REQUIRED FOR DISPATCH

22 AUTO FLIGHT
Flight Directors
(contd)
3) Flight
Director
Modes

07/09/2012

PAGE:

NUMBER INSTALLED
3.

10-02

18

REMARKS OR EXCEPTIONS

Except where enroute operations or approach

procedures require its use, individual flight director
modes may be inoperative provided Altitude Alerting
System is operative.

NOTE 1: Flight director altitude hold mode is required

for RVSM Operations.
NOTE 2: Any flight director mode which operates
normally may be used.
11-01

Autopilot Disconnect
Switches
(Control Wheel)

11-02

Flight Director Sync

Switches

11-03

Take-Off/GoAround (TOGA)
Switches
(on Thrust Levers)
1) 600-2B19,
600-2C10,
600-2D15,
600-2D24

(O) May be inoperative provided the autopilot is not

utilized at less than initial approach altitude.

(O) May be inoperative provided Autopilot System is

considered inoperative.

(O) Both may be inoperative provided alternate

procedures are established and used.
NOTE 1: All normal flight director modes are
available.
NOTE 2: Windshear escape guidance is not affected
by the loss of the TOGA function and
remains operative during the approach and
take-off phases of flight.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

12-01

V-Speed AutoSynchronization
System

12-02

Integrated Avionics
Processor System
(IAPS) Input/Output
Concentrator (IOC)
1) 600-2B19

4.

07/09/2012

22-3

NUMBER REQUIRED FOR DISPATCH

22 AUTO FLIGHT
Take-Off/GoAround (TOGA)
Switches
(contd)
2) 600-2E25

PAGE:

NUMBER INSTALLED
3.

11-03

18

REMARKS OR EXCEPTIONS

(O) Both may be inoperative provided:

a) Alternate procedures are established and
used, and
b) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

|
|
|
|
|
|

NOTE 1: All normal flight director modes are

available.
NOTE 2: Windshear escape guidance is not affected
by the loss of the TOGA function and
remains operative during the approach and
take off phases of flight.

|
|
|
|
|
|

May be inoperative provided V-Speed settings are

made manually by each pilot.

(M) One IAPS IOC may be inoperative provided

remaining IOCs are verified operative before the first
flight of the day.
NOTE 1: "IAPS DEGRADED" status message will be
displayed on EICAS.
NOTE 2: Although take-off configuration warning
system remains operative, "T/O CONFIG
OK" advisory message is inhibited.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M)(O) One IAPS IOC may be inoperative provided

remaining IOCs are verified operative before the first
flight of the day.
|
NOTE:

IAPS DEGRADED status message will be

displayed on EICAS.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18

PAGE:

07/09/2012

22-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

22 AUTO FLIGHT

4.

REMARKS OR EXCEPTIONS

21-01

Mach Trim System

Except where enroute operations require its use, may

be inoperative provided operations are conducted at or
below 250 KIAS / .7 M when autopilot is disengaged.

22-01

Yaw Dampers
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M) May be inoperative provided the affected yaw

damper is verified not engaged.

Auto-throttle System
(600-2B19 with
STC# SA8191NM-D)

(M) May be inoperative provided the Auto-throttle

System is deactivated.

|
|
|

(M) May be inoperative provided:

a) the Auto-throttle System is deactivated, and
b) Routine procedures do not require its use.

|
|
|

(O) May be inoperative provided the

Engage/Disengage Pushbutton Switch is verified
operative.

|
|
|
|
|

May be inoperative provided the Auto-throttle System

is considered inoperative.

|
|

May be inoperative on the non-flying pilot side and

Auto-throttle System is not used on that side.

|
|
|

May be inoperative provided the Auto-throttle System

is considered inoperative.

|
|

30-01

1) Auto-throttle
Disconnect
Pushbutton
Switch (On
Thrust Lever)

2) Auto-throttle
Mode Status
Display (MSD)

3) Auto-throttle
Engage LED
Annunciator

|
|
|
May be inoperative provided the Mode Status Display
(MSD) on the flying pilot side is operative.

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
23-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS

4.

REMARKS OR EXCEPTIONS

11-01

VHF
Communication
Systems

Any in excess of those required by regulations may be

inoperative provided it is not powered by the battery
bus and not required for emergency procedures.

12-01

HF Communication
Systems
***

Any in excess of those required by regulations may be

inoperative.

21-01

Selective Call
System (SELCAL)
***

(O) May be inoperative provided alternate procedures

are established and used.

May be inoperative provided procedures do not require

its use.

(O) May be inoperative provided alternate procedure

are established and used.

May be inoperative provided procedures do not require

its use.

(O) May be inoperative provided alternate procedures

are established and used.

1) Channels

22-01

Aircraft
Communications
Addressing and
Reporting System
(ACARS)
***

NOTE: Any portion of system which operates

normally may be used.
D

May be inoperative provided routine procedures do not

require its use.
NOTE: Any portion of system which operates
normally may be used.

22-02

22-03

AFIS (Automatic
Flight Information
System)
***

Printer
***

(O) May be inoperative provided alternate procedures

are established and used.

May be inoperative provided routine procedures do not

require its use.

|
|

|
|

(O) May be inoperative provided alternate procedures

are established and used.
NOTE: Any portion of system which operates
normally may be used.

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
B

Any station function(s) that operates

normally may be used.

(O) May be inoperative provided:

a) Alternate, normal and emergency procedures,
and/or operating restrictions are established
and used, and
b) Flight Attendant Call Switch Lights and Flight
Attendant Audio Alerting System of
Crewmember Interphone System are
operative.
NOTE:

2) Lavatory
Speakers

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) Alternate, normal and emergency procedures,
and/or operating restrictions are established
and used, and
b) Flight Attendant Call Switch Lights and Flight
Attendant Audio Alerting System of
Crewmember Interphone System are
operative.
NOTE:

1) Passenger
Address PA
Switch Lights
(Interphone
Control Unit and
Flight Attendant
Stations)
(light function
only)

23-2

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
Passenger Address
System

07/09/2012

PAGE:

NUMBER INSTALLED
3.

31-01

18

Any station function(s) that operates

normally may be used.

(O) May be inoperative provided alternate, normal and

emergency procedures, and/or operating restrictions
are established and used.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
B

Prerecorded
Announcement and
Boarding Music
System
***

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) Operative handset is located at an operative
Flight Attendant Seat Assembly, and
b) Alternate communication procedures for
affected flight attendant station are established
and used.
NOTE:

32-01

23-3

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
Flight Attendant
Handsets

07/09/2012

PAGE:

NUMBER INSTALLED
3.

31-02

18

Any handset function(s) that operates

normally may be used.

(O) May be inoperative provided alternate procedures

are established and used.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
23-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
40-01

18

4.

REMARKS OR EXCEPTIONS

Crewmember
Interphone System
1) Interphone
Voice
Communication
Function
a) Flight Deck to
Cabin
(Audio Control
Panel(s) to
Cabin)

(O) May be inoperative provided:

a) Either pilot or co-pilot flight deck to cabin
interphone voice communication function (two
way) operates normally, and
b) Alternate procedures for communication with
cabin are established and used.
NOTE:

b) Cabin to Flight
Deck
(Flight
Attendant
Station(s) to
Flight Deck)

Any station function(s) that operates

normally may be used.

(O) May be inoperative provided:

a) Cabin to flight deck interphone voice
communication function (two way) operates
normally at least at one flight attendant station,
b) Unaffected flight attendant station(s) has an
operative Flight Attendant Seat Assembly,
c) Unaffected flight attendant station(s) has an
operative Flight Attendant Handset, and
d) Alternate communication procedures for the
affected flight attendant station(s) are
established and used.
NOTE:

Any station function(s) that operates

normally may be used.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

d) Flight Deck to
Ground
(Audio Control
Panel(s) to
Ground)

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided alternate

communication procedures for the affected flight
attendant station(s) are established and used.
NOTE:

Any station function(s) that operates

normally may be used.

(O) May be inoperative provided alternate procedures

are established and used.

May be inoperative provided procedures do not require

its use.
NOTE:

e) Ground to
Flight Deck
(Maintenance
Interphone
Station(s) to
Flight Deck)

23-5

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
Crewmember
Interphone System
(contd)
1) Interphone
Voice
Communication
Function
(contd)
c) Cabin to Cabin
(Flight
Attendant
Station(s) to
Flight
Attendant
Station(s))

07/09/2012

PAGE:

NUMBER INSTALLED
3.

40-01

18

Any station function(s) that operates

normally may be used.

(O) May be inoperative provided alternate procedures

are established and used.

May be inoperative provided procedures do not require

its use.
NOTE:

Any station function(s) that operate normally

may be used.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
23-6

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
40-01

18

4.

REMARKS OR EXCEPTIONS

Crewmember
Interphone System
(contd)
2) Interphone
Alerting
Function
a) Flight Deck
Call Switch
Lights
("CALL" and
"EMER")
(600-2B19)

b) Flight Deck
Call Switch
Lights
("CALL" and
"EMER")
(light function
only)
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

c) Flight
Attendant Call
Switch Lights
("ATT", "FLT"
and "EMG")
(light function
only)

May be inoperative provided the flight compartment

audio alerting system (chime) is operative.
NOTE 1: Flight deck audio alerting system (chime)
must always be operative.
NOTE 2: Any Flight Deck Call Switch Light
function(s) that operates normally may be
used.

May be inoperative provided the flight compartment

audio alerting system (chime) is operative.
NOTE 1:
NOTE 2:

Flight deck audio alerting system (chime)

must always be operative.
Any Flight Deck Call Switch Light
function(s) that operates normally may be
used.

|
3

(O) May be inoperative provided:

a) Passenger Address System is operative, and
b) Alternate procedures for contacting flight
attendants are established and used.
NOTE 1: Passenger to Attendant Call System is
considered Non-Essential Equipment and
Furnishings (NEF).
NOTE 2: Any Flight Attendant Call Switch Light
function(s) that operates normally may be
used.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

e) Flight
Attendant
Audio Alerting
System
(Chime)

4.

NOTE 1: Passenger to Attendant Call System is

considered Non-Essential Equipment and
Furnishings (NEF).
NOTE 2: Any Flight Attendant Call Switch Light
function(s) that operates normally may be
used.
B

(O) May be inoperative provided:

a) Passenger Address System is operative, and
b) Alternate procedures for contacting flight
attendants are established and used.

Hand Held
Microphones

Passenger to Attendant Call System is

considered Non-Essential Equipment and
Furnishings (NEF).

(O) May be inoperative provided alternate procedures

are established and used.

May be inoperative provided procedures do not require

its use.
NOTE:

51-01

REMARKS OR EXCEPTIONS

(O) May be inoperative provided Passenger Address

System is operative.

NOTE:

f) Mechanic Call
Switch Lights
(CKPT "CALL"
and MECH
"CALL")

23-7

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
Crewmember
Interphone System
(contd)
2) Interphone
Alerting
Function
(contd)
d) Mid Cabin
Flight
Attendant Call
Lights
(Cockpit,
Lavatory,
Cabin)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

40-01

18

Any Mechanic Call Switch Light function(s)

that operates normally may be used.

One may be inoperative provided associated Boom

Microphone is operative and is used.

Both may be inoperative provided:

a) Boom Microphones are operative, and
b) Spare boom microphone is available in flight
compartment.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

PAGE:

07/09/2012

23-8

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
51-02

18

4.

REMARKS OR EXCEPTIONS

RT/IC Switches
1) Pilot's / Copilot's
RT/IC Switches

Two may be inoperative provided:

a) Switch is not failed in transmit mode,
b) One RT/IC switch operates normally for each
crewmember, and
c) Hand Held Microphone on affected side is
operative.

2) Observer's
RT/IC Switch

May be inoperative provided:

a) Switch is not failed in transmit mode,
b) Seat is acceptable to the FAA inspector for the
performance of official duties,
c) Required minimum safety equipment (safety
belt and oxygen) is available, and
d) Repairs are made within two flight days.
NOTE 1:

NOTE 2:

These provisos are intended to provide for

occupancy of the above seats by a FAA
inspector when the minimum safety
equipment (oxygen and safety belt) is
functional and the inspector determines
the conditions to be acceptable.
The pilot in command will determine if the
minimum safety equipment is functional for
other persons authorized to occupy the
observer seat.

51-03

Flight Compartment
Speakers

Both may be inoperative provided all flight crew

members on flight deck duty utilize headsets.

51-04

Boom Microphones

May be inoperative provided:

a) Flight Data Recorder is operative, and
b) Repairs are made within three flight days.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

51-06

4.
D

Observers Audio
Control Panel

Any in excess of those required for each person on

flight compartment duty may be inoperative.

|
1

May be inoperative provided:

a) Seat is acceptable to the FAA inspector for the
performance of official duties,
b) Required minimum safety equipment (safety
belt and oxygen) is available, and
c) Repairs are made within two flight days.

NOTE 2:

Cockpit Voice
Recorder (CVR)

23-9

REMARKS OR EXCEPTIONS

NOTE 1:

71-01

07/09/2012

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
Headsets
(600-2B19 with both
SBs 601R-23-004
and 601R-34-013),
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

PAGE:

NUMBER INSTALLED
3.

51-05

18

These provisos are intended to provide for

occupancy of the above seats by a FAA
inspector when the minimum safety
equipment (oxygen and safety belt) is
functional and the inspector determines
the conditions to be acceptable.
The pilot in command will determine if the
minimum safety equipment is functional for
other persons authorized to occupy the
observer seat.

May be inoperative provided:

a) Flight Data Recorder is operative, and
b) Repairs are made within three flight days.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

2) (600-2C10,
600-2D15,
600-2D24 with
Modsum
670T122173 or
670T31608),
(600-2E25)

23-10

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
#2 Radio Tuning
Unit (RTU)
1) (600-2B19),
(600-2C10,
600-2D15,
600-2D24
without Modsum
670T122173 or
670T31608)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

81-01

18

4.

REMARKS OR EXCEPTIONS

May be inoperative provided:

a) COM/NAV Standby Tuning Unit is operative
b) Cross-side tuning from RTU#1 is operative,
c) For single HF installation, operations do not
require the use of HF, and
d) RTU #2 is de-selected using its RTU INHIBIT
switch to ensure cross-side tuning by RTU #1.

(O) May be inoperative provided:

a) Backup tuning control on at least one FMS is
operative,
b) Cross-side tuning from RTU#1 is operative,
c) For single HF installation, operations do not
require the use of HF, and
d) RTU #2 is de-selected using its RTU INHIBIT
switch to ensure cross-side tuning by RTU #1.

(O) May be inoperative provided:

a) Cross-side tuning from RTU#1 is operative,
b) Backup tuning control on at least one FMS is
operative,
c) For single HF installation, operations do not
require the use of HF, and
d) RTU #2 is de-selected using its RTU INHIBIT
switch to ensure cross-side tuning by RTU #1.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

82-02

FMS TUNE INHIBIT

Switch

4.

REMARKS OR EXCEPTIONS

May be inoperative provided RTU #2 is operative.

(O) May be inoperative provided:

a) Backup tuning control on at least one FMS is
operative, and
b) FMS TUNE INHIBIT Switch is operative.

May be inoperative in ON (INHIBIT) position provided

both RTUs are operative.
NOTE:

1) (600-2B19),
(600-2C10,
600-2D15,
600-2D24
without Modsum
670T122173 or
670T31608)

23-11

NUMBER REQUIRED FOR DISPATCH

23 COMMUNICATIONS
COM/NAV Standby
Tuning Unit
(600-2B19),
(600-2C10,
600-2D15,
600-2D24 without
Modsum
670T122173 or
670T31608)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

82-01

18

Tuning function of the FMS will be inhibited.

FMS navigation performance may be
degraded if GPS is not available.

May be inoperative in ON (INHIBIT) position provided

COM/NAV Standby Tuning Unit is operative.
NOTE:

Tuning function of the FMS will be inhibited.

FMS navigation performance may be
degraded if GPS is not available.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

23 COMMUNICATIONS

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
23-12

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

24-1

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
Integrated Drive
Generator (IDG)
Systems
1) Constant Speed
Drives (CSD)
(600-2B19)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-01

18

REMARKS OR EXCEPTIONS

(M)(O) One may be inoperative provided:

a) Respective GEN 1/2 switch is selected to
OFF/RESET,
b) Respective IDG is disconnected,
c) APU generator is operated continuously
throughout flight,
d) AFM performance corrections for APU ON are
applied,
e) APU Battery and APU Battery Charger System
is operative,
f) Cross-side Hydraulic Motor Pump (ACMP) is
selected ON,
g) Same side Hydraulic AC Motor Pump (ACMP)
is operative,
h) Repairs are made within 30 flight hours
(cumulative), and
i) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(contd)

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

24-2

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
Integrated Drive
Generator (IDG)
Systems
2) Constant Speed
Drives (CSD)
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-01

18

REMARKS OR EXCEPTIONS

(O) One may be inoperative provided:

a) Respective GEN 1/2 switch is selected to
OFF/RESET,
b) Respective IDG is disconnected,
c) APU generator is operated continuously
throughout flight,
d) AFM performance corrections for APU ON are
applied,
e) Operations are conducted at or below
FL 320, and
f) Repairs are made within 100 flight hours
(cumulative).

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

24-3

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
Integrated Drive
Generator (IDG)
Systems
(contd)
3) Generators,
Generator
Control Units
(GCU)
(600-2B19)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-01

18

REMARKS OR EXCEPTIONS

(M) One may be inoperative provided:

a) Respective GEN 1/2 switch is selected to
OFF/RESET,
b) APU generator is operated continuously
throughout flight,
c) AFM performance corrections for APU ON are
applied,
d) APU Battery and APU Battery Charger System
is operative,
e) Cross-side Hydraulic Motor Pump (ACMP) is
selected ON,
f) Same side Hydraulic AC Motor Pump (ACMP)
is operative, and
g) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(contd)

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

24-4

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
Integrated Drive
Generator (IDG)
Systems
(contd)
4) Generators,
Generator
Control Units
(GCU)
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-01

18

11-02

IDG 1/2
"FAULT/DISC"
Switch Lights
(light function only)

22-01

APU Generator
System

REMARKS OR EXCEPTIONS

One may be inoperative provided:

a) Respective GEN 1/2 switch is selected to
OFF/RESET,
b) APU generator is operated continuously
throughout flight,
c) AFM performance corrections for APU ON are
applied, and
d) Operations are conducted at or below
FL 320.

May be inoperative provided:

a) IDG 1 and IDG 2 are operative, and
b) APU GEN switch is selected to OFF/RESET.
NOTE:

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
24-5

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
23-01

18

4.

REMARKS OR EXCEPTIONS

Air Driven Generator

(ADG) Auto-deploy
System

(M) May be inoperative provided system is

deactivated.

1) ADG
Deployment
Squib
(600-2B19
without
ModSum
TC 601R14177
(wet ADG))

(M) May be inoperative provided Deployment Squib is

deactivated.

24-01

AUTO XFER
"FAIL/OFF"
Switch Lights
(light function only)

31-01

Transformer
Rectifier Units
(TRUs)
1) 600-2B19

(M)(O) One may be inoperative provided ESS TRU 1

and TRU 1 are operative.

(M)

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25
31-02

TRU Cooling Fans

1) 600-2B19

(M) One or two cooling fans may be inoperative

provided:
a) One ESS TRU Cooling Fan is operative, and
b) Forward equipment doors are OPENED for
stationary ground operations at temps. greater
than 30C.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

24-6

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
Main Battery and
Main Battery
Charger System
1) 600-2B19
(AHRS equipped
aircraft or
aircraft with
ModSum
TC601R15209);

PAGE:

NUMBER INSTALLED
3.

32-01

18

4.

REMARKS OR EXCEPTIONS
|
|
|

(M)(O) May be inoperative provided:

a) Main Battery and Main Battery Charger
System is deactivated,
b) APU air intake door is secured fully OPEN,
c) AFM performance corrections for APU ON are
applied,
d) APU is operated continuously during flight or
aircraft speed is limited to 300 KIAS if APU is
OFF,
e) APU Battery and APU Battery Charger System
is operative,
f) APR is selected OFF,
g) Operations are conducted in accordance with
AFM APR OFF performance data, and
h) Repairs are made within one flight day.

|
|

|
|

|
NOTE 1: DG mode heading slew function will be
inoperative.
NOTE 2: Service Lights will be inoperative.
NOTE 3: Maintenance Lights will be inoperative.

(contd)

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

24-7

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
Main Battery and
Main Battery
Charger System
(contd)
1) 600-2B19
(AHRS equipped
aircraft or
aircraft with
ModSum
TC601R15209);
(contd)

PAGE:

NUMBER INSTALLED
3.

32-01

18

4.

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative provided:

a) Main Battery and Main Battery Charger
System is deactivated,
b) APU air intake door is secured fully CLOSED,
c) APU is not used,
d) APU Battery and APU Battery Charger System
is operative,
e) APR is selected OFF,
f) Operations are conducted in accordance with
AFM APR OFF performance data, and
g) Repairs are made within one flight day.

|
|
|

2) 600-2C10,
600-2D15,
600-2D24
600-2E25

32-02

Main Battery
Charger

NOTE 1: DG mode heading slew function will be

inoperative.
NOTE 2: Service Lights will be inoperative.
NOTE 3: Maintenance Lights will be inoperative.

|
|

(M) May be inoperative provided:

a) Main Battery and Main Battery Charger
System is deactivated, and
b) Repairs are made within one flight day

|
|
|
|

Combined with item 24-32-01

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
A

24-8

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
APU Battery and
APU Battery
Charger System
(600-2B19)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

32-03

18

(M) May be inoperative provided:

a) APU Battery and APU Battery Charger System
is deactivated,
b) Main Battery and Main Battery Charger
System is operative,
c) AFM performance corrections for APU ON are
applied when APU is used, and
d) Repairs are made within one flight day.
NOTE:

32-04

APU Battery
Charger
(600-2B19)

33-01

DC TIE 1/2
"CLOSED" Switch
Lights
(light function only)
(600-2B19)

33-02

DC ESS TIE
CLOSED" Switch
Light
(light function only)
(600-2B19)

41-01

External AC Power
"AVAIL/IN USE"
Switch Light
(Overhead Panel)
(light function only)

REMARKS OR EXCEPTIONS
|
|
|
|
|

External DC power will be required to start

the APU and for pressure refueling.

Combined with item 24-32-03

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

41-02

External AC Power
"AVAIL /IN USE"
Switch Light
(Service Panel)
(light function only)

41-03

External AC Power
System

42-01

External DC Power
"AVAIL/IN USE"
Switch Light
(light function only)
(600-2B19)

42-02

External DC Power
System
(600-2B19)

50-01

AC Service Bus
(600-2B19)
Except for aircraft
with
Photoluminescent
Floor Proximity
Emergency Escape
Path Marking
System installed.

24-9

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Lavatory door is locked CLOSED and
placarded "INOPERATIVE - DO NOT ENTER",
b) Lavatory is not used for any purpose,
c) DC ESS TIE Switch Light is selected CLOSED,
d) Sufficient lighting is operative for cabin crew to
perform required duties, and
e) Lighting configuration at dispatch is acceptable
to the flight crew.
NOTE:

07/09/2012

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER

Synoptic Page AC
Service Bus
Indication
(600-2B19)

PAGE:

NUMBER INSTALLED
3.

50-02

18

Cabin Interior Lights will be inoperative.

May be inoperative provided:

a) "DC TIE 1/2" and "DC ESS TIE" are not
displayed on EICAS, and
b) DC SERVICE BUS on EICAS is powered
normally.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

Load Shedding
System
***
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

51-01

AC ESS XFER
"ALTN" Switch Light
(light function only)

51-02

AC Essential Power
Transfer Relay
(K3XD)
(600-2B19)

DC Utility Bus
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

REMARKS OR EXCEPTIONS

May be inoperative provided:

a) IDG1 and IDG2 are operative,
b) ESS TRU 2 is operative, and
c) EICAS AC ESS BUS caution message is not
displayed.
NOTE:

61-02

24-10

NUMBER REQUIRED FOR DISPATCH

24 ELECTRICAL POWER
1

07/09/2012

PAGE:

NUMBER INSTALLED
3.

50-03

18

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

May be inoperative provided cabin right side reading

lights are considered inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

11-01

Pilot seats

07/09/2012

25-1

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
"Fasten Seat Belt
While Seated"
Placards

PAGE:

NUMBER INSTALLED
3.

00-01

18

4.

REMARKS OR EXCEPTIONS

One or more placards may be illegible or missing

provided a legible sign or placard is readable from
each occupied passenger seat.

1) Lumbar
Supports

May be inoperative in lowest position provided seat is

acceptable to affected crew member.

2) Arm rests

(M) May be inoperative or missing provided:

a) Egress is not impaired, and
b) Seat is acceptable to affected crew member.

3) Height
Adjustments

(M) May be inoperative provided:

a) Seat is secured in vertical position acceptable
to affected crew member,
b) Fore/Aft Adjustments are verified operative,
c) Egress is not impaired, and
d) If HGS is installed and required for flight, the
vertical position of the seat must be acceptable
to affected crew member.

4) Fore/Aft
Adjustments

(M) May be inoperative provided:

a) Seat is secured in fore/aft position acceptable
to affected crew member,
b) Height Adjustments are verified operative,
c) Egress is not impaired, and
d) If HGS is installed and required for flight, the
fore/aft adjustment seat must be acceptable to
affected crew member.

5) Recline
Adjustments

(M) May be inoperative provided:

a) Backrest is secured in a position acceptable to
affected crew member, and
b) If HGS is installed and required for flight, the
recline adjustments of the seat must be
acceptable to affected crew member.

6) Thigh Supports

May be inoperative provided seat is acceptable to

affected crew member.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

REMARKS OR EXCEPTIONS

May be inoperative provided:

a) A passenger seat in the passenger cabin is
made available to the FAA inspector for
performance of official duties, and
b) Repairs are made within two flight days.

May be inoperative provided:

a) Required minimum safety equipment (safety
belt and oxygen) is available,
b) Seat is acceptable to the FAA inspector for the
performance of official duties, and
c) Repairs are made within two flight days.
NOTE 1:

NOTE 2:

18-01

Cockpit Sunvisors

25-2

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
Observer's Seat
(including
associated
equipment)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

12-01

18

These provisos are intended to provide for

occupancy of the above seats by a FAA
inspector when the minimum safety
equipment (oxygen and safety belt) is
functional and the inspector determines the
conditions to be acceptable.
The pilot in command will determine if the
minimum safety equipment is functional for
other persons authorized to occupy the
observer seat.

May be inoperative provided affected sunvisor does not

obstruct either pilot's field of view for take-off and
landing.

May be inoperative provided affected sunvisor is

properly secured or removed from aircraft.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-01

Passenger Seats

4.
C

May be inoperative provided affected holder does not

impede associated crew member to perform his duties.

(M) May be inoperative provided affected holder is

removed.

One holder may be inoperative or missing provided the

EFB on the same side is operative.

(O) May be inoperative provided:

a) Seat does not block an Emergency Exit,
b) Seat does not restrict any passenger from
access to the main aircraft aisle, and
c) The affected seat(s) is blocked and placarded
"DO NOT OCCUPY".

NOTE 2:
NOTE 3:

2) Underseat
Baggage
Restraining Bars

25-3

REMARKS OR EXCEPTIONS

NOTE 1:

1) Recline
Mechanism

07/09/2012

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
Cockpit Chart
Holders
(Control Column
and Window)

PAGE:

NUMBER INSTALLED
3.

18-02

18

A seat with an inoperative seat belt is

considered inoperative.
Inoperative seats do not affect the required
number of Flight Attendants.
Affected seat(s) may include the seat(s)
behind and/or adjacent outboard seat(s).

May be inoperative and seat occupied provided

seatback is immovable in full upright position.

(M) May be inoperative and seat occupied provided

seat is secured in the up-right position.

(O) May be inoperative provided:

a) Baggage is not stowed under seat with
inoperative restraining bar,
b) Associated seat is placarded "DO NOT STOW
BAGGAGE UNDER THIS SEAT",
c) Restraining Bar does not restrict any passenger
from access to main aircraft aisle or emergency
exit, and
d) Procedures are established to alert cabin crew
of inoperative restraining bar.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

25-4

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
Passenger Seats
(contd)
3) Armrest
a) Armrest with
Recline
Mechanism

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-01

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative or missing and seat occupied

provided:
a) Armrest does not block an Emergency Exit,
b) Armrest does not restrict any passenger from
access to the main aircraft aisle, and
c) If armrest is missing, seat is secured in the full
upright position.

b) Armrest
without Recline
Mechanism

May be inoperative or missing and seat occupied

provided:
a) Armrest does not block an Emergency Exit,
and
b) Armrest does not restrict any passenger from
access to the main aircraft aisle.

c) Downlock
Mechanism

May be inoperative and seat occupied provided:

a) Armrest does not block an Emergency Exit,
and
b) Armrest does not restrict any passenger from
access to the main aircraft aisle.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

PAGE:

07/09/2012

25-5

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
22-01

18

4.

REMARKS OR EXCEPTIONS

Flight Attendant
Seat Assembly
1) Single Seat
Configuration
(600-2B19)

(M)(O) May be inoperative provided:

a) Affected seat is not occupied,
b) Flight Attendant displaced by inoperative seat
occupies the passenger seat most accessible
to the inoperative seat,
c) Alternate procedures are established and used
as published in crew members manuals,
d) Folding type seat is stowed or is secured in the
retracted position,
e) Passenger seat assigned to flight attendant is
placarded "FOR FLIGHT ATTENDANT ONLY",
and
f) Repairs are made within two flight days.
NOTE 1 : An automatic folding seat that will not stow
automatically is considered inoperative.
NOTE 2 : A seat position with an inoperative or missing
restraint system is considered inoperative.
NOTE 3 : The above provisos apply to flight attendant
seats. Individual operators, when operating
with inoperative seats, will consider the
locations and combinations of seats to
ensure that the proximity to exits and
distribution requirements of the applicable
regulations are met.

(M) May be inoperative provided:

a) Flight Attendant is not required by FAR,
b) Affected seat is not occupied, and
c) Folding type seat stows automatically or is
secured in the retracted position.
NOTE 1 : An automatic folding seat that will not stow
automatically is considered inoperative.
NOTE 2 : A seat position with an inoperative or missing
restraint system is considered inoperative.

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

25-6

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
Flight Attendant
Seat Assembly
(contd)
2) Required Flight
Attendant Seats

07/09/2012

PAGE:

NUMBER INSTALLED
3.

22-01

18

REMARKS OR EXCEPTIONS

(M)(O) One seat position may be inoperative provided:

a) Affected seat position is not occupied,
b) Flight Attendant displaced by inoperative seat
occupies the passenger seat most accessible
to the inoperative seat, so as to most effectively
perform assigned duties,
c) Alternate procedures are established and used
as published in crew members manuals,
d) Folding type seat stows automatically or is
secured in the retracted position, and
e) Passenger seat assigned to flight attendant is
placarded "FOR FLIGHT ATTENDANT ONLY".
NOTE 1 : An automatic folding seat that will not stow
automatically is considered inoperative.
NOTE 2 : A seat position with an inoperative or missing
restraint system is considered inoperative.
NOTE 3 : Individual operators when operating with
inoperative seats, will consider the locations
and combinations of seats to ensure that the
proximity to exits and distribution
requirements of the applicable regulations
are met.

3) Excess Flight
Attendant Seats

(M) May be inoperative provided:

a) Affected seat position or seat assembly is not
occupied, and
b) Folding type seat stows automatically or is
secured in the retracted position.
NOTE 1: Inoperative automatic stow feature of a
folding seat renders the seat inoperative.
NOTE 2: A seat with a missing or inoperative safety
belt (including shoulder harness) or headrest
renders the seat inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
C

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Procedures are established to secure
compartment CLOSED,
b) Any emergency equipment located in affected
compartment is considered inoperative, and
c) Affected compartment is not used for storage of
any item(s) except for those permanently
affixed.
NOTE:

25-7

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
Overhead Storage
Bin(s)/Cabin and
Galley Storage
Compartment/
Closets

07/09/2012

PAGE:

NUMBER INSTALLED
3.

23-01

18

If no partitions are installed, the entire

overhead storage compartment is
considered one bin or compartment.

(M)(O) May be inoperative provided:

a) Affected door(s) is removed,
b) Associated bin or compartment is not used for
storage of any items, except those permanently
affixed,
c) Associated bin or compartment prominently
placarded DO NOT USE.
d) Procedures are established and used to alert
crewmembers and passengers of inoperative
bins, and
e) Passengers are briefed that associated bin or
compartment is not used.
NOTE 1 : If no partitions are installed, the entire
overhead storage compartment is
considered one bin or compartment.
NOTE 2 : Any emergency equipment located in the
associated compartment (permanently
affixed) is available for use.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
25-8

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING

4.

REMARKS OR EXCEPTIONS

32-01

Galley/Cabin Waste
Receptacles Access
Doors/Covers

(M)(O) May be inoperative provided:

a) Container is empty and the access is secured
to prevent waste introduction into the
compartment, and
b) Procedures are established to ensure that
sufficient galley waste receptacles are available
to accommodate all waste that may be
generated on a flight.

40-01

Lavatory Door
Ashtray

May be missing provided it is replaced within three

calendar days.

40-02

Lavatory Waste
Compartment
Access Door / Flap
Assembly

May be inoperative or missing provided associated

Lavatory Fire Extinguishing System is considered
inoperative.

42-01

Lavatory Door
Springs

(O) May be inoperative or missing provided:

a) Door is verified operative (open and close)
without interference,
b) Associated lavatory door is locked before each
takeoff and landing, and
c) Alternate procedures to close door(s) when
required are established and used.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

REMARKS OR EXCEPTIONS

Baggage Retrieval
Modules
***
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

Cargo Compartment
Door Restraint Nets
(Including
associated
equipment)

May be damaged or missing provided affected cargo

compartment is empty.

(M) May be damaged or missing provided cargo in

affected cargo compartment is secured.

(M) One or both may be inoperative provided affected

module(s) is/are secured at the bulkhead position.

NOTE:

51-03

25-9

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING

51-02

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

Associated equipment includes snap latches,

restraint net brackets and floor pan fitting
rings/posts.

Aft Cargo
Compartment
Dividing Nets
(Including
associated
equipment)
***
1) 600-2B19

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

May be damaged or missing provided affected cargo

compartment is empty.

(M)

NOTE:

Associated equipment includes quick release

attachments, anchor plates, net posts,
narrow-hooks and floor pan fitting ring/posts.

NOTE:

Associated equipment includes quick release

attachments, anchor plates and cam
buckles.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
25-10

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
51-04

18

4.

REMARKS OR EXCEPTIONS

Fwd Cargo
Compartment
Dividing Net
(Including
associated
equipment)
1) 600-2C10

0
NOTE:

Associated equipment includes quick release

attachments, snap latches, anchor plates
and floor pan fitting rings/posts.

2) 600-2D15,
600-2D24,
600-2E25

a) Middle Nets
(attached to
door restrain
nets)

b) Divider Net
(located
between fwd
cargo
compartment
doors)

May be damaged or missing provided fwd cargo

compartment is empty.

May be damaged or missing provided baggage load in

the fwd cargo compartment does not exceed 850 lbs.

(M) May be damaged or missing provided cargo in the

fwd cargo compartment is secured.
NOTE:

Associated equipment includes quick release

attachments, snap latches, anchor plates
and floor pan fitting rings/posts.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
C

25-11

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
Cargo Compartment
Liners and Floor
Panels

07/09/2012

PAGE:

NUMBER INSTALLED
3.

52-01

18

REMARKS OR EXCEPTIONS

(M) May be damaged (punctured, torn or deformed)

provided:
a) Affected area is visually inspected for damage,
and
b) Procedures are established and used to
ensure the associated cargo compartment
remains empty, or is verified to contain only
empty cargo handling equipment, ballast
(ballast may be loaded in ULDs), and/or Fly
Away Kits.
NOTE: Operator MELs must define which items are
approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

61-01

Megaphones
***

Any in excess of those required by regulations may be

inoperative or missing provided:
a) Inoperative megaphone is removed from the
passenger cabin, and
b) Required distribution is maintained.

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
25-12

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
61-02

18

4.

REMARKS OR EXCEPTIONS

Emergency Medical
Equipment
1) Automatic
External
Defibrillator
(AED) and/or
Associated
Equipment

2) Emergency
Medical Kit
(EMK) and/or
Associated
Equipment

3) First Aid Kit

(FAK) and/or
Associated
Equipment

(O) May be incomplete, missing or inoperative

provided:
a) AED is resealed in a manner that will identify it
as a unit that can not be mistaken for a fully
serviceable unit, and
b) Repairs or replacements are made within three
flight cycles

Any in excess of those required by regulation may be

incomplete, missing or inoperative.

(O) May be incomplete, missing or inoperative

provided:
a) EMK is resealed in a manner that will identify it
as a unit that can not be mistaken for a fully
serviceable unit, and
b) Repairs or replacements are made within three
flight cycles

Any in excess of those required by regulation may be

incomplete, missing or inoperative.

(O) If more than one is required by regulation, only one

of the required first aid kits may be incomplete, missing
or inoperative provided:
a) FAK is resealed in a manner that will identify it
as a unit that can not be mistaken for a fully
serviceable unit, and
b) Repairs or replacements are made within three
flight cycles

Any in excess of those required by regulation may be

incomplete, missing or inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

64-01

25-13

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING

62-01

07/09/2012

PAGE:

NUMBER INSTALLED
3.

61-04

18

4.

REMARKS OR EXCEPTIONS

Flashlights /
Flashlight Holders
1) Flashlights

(O) May be inoperative or missing provided a flashlight

of equivalent characteristics is readily available.

2) Flashlight
Holders

(M)(O) May be inoperative or missing provided

alternate stowage means are provided.

Emergency Locator
Transmitter (ELT)
***

(M) May be inoperative provided:

a) System is deactivated, and
b) Repairs are made within 90 days.

May be missing provided repairs are made within 90

days.

(M) Any in excess of those required by FAR may be

inoperative provided system is deactivated.

Any in excess of those required by FAR may be

missing.

As required by regulations.

Flotation Equipment
(Crew and
Passenger)
***

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

25-14

NUMBER REQUIRED FOR DISPATCH

25 EQUIPMENT/FURNISHING
Non-Essential
Equipment and
Furnishings (NEF)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

70-01

18

4.
-

REMARKS OR EXCEPTIONS

May be inoperative, damaged or missing provided that

the item(s) is deferred in accordance with operators
NEF deferral program. The NEF program, procedures
and processes are outlined in the operators (insert
name) manual. (M) and (O) procedures, if required,
must be available to the flight crew and included in the
operators appropriate document.
NOTE:

EXTERIOR LAVATORY DOOR ASHTRAYS

ARE NOT CONSIDERED NEF ITEMS.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
26-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

26 FIRE PROTECTION
00-01

18

4.

REMARKS OR EXCEPTIONS

FIDEEX System
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

FIDEEX-Control
Unit ARINC
Communication
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

11-01

Engine Fire
Detection Loops
(600-2B19)

One loop (A or B) may be inoperative, on each engine

provided fire detection switch is selected to the
operative loop.

11-02

Jet Pipe Fire

Detection Loops
(600-2B19)

One loop (A or B) may be inoperative, on each engine

provided fire detection switch is selected to the
operative loop.

12-01

APU Fire Detection

Loops
1) 600-2B19

(M) One loop (A or B) may be inoperative provided

APU fire detection switch is selected to the operative
loop.

Both loops A and B may be inoperative provided APU

is considered inoperative.

Both loops A and B may be inoperative provided APU

is considered inoperative.

00-02

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

System redundancy may be degraded as indicated by

FIRE SYS FAULT status message.

|
1

May be inoperative provided FIRE

DETECTION/FIREX MONITOR pilot initiated test is
performed prior to each flight.

|
C

(M) Both loops A and B may be inoperative provided:

a) APU is used on ground (for engine start only),
b) APU access doors are opened,
c) APU is visually monitored,
d) APU is pneumatically loaded only, and
e) Total APU operating time shall not exceed 5
minutes.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
26-2

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

26 FIRE PROTECTION

4.

REMARKS OR EXCEPTIONS

12-02

APU Fire Warning

Horn
(600-2B19)

May be inoperative provided a qualified operator

remains in the cockpit to monitor the APU Fire
Warning System while the APU is running.

14-01

Main Landing Gear

Bay Overheat
Detection System

(O) May be inoperative provided:

a) MLG BAY OVHT warning message is not
displayed,
b) EICAS Brake Temperature Monitoring
Readouts are operative,
c) Landing gear is left extended for a minimum of
ten minutes after take-off,
d) Take-off performance is in accordance with
AFM Supplement (Flight with Landing Gear
Down), and
e) Take-off is not conducted in icing conditions.

(M)(O) May be inoperative provided:

a) System is deactivated,
b) EICAS Brake Temperature Monitoring
Readouts are operative,
c) Landing gear is left extended for a minimum of
ten minutes after take-off,
d) Take-off performance is in accordance with
AFM Supplement (Flight with Landing Gear
Down), and
e) Take-off is not conducted in icing conditions.

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

26-3

NUMBER REQUIRED FOR DISPATCH

26 FIRE PROTECTION

15-01

07/09/2012

PAGE:

NUMBER INSTALLED
3.

14-01

18

4.

REMARKS OR EXCEPTIONS

Main Landing Gear

Bay Overheat
Detection System
(contd)
A

(M) May be inoperative provided:

a) Operations are conducted in accordance with
AFM Supplement (Flight with Landing Gear
Down),
b) Ground lock pins are installed to ensure that all
three landing gears are locked down
throughout flight,
c) Operations are not conducted in known or
forecast icing conditions,
d) In-flight performance information given in the
Flight Planning and Cruise Control Manual is
used,
e) Extended overwater operations are prohibited,
f) Both headsets are worn, and
g) Repairs are made within one flight day.

(M) Both may be inoperative provided procedures are

established and used to ensure the cargo
compartment remains empty, or is verified to contain
only empty cargo handling equipment, ballast (ballast
may be loaded in ULDs), and / or Fly Away Kits.

Cargo Compartment
Smoke Detectors
1) 600-2B19

NOTE:

a) A/c with
ModSum

Operators MELs must define which items

are approved for inclusion in the Fly Away
Kits, and which materials can be used as
ballast.

(M)(O) One may be inoperative provided remaining

detector is verified operative prior to each flight.

(M)(O) Forward smoke detector may be inoperative

provided aft smoke detector is verified operative prior
to each flight.

TC601R101264

b) A/c without
ModSum
TC601R101264

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

Cargo Compartment
Smoke Detectors
(contd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25
(FWD CARGO)

NOTE:

26-4

NUMBER REQUIRED FOR DISPATCH

26 FIRE PROTECTION

07/09/2012

PAGE:

NUMBER INSTALLED
3.

15-01

18

3) 600-2C10,
600-2D15,
600-2D24,
600-2E25
(AFT CARGO)

REMARKS OR EXCEPTIONS

Relief for single or dual Fwd Cargo

Compartment Smoke Detector failure is
covered by item 26-00-01 with the FIRE
SYS FAULT status message shown.

|
|
|

(M) All may be inoperative provided procedures are

established and used to ensure the fwd cargo
compartment remains empty, or is verified to contain
only empty cargo handling equipment, ballast (ballast
may be loaded in ULDs), and / or Fly Away Kits.
NOTE:

Operators MELs must define which items

are approved for inclusion in the Fly Away
Kits, and which materials can be used as
ballast.

NOTE:

Relief for single Aft Cargo Compartment

Smoke Detector failure is covered by item
26-00-01.
|

(M) All may be inoperative provided procedures are

established and used to ensure the aft cargo
compartment remains empty, or is verified to contain
only empty cargo handling equipment, ballast (ballast
may be loaded in ULDs), and / or Fly Away Kits.
NOTE:

Operators MELs must define which items

are approved for inclusion in the Fly Away
Kits, and which materials can be used as
ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
C

REMARKS OR EXCEPTIONS

(M)(O) For each lavatory, the lavatory smoke detection

system may be inoperative provided:
a) Lavatory waste receptacle is empty,
b) Associated lavatory door is locked CLOSED
and placarded, "INOPERATIVE - DO NOT
ENTER", and
c) Lavatory is used only by crewmembers.
NOTE 1:
NOTE 2:

22-01

23-01

26-5

NUMBER REQUIRED FOR DISPATCH

26 FIRE PROTECTION
Lavatory Smoke
Detection System

07/09/2012

PAGE:

NUMBER INSTALLED
3.

16-01

18

These provisos are not intended to prohibit

lavatory inspections by crewmembers.
Lavatory smoke detection system is not
required for all-cargo operations.

APU Fire
Extinguishing
System
1) 600-2B19

May be inoperative provided APU is considered

inoperative.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

May be inoperative provided APU is considered

inoperative.

Portable Fire
Extinguishers

|
C

(M) May be inoperative provided:

a) APU is used on ground (for engine start only),
b) APU access doors are opened,
c) APU is visually monitored,
d) APU Fire Detection System is operative,
e) APU is pneumatically loaded only, and
f) Total APU operating time shall not exceed 5
minutes.

Any in excess of those required by regulations may be

inoperative or missing provided:
a) Inoperative fire extinguisher is tagged
inoperative, removed from the installed
location, and placed out of sight so it cannot be
mistaken for a functional unit, and
b) Required distribution is maintained.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
26-6

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

26 FIRE PROTECTION
25-01

18

4.

REMARKS OR EXCEPTIONS

Cargo Compartment
Fire Extinguishing
System
1) 600-2B19

May be inoperative provided procedures are

established and used to ensure the cargo
compartment remains empty, or is verified to contain
only empty cargo handling equipment, ballast (ballast
may be loaded in ULDs), and/or Fly Away Kits.
NOTE:

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

May be inoperative provided procedures are

established and used to ensure the cargo
compartments remain empty, or are verified to contain
only empty cargo handling equipment, ballast (ballast
may be loaded in ULDs), and/or Fly Away Kits.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
26-7

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

26 FIRE PROTECTION
25-02

18

4.

REMARKS OR EXCEPTIONS

Cargo Compartment
Fire Extinguisher
Squibs
1) 600-2B19

One may be inoperative provided:

a) Cargo fire test is performed prior to each flight,
and
b) Repairs are made within three flight days.
All may be inoperative provided procedures are
established and used to ensure the cargo
compartment remains empty, or is verified to contain
only empty cargo handling equipment, ballast (ballast
may be loaded in ULDs), and/or Fly Away Kits.
NOTE:

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25
a) Fwd Squibs

Aft Squibs

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

|
C

All may be inoperative provided procedures are

established and used to ensure the fwd cargo
compartment remains empty, or is verified to contain
only empty cargo handling equipment, ballast (ballast
may be loaded in ULDs), and/or Fly Away Kits.
NOTE:

b)

|
|

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

All may be inoperative provided procedures are

established and used to ensure the aft cargo
compartment remains empty, or is verified to contain
only empty cargo handling equipment, ballast (ballast
may be loaded in ULDs), and/or Fly Away Kits.
NOTE:

Operator MELs must define which items are

approved for inclusion in the Fly Away Kits,
and which materials can be used as ballast.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

26-8

NUMBER REQUIRED FOR DISPATCH

26 FIRE PROTECTION
Lavatory Fire
Extinguishing
System

07/09/2012

PAGE:

NUMBER INSTALLED
3.

26-01

18

4.

REMARKS OR EXCEPTIONS

For each lavatory, the lavatory fire extinguishing

system may be inoperative provided Lavatory Smoke
Detection System operates normally.

(M)(O) For each lavatory, the lavatory fire

extinguishing system may be inoperative provided:
a) Lavatory waste receptacle is empty,
b) Associated lavatory door is locked CLOSED
and placarded, "INOPERATIVE - DO NOT
ENTER", and
c) Lavatory is used only by crewmembers.
NOTE 1:
NOTE 2:

These provisos are not intended to prohibit

lavatory inspections by crewmembers.
A lavatory fire extinguishing system is not
required for all-cargo operations.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

27-1

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
Aileron Trim System
1) 600-2B19

07/09/2012

PAGE:

NUMBER INSTALLED
3.

12-01

18

4.

REMARKS OR EXCEPTIONS

May be inoperative provided:

a) Autopilot is operative,
b) Both Power Crossflow SOVs are operative, and
c) Aileron trim system is centered.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

May be inoperative provided:

a) Autopilot is operative,
b) XFlow Pump is operative, and
c) Aileron trim system is centered.

15-02

Aileron Flutter
Dampers

(O) One per surface may indicate low reservoir fluid

provided:
a) Each individual PCU is verified operative prior
to further flight, and
b) Repairs are made within one flight day.

21-01

Rudder System
(600-2E25)

System redundancy may be degraded as indicated by

RUDDER FAULT status message provided:
a) Only one of the following indications or
messages is also present:
i) Rad Alt red flag with SPLR/STAB FAULT
status message, or
ii) IAPS DEGRADED status message, or
iii) FLAP HALFSPEED status message, or
iv) SLAT HALFSPEED status message, or
v) L FADEC FAULT 1(2) status message, or
vi) R FADEC FAULT 1(2) status message, or
vii) A/SKID INBD caution message, or
viii) A/SKID OUTBD caution message.
b) Repairs are made within three flight days

24-01

EICAS Rudder
Control Surface
Position Indication
(600-2B19)

(M) May be inoperative provided visual inspection of

affected control surface for correct operation is made
before each departure.

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|
|
|
|
|
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|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

27-2

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
Rudder Pedal
Adjustment Systems

07/09/2012

PAGE:

NUMBER INSTALLED
3.

24-02

18

4.

REMARKS OR EXCEPTIONS

(O) One may be inoperative provided:

a) Pedals are in position acceptable to affected
crewmember,
b) EICAS Rudder Control Surface Position
Indication is operative, and
c) Rudder and brake pedals are checked for full
and unrestricted movement at both pilot
stations.

(M)(O) One may be inoperative provided:

a) Pedals are adjusted to position acceptable to
affected crewmember,
b) EICAS Rudder Control Surface Position
Indication is operative, and
c) Rudder and brake pedals are checked for full
and unrestricted movement at both pilot
stations.

34-01

EICAS Elevator
Control Surface
Position Indication
(600-2B19)

(M) May be inoperative provided visual inspection of

affected control surface for correct operation is made
before each departure.

35-01

Stall Warning Switch

Lights
(light function only)

(O) May be inoperative provided shaker and pusher

are checked operative prior to each flight.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
27-3

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
51-01

18

4.

REMARKS OR EXCEPTIONS

Flap Electronic
Control Unit (FECU)
Channels
(600-2B19)
1) A/c without
ModSum

TC601R15447
or

TC601R15318
a)

Flap Power
Drive Unit
(PDU) Motors

2) A/c with
ModSum

May be inoperative provided Flap Power Drive Unit

Motor on the opposite side is operative.
NOTE:

Flap will operate at half-speed.

NOTE:

Flap will operate at half-speed.

TC601R15447
or

TC601R15318

May be inoperative provided:

a) Flap Power Drive Unit Motor on the opposite
side is operative, and
b) Skew Detection System is considered
inoperative.
NOTE:

(M) May be inoperative provided:

a) Flap Power Drive Unit Motor on the opposite
side is operative, and
b) Skew Detection System is verified operative
before each flight.
NOTE:

a)

Flap Power
Drive Unit
(PDU) Motors

Flap will operate at half-speed.

May be inoperative provided Skew Detection System is

considered inoperative.
NOTE:

Flap will operate at half-speed.

Flap will operate at half-speed.

(M) May be inoperative provided Skew Detection

system is verified operative before each flight.
NOTE:

Flap will operate at half-speed.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
27-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
51-02

18

4.

REMARKS OR EXCEPTIONS

Slat / Flap System

1) (600-2C10,
600-2D15,
600-2D24
without ModSum
670T31732)
a) Flap
Subsystem

(M) System redundancy may be degraded as indicated

by FLAPS HALFSPEED status message provided:
a) Both Flap PDU brakes are verified operative,
b) SLATS HALFSPEED status message is not
displayed, and
c) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
NOTE:

b) Slat
Subsystem

Flaps will operate at half-speed.

(M) System redundancy may be degraded as indicated

by SLATS HALFSPEED status message provided:
a) Both Slat PDU brakes are verified operative,
b) FLAPS HALFSPEED status message is not
displayed, and
c) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
NOTE:

Slats will operate at half-speed.

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

REMARKS OR EXCEPTIONS

|
C

System redundancy may be degraded as indicated by

FLAPS HALFSPEED status message provided:
a) SLATS HALFSPEED and/or FLAP FAULT
status messages are not displayed, and
b) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
NOTE:

b) Slat
Subsystem

27-5

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
Slat / Flap System
(contd)
2) (600-2C10,
600-2D15,
600-2D24
with ModSum
670T31732),
(600-2E25)
a) Flap
Subsystem

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-02

18

Flaps will operate at half-speed.

System redundancy may be degraded as indicated by

SLATS HALFSPEED status message provided:
a) FLAPS HALFSPEED and/or FLAP FAULT
status messages are not displayed, and
b) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
NOTE:

Slats will operate at half-speed.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative provided:

a) System is deactivated, and
b) Flaps are visually checked before each flight.

(M)(O) May be inoperative provided:

a) System reset is performed before each flight,
b) Flaps are visually checked before each flight,
and
c) EICAS FLAPS FAIL caution message is not
displayed.
NOTE 1:

NOTE 2:

51-04

Slat Disconnect
Detection System
(600-2C10,
600-2D15,
600-2D24
600-2E25)

27-6

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
Skew Detection
System
(600-2B19 with
ModSum
TC601R15447 or
TC601R15318)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-03

18

On the aircraft without ModSum

TC601R15059 or TC601R15010 (Non
EICAS 2000) flap will operate at half
speed.
On the aircraft with ModSum
TC601R15059 or TC601R15010 (EICAS
2000) flap may operate at half-speed if the
Skew Detection System DC power supply
fails.

(M)(O) May be inoperative as indicated by SLAT

FAULT status message provided:
a) Slats are inspected once each flight day to
ensure no mechanical disconnect is present,
b) Slats are inspected before next flight to ensure
no mechanical disconnect is present if 0g or
less is encountered as result of pilot
maneuvering in last flight, and
c) Repairs are made within three flight days.

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U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

27-7

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
Flap System
1) (600-2C10,
600-2D15,
600-2D24
without ModSum
670T31732)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-05

18

4.

REMARKS OR EXCEPTIONS

(M) System redundancy may be degraded as indicated

by FLAP FAULT status message provided nondispatchable Flap System failures are verified not
present before each flight.

2) (600-2C10,
600-2D15,
600-2D24
with ModSum
670T31732),
(600-2E25)

System redundancy may be degraded as indicated by

FLAP FAULT status message.

53-01

Flap Actuator
Heater System
(600-2B19 with
STC# 03032NY)

(M) May be inoperative provided:

a) Flap Actuator Heater System is deactivated,
and
b) Flap Actuator Heater System is visually
inspected for damage.

54-01

Flap Position
Potentiometers
(600-2B19)
1) A/c without
ModSum
TC601R15447
or
TC601R15318

(M) May be inoperative provided affected

potentiometer is deactivated.

(M) May be inoperative provided:

a) Affected potentiometer is deactivated,
b) R/H Flap Position Potentiometer is operative,
and
c) Skew Detection System is considered
inoperative.

(M) May be inoperative provided:

a) Affected potentiometer is deactivated, and
b) L/H Flap Position Potentiometer is operative.

2) A/c with
ModSum
TC601R15447
or
TC601R15318
a) L/H

b) R/H

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U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

62-01

Spoiler Electronic
Control Unit (SECU)
Channels
(600-2B19)
1) Flight Spoiler
Channels

27-8

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
EICAS Ground
Spoilers Control
Surface Position
Indications

07/09/2012

PAGE:

NUMBER INSTALLED
3.

60-01

18

4.

REMARKS OR EXCEPTIONS

(M) Any may be inoperative provided:

a) GLD auto and manual modes are visually
verified operative prior to each flight, and
b) GLD spoilers are verified stowed before each
flight.

(M)(O) One may be inoperative provided:

a) INBD and OUTBD Ground Spoilers are verified
operative prior to each flight,
b) Flight spoilers are verified operative prior to
each flight,
c) EICAS "R/L FLIGHT SPOILER", "FLIGHT
SPOILERS" and "FLIGHT SPOILER DEPLOY"
caution messages are not displayed, and
d) T/O Configuration Warning System is verified
operative before first flight each day.

2) Ground Spoiler
Channels

(O) One per SECU may be inoperative provided:

a) INBD and OUTBD Ground Spoilers are verified
operative prior to each flight, and
b) T/O Configuration Warning System is verified
operative before first flight each day.

3) Spoileron
Channels

(M)(O) One may be inoperative provided:

a) Spoilerons are verified operative prior to each
flight,
b) Remaining SECU Spoileron Channel is
controlled by SECU p/n 49-164-05, 49-164-07
or 49-164-21,
c) EICAS "SPOILERONS ROLL", "SPOILERONS"
and
"R/L SPOILERON" caution messages are not
displayed,
d) T/O Configuration Warning System is verified
operative before first flight each day, and
e) Repairs are made within three flight days.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
27-9

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS

4.

REMARKS OR EXCEPTIONS

62-02

Flight Spoiler PCUs

(600-2B19)

(M)(O) One Flight Spoiler PCU per surface may be

inoperative provided:
a) INBD and OUTBD Ground Spoilers are
confirmed operative prior to each flight,
b) Flight spoilers are confirmed operative prior to
each flight,
c) Both SECU Channels are operative,
d) EICAS "R/L FLIGHT SPOILER", "FLIGHT
SPOILERS" and "FLIGHT SPOILER DEPLOY"
caution messages are not displayed, and
e) T/O Configuration Warning System is verified
operative before first flight each day.

62-03

Spoileron PCUs
(600-2B19)

(M)(O) One per surface may be inoperative provided:

a) Spoilerons are verified operative prior to each
flight,
b) One spoileron PCU per surface is operative
and controlled by SECU p/n 49-164-05, 49164-07 or 49-164-21,
c) EICAS "SPOILERONS ROLL", "SPOILERONS"
and "R/L SPOILERON" caution messages are
not displayed,
d) T/O Configuration Warning System is verified
operative before first flight each day, and
e) Repairs are made within three flight days.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
27-10

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
65-01

18

4.

REMARKS OR EXCEPTIONS

Ground Spoilers
(Inboard or
Outboard Pair)
1) 600-2B19

(M)(O) One pair of Ground Spoilers Inboard (IB) or

Outboard (OB) may be inoperative in the RETRACTED
position provided:
a) All remaining spoiler surfaces are operative in
GLD auto and manual modes,
b) Affected Inboard or Outboard Ground Spoiler
pair is secured stowed,
c) Both surfaces of the inoperative pair are
verified fully retracted prior to each flight, and
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M)(O) One pair of Ground Spoilers Inboard (IB) or

Outboard (OB) may be inoperative in the RETRACTED
position provided:
a) All MFS and the remaining ground spoiler pair
is operative in GLD AUTO and manual ARM
modes,
b) Affected Inboard or Outboard Ground Spoiler
pair is secured stowed,
c) Both surfaces of the inoperative pair are
verified fully retracted prior to each flight,
d) Both Thrust Reversers are operative,
e) No other GS, MFS status message are
displayed, and
f) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

2) SSCU 2
Channels
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
3) Spoiler /
Stabilizer
Subsystem
a) A/c without
ModSum
670T31194
(600-2C10,
600-2D15,
600-2D24)

b) A/c with
ModSum
670T31194
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

4.

27-11

NUMBER REQUIRED FOR DISPATCH

27 FLIGHT CONTROLS
Spoiler and
Stabilizer Control
System (SSCS)
1) SSCU 1
Channels
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

65-02

18

REMARKS OR EXCEPTIONS

May be inoperative as indicated by "SSCU 1 FAULT"

status message provided both SSCU 2 Channels are
operative.

|
C

May be inoperative as indicated by "SSCU 2 FAULT"

status message provided both SSCU 1 Channels are
operative.

(M) System redundancy may be degraded as indicated

by SPLR/STAB FAULT status message provided:
a) Both SSCU 1 Channels and both SSCU 2
Channels are operative, and
b) Not-dispatchable spoiler / stabilizer subsystem
failures are verified not present once each flight
day.

System redundancy may be degraded as indicated by

SPLR/STAB FAULT status message provided both
SSCU 1 Channels and both SSCU 2 Channels are
operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

27 FLIGHT CONTROLS

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
27-12

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

PAGE:

07/09/2012

28-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

28 FUEL
13-01

18

4.

REMARKS OR EXCEPTIONS

APU Fuel Feed

SOV
1) 600-2B19

(M) May be inoperative CLOSED provided APU is

considered inoperative.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M) May be inoperative CLOSED provided APU is

considered inoperative.
|

13-02

XFLOW AUTO
OVERRIDE "MAN"
Switch Light
(light function only)

13-03

XFLOW L/R
"ON/FAIL" Switch
Lights
(light function only)

(M)(O) May be inoperative OPEN provided:

a) APU is used for engine starting on ground
only,
b) APU is shutdown after one engine start,
c) APU is not used in flight,
d) APU Fire Detection System is operative, and
e) APU Fire Extinguishing System is operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
28-2

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

28 FUEL

4.

REMARKS OR EXCEPTIONS

13-04

GRAVITY XFLOW
"OPEN/FAIL" Switch
Light
(light function only)

13-06

Power Crossflow
SOVs
(600-2B19)

(O) May be inoperative CLOSED provided:

a) All Fuel Quantity Readouts are operative, and
b) Gravity crossflow SOV is verified operative
before each flight.

13-07

Transfer Ejectors
(Center Tank)
B

(M) One may be inoperative provided:

a) Center tank is empty, and
b) EICAS Center Tank Fuel Quantity Readout is
operative.

(M) One may be inoperative provided:

a) Center tank contains less than 500 pounds of
fuel prior to each flight,
b) Remaining fuel in center tank is considered
unusable,
c) Aircraft range is limited accordingly,
d) EICAS Center Tank Fuel Quantity Readout is
operative,
e) Both Power Crossflow SOVs are operative,
and
f) XFLOW/APU Fuel Pump is operative.

1) 600-2B19

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

28-3

NUMBER REQUIRED FOR DISPATCH

28 FUEL
Transfer Ejectors
(Center Tank)
(contd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

13-07

18

REMARKS OR EXCEPTIONS

(M) One may be inoperative provided:

a) Center tank is empty, and
b) EICAS Center Tank Fuel Quantity Readout is
operative.
(M) One may be inoperative provided:
a) Center tank contains less than 500 pounds of
fuel prior to each flight,
b) Remaining fuel in center tank is considered
unusable,
c) Aircraft range is limited accordingly,
d) EICAS Center Tank Fuel Quantity Readout is
operative, and
e) Flight crew monitors center tank fuel quantity
for proper transfer.

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
28-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

28 FUEL
13-08

18

4.

REMARKS OR EXCEPTIONS

Fuel Transfer SOVs

(Center Tank)
1) 600-2B19

a) Without
ModSum

(M) One may be inoperative CLOSED provided:

a) Center tank is empty, and
b) EICAS Center Tank Fuel Quantity Readout is
operative.

(M) One may be inoperative CLOSED provided:

a) Center tank contains less than 500 pounds of
fuel prior to each flight,
b) Remaining fuel in center tank is considered
unusable,
c) Aircraft range is limited accordingly,
d) EICAS Center Tank Fuel Quantity Readout is
operative,
e) Both Power Crossflow SOVs are operative,
and
f) XFLOW/APU Fuel Pump is operative.

(M) Both may be inoperative OPEN provided center

tank is empty.

(M) Both may be inoperative OPEN.

TC601R12716

b) With
ModSum
TC601R12716

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

28-5

NUMBER REQUIRED FOR DISPATCH

28 FUEL
Fuel Transfer SOVs
(Center Tank)
(contd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

13-08

18

REMARKS OR EXCEPTIONS

(M) One may be inoperative CLOSED provided:

a) Center Tank is empty,
b) Opposite Transfer Ejector (Center Tank) is
operative, and
c) EICAS Center Tank Fuel Quantity Readout is
operative.
(M) One may be inoperative CLOSED provided:
a) Center tank contains less than 500 pounds of
fuel prior to each flight,
b) Opposite Transfer Ejector (Center Tank) is
operative,
c) Remaining fuel in center tank is considered
unusable,
d) Aircraft range is limited accordingly,
e) EICAS Center Tank Fuel Quantity Readout is
operative, and
f) Flight crew monitors center tank fuel quantity
for proper transfer.
(M) Both may be inoperative OPEN provided center
tank is empty.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

23-01

23-02

4.
C

28-6

NUMBER REQUIRED FOR DISPATCH

28 FUEL
XFlow Pump
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

13-10

18

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative provided:

a) All EICAS Fuel Tank Quantity Readouts are
operative, and
b) Gravity crossflow SOV is verified operative.

Fuel Boost Pumps

1) 600-2B19

(M) One may be inoperative provided:

a) Inoperative boost pump is selected OFF,
b) Inoperative boost pump is deactivated,
c) XFLOW/APU Fuel Pump is operative, and
d) Power Crossflow SOVs are operative.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M) One may be inoperative provided:

a) Inoperative boost pump is deactivated, and
b) XFlow Pump is operative.

Fuel Boost Pumps

ON/INOP
Switch Lights
(light function only)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

28-7

NUMBER REQUIRED FOR DISPATCH

28 FUEL
XFLOW/APU Fuel
Pump
(600-2B19)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

24-01

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) APU is considered inoperative,
b) Power Crossflow SOVs are considered
inoperative,
c) All Fuel Quantity Readouts are operative, and
d) Operations are conducted in accordance with
AFM if fuel crossflow is required.

(M)(O) May be inoperative provided:

a) Satisfactory APU operations with both engines
OFF is established before each departure by
starting the APU using Fuel Boost Pumps,
selecting APU Bleed ON, selecting both Air
Conditioning Packs ON, and verifying the APU
operates normally,
b) Power Crossflow SOVs are considered
inoperative,
c) All Fuel Quantity Readouts are operative,
d) Operations are conducted in accordance with
AFM if fuel crossflow is required, and
e) APU Battery and APU Battery Charger System
is operative
NOTE:

Auto and manual power crossflow are

inoperative for either option.

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18

PAGE:

07/09/2012

28-8

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

28 FUEL

4.

REMARKS OR EXCEPTIONS

24-02

APU Negative
Gravity Feed Check
Valve
(600-2B19)

(O) May be inoperative provided flight operations are

not dependent on use of the APU.

24-03

APU Fuel Pump

(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M) May be inoperative provided APU is considered

inoperative.

24-04

APU PWR FUEL

"PUMP FAIL/SOV
FAIL" Switch Light
(light function only)

25-01

External Single
Point Pressure
Refueling System
(Refuel/Defuel
Control Panel)

May be inoperative provided Internal Single Point

Pressure Refueling System is operative.

1) (600-2B19)

(O) May be inoperative provided gravity refueling

procedures are used.

NOTE:

Refer to AFM for reduced fuel quantity

available when using gravity refueling.

a) Automatic
Mode

(O) May be inoperative provided manual or gravity

refueling procedure is used.

b) Manual Mode

(O) May be inoperative provided automatic or gravity

refueling procedure is used.

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

2) (600-2C10,
600-2D15,
600-2D24,
600-2E25)

28-9

NUMBER REQUIRED FOR DISPATCH

28 FUEL
External Single
Point Pressure
Refueling System
(Refuel/Defuel
Control Panel)
(contd)
1) (600-2B19)
(contd)
c) Fuel Quantity
Display
Indication

07/09/2012

PAGE:

NUMBER INSTALLED
3.

25-01

18

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) Manual or gravity refueling procedure is used,
and
b) All EICAS Fuel Tank Quantity Readouts are
operative.

(O) May be inoperative provided:

a) Manual or gravity refueling procedure is used,
and
b) All MLIs are operative.

May be inoperative provided gravity refueling

procedures are used.
NOTE:

Refer to AFM for reduced fuel quantity

available when using gravity refueling.

a) Automatic
Mode

May be inoperative provided manual or gravity

refueling procedure is used.

b) Manual Mode

May be inoperative provided automatic or gravity

refueling procedure is used.

c) Fuel Quantity
Display
Indication

May be inoperative provided:

a) Manual or gravity refueling procedure is used,
and
b) All EICAS Fuel Tank Quantity Readouts are
operative.

May be inoperative provided:

a) Manual or gravity refueling procedure is used,
and
b) All MLIs are operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

25-03

Refuel SOVs
1) 600-2B19

28-10

NUMBER REQUIRED FOR DISPATCH

28 FUEL
Refuel/Defuel
Adapter Cap

07/09/2012

PAGE:

NUMBER INSTALLED
3.

25-02

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative (missing) provided:

a) Pressure refueling adapter door is not missing,
b) Refuel/defuel adapter is visually checked for
contamination prior to each refueling, and
c) No leakage can be detected after refueling is
complete.

(M) May be inoperative CLOSED provided gravity

refueling procedures are used.
NOTE:

2) Wing
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

3) Center
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M) May be inoperative CLOSED provided gravity

refueling procedures are used for the affected tank(s).
NOTE:

Refer to AFM for reduced fuel quantity

available when using gravity refueling.

Refer to AFM for reduced fuel quantity

available when using gravity refueling.

May be inoperative provided center tank remains

empty when remaining fuel is consumed.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

Refer to AFM for reduced fuel quantity

available when using gravity refueling.

(O) Both may be inoperative provided:

a) Gravity refueling procedures are used for
affected wing tank,
b) All EICAS Fuel Tank Quantity Readouts are
operative,
c) XFlow Pump is operative,
d) Both Transfer Ejectors are operative, and
e) Both Transfer SOVs are operative.
NOTE:

25-05

REMARKS OR EXCEPTIONS

May be inoperative provided gravity refueling

procedures are used for affected tank.
NOTE:

2) Wing
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

28-11

NUMBER REQUIRED FOR DISPATCH

28 FUEL
High Level Sensors
1) 600-2B19

07/09/2012

PAGE:

NUMBER INSTALLED
3.

25-04

18

Refer to AFM for reduced fuel quantity

available when using gravity refueling.

(M)(O) Both may be inoperative provided:

a) Manual refueling procedures are used for
affected wing tank,
b) All EICAS Fuel Tank Quantity Readouts are
operative,
c) XFlow Pump is operative,
d) Both Transfer Ejectors are operative, and
e) Both Transfer SOVs are operative.

3) Center
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

May be inoperative provided center tank remains

empty.

Internal Single Point

Pressure Refueling
System
(Refuel/Defuel
Control Panel)
***

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1

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

41-01

EICAS Fuel Tank

Quantity Readouts
(Left, Right and
Total)
1) 600-2B19

28-12

NUMBER REQUIRED FOR DISPATCH

28 FUEL
EICAS Bulk Fuel
Temperature
Indication

07/09/2012

PAGE:

NUMBER INSTALLED
3.

40-01

18

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) TAT is used as an indication of fuel
temperature,
b) TAT is monitored during flight,
c) For the first flight of the day, the ambient
temperatures during last 10 hours were above
-29C for A/C last fueled with Jet A or above 36C for A/C last fueled with Jet A-1, and
d) On subsequent flights, when refueling
activities are to be conducted, local
temperatures are to be above -25C for A/C
using Jet A or above -32C for A/C using Jet
A-1 for at least 10 hours prior to the re-fueling.

(M)(O) One main fuel tank quantity readout plus total

quantity readout may be inoperative provided:
a) Both LH and RH tanks are completely filled,
b) XFLOW auto-override is selected to MANUAL,
and
c) Aircraft is refueled using Single Point Pressure
Refueling System.

(M)(O) One main fuel tank quantity readout plus total

quantity readout may be inoperative provided:
a) Total fuel carried includes at least 10% more
than the fuel load required for the planned
flight and this extra fuel is considered
unusable,
b) Manual or gravity refueling mode is used,
c) MLIs are used to verify main tank quantities
prior to each flight, and
d) XFLOW auto-override is selected to MANUAL.
NOTE:

Refer to AFM for reduced fuel quantity

available when using gravity refueling.

CAUTION:

Ensure FCOM MLI Chart, LBS or KG

column, is used as applicable.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

28-13

NUMBER REQUIRED FOR DISPATCH

28 FUEL
EICAS Fuel Tank
Quantity Readouts
(Left, Right and
Total)
(contd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

41-01

18

REMARKS OR EXCEPTIONS

(M)(O) One main fuel tank quantity readout plus total

quantity readout may be inoperative provided:
a) Both LH and RH tanks are completely filled,
b) XFLOW auto-override is selected to MANUAL,
c) Airplane is refueled using Single Point
Pressure Refueling System.
d) Associated High Level Sensor is operative,
e) Opposite side Transfer Ejector is operative,
and
f) Opposite side Fuel Transfer SOV is operative.
(M)(O) One main fuel tank quantity readout plus total
quantity readout may be inoperative provided:
a) Total fuel carried includes at least 10% more
than the fuel load required for the planned
flight,
b) Manual or gravity refueling mode is used,
c) MLIs are used to verify main tank quantities
before each flight,
d) XFLOW auto-override is selected to MANUAL,
e) Associated High Level Sensor is operative,
f) Opposite side Transfer Ejector is operative,
and
g) Opposite side Fuel Transfer SOV is operative.
NOTE:

Refer to AFM for reduced fuel quantity

available when using gravity refueling.
CAUTION: Ensure FCOM MLI Chart, LBS or KG
column, is used as applicable.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
28-14

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

28 FUEL
41-02

18

4.

REMARKS OR EXCEPTIONS

EICAS Fuel Tank

Quantity Readouts
(Center and Total)
1) 600-2B19

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M) Both may be inoperative provided:

a) Center tank remains empty,
b) Left and Right EICAS Fuel Tank Quantity
Readouts are operative, and
c) MLI is used to verify that center tank is empty
once each flight day.

(M) Both may be inoperative provided:

a) Center tank is completely filled,
b) Left and Right EICAS Fuel Tank Quantity
Readouts are operative, and
c) Aircraft is refueled using Single Point Pressure
Refueling System.

(M) Both may be inoperative provided:

a) Center tank is refueled using Single Point
Pressure Refueling System,
b) MLI is used to verify center tank quantity prior
to each flight, and
c) Left and Right EICAS Fuel Tank Quantity
Readouts are operative.

(M)(O) Both may be inoperative provided:

a) Center fuel tank remains empty,
b) Left and Right EICAS Fuel Tank Quantity
Readouts are operative, and
c) MLI is used to verify that center tank is empty
once each flight day.

(M)(O) Both may be inoperative provided:

a) Center fuel tank is completely filled,
b) Left and Right EICAS Fuel Tank Quantity
Readouts are operative, and
c) Aircraft is refueled using Single Point Pressure
Refueling System.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

28-15

NUMBER REQUIRED FOR DISPATCH

28 FUEL

41-03

07/09/2012

PAGE:

NUMBER INSTALLED
3.

41-02

18

4.

REMARKS OR EXCEPTIONS

EICAS Fuel Tank

Quantity Readouts
(Center and Total)
(contd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25
(contd)

|
B

(M)(O) Both may be inoperative provided:

a) Center fuel tank is refueled using Single Point
Pressure Refueling System,
b) MLI is used to verify center tank quantity
before each flight, and
c) Left and Right EICAS Fuel Tank Quantity
Readouts are operative.

1) FSC
(600-2B19)

One may be inoperative provided:

a) Both Transfer Ejectors (Center Tank) are
operative,
b) Both Fuel Transfer SOVs (Center Tank) are
operative,
c) Both Fuel Flow "FF" Readouts are operative,
and
d) Fuel Used Readout on synoptic page is
operative and reset prior to each flight.

2) FQGC
(600-2C10
with SB
670BA-28-008,
600-2D15,
600-2D24,
600-2E25)

(O) One may be inoperative provided:

a) Remaining fuel in center tank is considered
unusable,
b) Center tank contains less than 500 pounds of
fuel at dispatch, and
c) Gravity crossflow SOV is verified operative.

Fuel Computer
Channels

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
28-16

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

28 FUEL

4.

REMARKS OR EXCEPTIONS

41-04

Magnetic Level
Indicators

All may be inoperative provided associated EICAS

Fuel Tank Quantity Readouts are operative.

41-05

Fuel Pitch and Roll

Inclinometers

May be inoperative provided all EICAS Fuel Tank

Quantity Readouts (Left, Right, Center and Total) are
operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

REMARKS OR EXCEPTIONS

(M)(O) One may be inoperative provided:

a) Hydraulic AC Motor Pump (ACMP) 1B and
Hydraulic AC Motor Pump (ACMP) 2B are
operated continuously during flight,
b) All Hydraulic AC Motor Pumps (ACMP) are
operative,
c) Affected pump is mechanically removed and a
blanking plate is installed,
d) Both Integrated Drive Generators (IDG) are
operative, and
e) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
NOTE:

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

29-1

NUMBER REQUIRED FOR DISPATCH

29 HYDRAULIC POWER
Engine Driven
Pumps (EDP)
(Systems 1 and 2)
1) 600-2B19

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-01

18

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

(M)(O) One may be inoperative provided:

a) Same side Hydraulic AC Motor Pump (ACMP)
is operated continuously during flight,
b) All Hydraulic AC Motor Pumps (ACMP) are
operative,
c) Affected pump is mechanically removed and a
blanking plate is installed,
d) Flexible hydraulic lines at the pylon quickdisconnects are disconnected, capped and
stowed, and
e) Repairs are made within one flight day.

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
29-2

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

29 HYDRAULIC POWER
11-02

18

4.

REMARKS OR EXCEPTIONS

Hydraulic AC Motor
Pumps (ACMP)
(Systems 1 and 2)
(600-2B19)
1) ACMP 1B

(M) May be inoperative provided:

a) All other hydraulic pumps are operative,
b) Affected pump is selected OFF,
c) Inboard Ground Spoiler Pair is operative,
d) Nosewheel Steering is operative, and
e) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

2) ACMP 2B

(M) One may be inoperative provided:

a) All other hydraulic pumps are operative,
b) Affected pump is selected OFF,
c) Outboard Ground Spoiler Pair is operative,
d) Nosewheel Steering is operative,
e) Both Thrust Reverser Systems are operative,
f) Inboard Anti-Skid (System) Channel is
operative,
g) Take-off or landing is not conducted from a
contaminated runway, and
h) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

11-03

Hydraulic Heat
Exchanger Cooling
Fan

May be inoperative provided hydraulic temperature of

#1 and #2 systems on the synoptic page is monitored
not to exceed 96 degrees Celsius during ground
operations.

11-04

Hydraulic Switches
"AUTO" Function
(Hydraulic AC Motor
Pumps)

All may be inoperative provided affected pumps are

manually selected ON before each take-off and
landing.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

29-3

NUMBER REQUIRED FOR DISPATCH

29 HYDRAULIC POWER
Hydraulic
Accumulator
Pressure Gauges

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-05

18

4.

REMARKS OR EXCEPTIONS

(M) All may be inoperative provided accumulator precharge pressure is checked using a suitable ground
gauge each flight day.

(M) May be inoperative provided:

a) Affected Hydraulic Firewall SOV is deactivated,
b) Flexible hydraulic lines at the pylon quickdisconnects are disconnected, capped and
stowed,
c) Same side Engine Driven Pump (EDP) is
considered inoperative, and
d) Engine Driven Pump (EDP) on the opposite
side is operative.

(M) May be inoperative provided:

a) Affected Hydraulic Firewall SOV is deactivated,
b) Same side Engine Driven Pump (EDP) is
considered inoperative,
c) Engine Driven Pump (EDP) on the opposite
side is operative, and
d) Repairs are made within one flight day.

(Systems 1, 2 and 3)

11-06

Hydraulic
Accumulators
(Systems 1 and 2)

11-08

Hydraulic Firewall
SOVs
(Systems 1 and 2)
1) 600-2B19

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
29-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

29 HYDRAULIC POWER
12-01

18

4.

REMARKS OR EXCEPTIONS

Hydraulic AC Motor
Pump (ACMP) 3A
1) 600-2B19

(M)(O) May be inoperative provided:

a) Hydraulic AC Motor Pumps (ACMP) 3B is
operated continuously during flight,
b) Both Integrated Drive Generators (IDG 1 and
IDG 2) are operative,
c) All other hydraulic pumps are operative, and
d) Takeoff and landing performance is in
accordance with the AFM Supplement (Flight
with Landing Gear Down).
NOTE:

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

2) 600-2C10

(M)(O) May be inoperative provided:

a) Hydraulic AC Motor Pumps (ACMP) 3B is
operated continuously during flight,
b) All other hydraulic pumps are operative, and
c) Repairs are made within one flight day.

3) 600-2D15,
600-2D24,
600-2E25

(M)(O) May be inoperative provided:

a) Hydraulic AC Motor Pumps (ACMP) 3B is
operated continuously during flight,
b) All other hydraulic pumps are operative,
c) Cat II and Cat III operations are prohibited,
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative), and
e) Repairs are made within one flight day,

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|

|
|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

32-01

4.
C

EICAS Hydraulic
Reservoir Quantity
Readouts

29-5

NUMBER REQUIRED FOR DISPATCH

29 HYDRAULIC POWER
EICAS Hydraulic
Pressure Readouts
(Systems 1, 2 and 3)
(600-2B19,
600-2C10,
600-2D15,
600-2D24)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

31-01

18

REMARKS OR EXCEPTIONS

(O) All may be inoperative provided associated

pressure switches are operative.
|
|
|
|

(O) All may be inoperative provided quantity in

associated reservoir(s) is checked on reservoir sight
glass prior to each flight.

(Systems 1, 2 and 3)

34-01

Hydraulic Pump Low

Pressure Switches
(Systems 1, 2 and 3)

Three may be inoperative provided:

a) At least one Low Pressure Switch is operative
for each hydraulic system,
b) Hydraulic AC Motor Pump(s) B of the
associated system(s) is operated continuously
throughout flight, and
c) Associated Hydraulic Pressure and Quantity
Readouts are monitored during flight.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

29 HYDRAULIC POWER

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
29-6

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

PAGE:

07/09/2012

30-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

12-01

18

4.

REMARKS OR EXCEPTIONS

Wing Anti-Ice
Modulating and
SOVs

(M) Both may be inoperative provided:

a) Valves are secured CLOSED,
b) Operations are not conducted in known or
forecast icing conditions, and
c) Both Ice Detection Systems are operative.

1) 600-2B19

(M) May be inoperative CLOSED provided:

a) Valve is secured CLOSED, and
b) 14th Stage ISOL Valve is operative and
selected OPEN.

2) (600-2C10,
600-2D15,
600-2D24
without
ModSum
670T11216)

(M)(O) May be inoperative CLOSED provided:

a) Air Conditioning Pack on the affected side is
operative and is operated continuously
throughout flight,
b) Wing Cross Bleed Valve is operative,
c) Wing cross bleed selector switch is selected to
the opposite side (FROM LEFT or FROM
RIGHT), and
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

3) (600-2C10,
600-2D15,
600-2D24
with ModSum
670T11216),
(600-2E25)

(M) May be inoperative CLOSED provided:

a) Wing Cross Bleed Valve is operative,
b) Wing cross bleed selector switch is selected to
the opposite side (FROM LEFT or FROM
RIGHT), and
c) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18

PAGE:

07/09/2012

30-2

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

4.

REMARKS OR EXCEPTIONS

12-02

14th Stage ISOL

Valve
(600-2B19)

(M) May be inoperative OPEN provided:

a) Valve position indication is operative,
b) Both Ice Detection Systems are operative,
c) Both 14th Stage SOVs are operative, and
d) Both Wing Anti-Ice Modulating and SOVs are
operative.

12-03

Wing Anti-Ice
System
(600-2B19
with ModSum
TC601R15010
or
TC601R15059)

May be inoperative provided:

a) Operations are not conducted in known or
forecast icing conditions, and
b) Both Ice Detection Systems are operative.

1) Normal Control
(600-2B19
with or without
ModSum
TC601R15010
or
TC601R15059)

(M)(O) May be inoperative provided:

a) Standby Control is verified operative prior to
each flight,
b) Both Ice Detection Systems are operative, and
c) 14th Stage Isolation Valve is operative.

2) Standby Control
(600-2B19
with or without
ModSum
TC601R15010
or
TC601R15059)

(M) May be inoperative provided Normal Control is

operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

b) (600-2C10,
600-2D15,
600-2D24
with
ModSum
670T11216),
(600-2E25)

3) Outboard
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

30-3

REMARKS OR EXCEPTIONS

May be inoperative provided:

a) Wing Anti-Ice System is selected OFF,
b) Operations are not conducted in known or
forecast icing conditions, and
c) Both Ice Detection Systems are operative.
NOTE:

2) Inboard
a) (600-2C10,
600-2D15,
600-2D24
without
ModSum
670T11216)

07/09/2012

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

Wing Anti-Ice
Temperature
Sensor Elements
1) Inboard/
Outboard
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

PAGE:

NUMBER INSTALLED
3.

12-04

14

Caution message(s) will revert to a status

WING A/I FAULT upon selection of wing
anti-ice system to OFF.

(O) Two elements in one sensor pair may be

inoperative provided:
a) Air Conditioning Pack on the affected side is
operative and is operated continuously
throughout flight,
b) Wing Cross Bleed Valve is operative,
c) Wing cross bleed selector switch is selected to
the opposite side (FROM LEFT or FROM
RIGHT), and
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(O) Two elements in one sensor pair may be

inoperative provided:
a) Wing Cross Bleed Valve is operative,
b) Wing cross bleed selector switch is selected to
the opposite side (FROM LEFT or FROM
RIGHT), and
c) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(O) One element per sensor pair may be inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

30-4

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

12-06

07/09/2012

PAGE:

NUMBER INSTALLED
3.

12-05

18

4.

REMARKS OR EXCEPTIONS

Wing Cross Bleed

Valve
(Anti-Ice)
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

1) (600-2C10,
600-2D15,
600-2D24
without ModSum
670T11216)

(M)(O) May be inoperative OPEN provided:

a) Wing Cross Bleed Valve is secured open,
b) Air Conditioning Pack on the non-selected
side is operative and is operated continuously
throughout flight, and
c) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

|
|

2) (600-2C10,
600-2D15,
600-2D24
with ModSum
670T11216,
(600-2E25)

(M) May be inoperative OPEN provided:

a) Wing Cross Bleed Valve is secured open, and
b) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

|
|

Anti-Ice/Bleed Leak
Detection Controller
(AILC) Channels
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M) May be inoperative CLOSED provided:

a) Both Wing Anti-Ice Modulating SOVs are
operative,
b) Wing Cross Bleed Valve is secured closed,
c) Operations are not conducted in known or
forecast icing conditions, and
d) Both Ice Detection Systems are operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
30-5

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

4.

REMARKS OR EXCEPTIONS

12-07

BLEED AIR 14th

Stage ISOL "OPEN"
Switch Light
(light function only)
(600-2B19)

12-08

Outboard Low Heat

Switches
(600-2B19
with ModSum
TC601R17364 or
TC601R17494)

May be inoperative until required by FAR

(O) May be inoperative provided:

a) Operations are not conducted in known or
forecast icing conditions, and
b) Both Ice Detection Systems are operative.

(M) One switch per wing may be inoperative provided:

a) Switch failed in closed state is deactivated,
and
b) Remaining switch is verified operative.

22-01

Engine Cowl
Anti-Ice SOVs

(M) One may be inoperative provided:

a) Valve is secured CLOSED,
b) Both Ice Detection Systems are operative,
c) Operations are not conducted in known or
forecast icing conditions, and
d) Operations are conducted in accordance with
AFM Limitations.

22-02

Engine Cowl
Anti-Ice Pressure
Relief Valves
(Blow-Off Valves)
(600-2B19)

One may be inoperative OPEN provided:

a) Both Ice Detection Systems are operative,
b) Associated Thrust Reverser is operative,
c) Associated Bleed Air 14th Stage SOV is
operative, and
d) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

May be inoperative OPEN provided:

a) Associated Engine Cowl Anti-Ice SOV is
selected OFF,
b) Both Ice Detection Systems are operative, and
c) Operations are not conducted in known or
forecast icing conditions.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

31-01

4.
2

30-6

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

Cowl Anti-Ice
Double Wall Duct
Pressure
Transducers
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

22-03

18

REMARKS OR EXCEPTIONS

One may be inoperative provided:

a) Associated Engine Cowl Anti-Ice SOV is
selected OFF and considered inoperative,
b) Both Ice Detection Systems are operative, and
c) Operations are not conducted in known or
forecast icing conditions.
|

Probe Heaters
1) Pitot / Static
Probe Heaters

(M) Except where enroute operations require its use,

one may be inoperative provided:
a) Standby Pitot Head Heater is operative,
b) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
c) Operations are not conducted in known or
forecast icing conditions,
d) Both Ice Detection Systems are operative, and
e) Operations are conducted in day VMC only.

2) Static Port
Heaters

(M) Except where enroute operations require its use,

one may be inoperative provided:
a) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
b) Operations are not conducted in known or
forecast icing conditions,
c) Both Ice Detection Systems are operative, and
d) Operations are conducted in day VMC only.

3) Angle of Attack
Vane Heaters

(M) One may be inoperative provided:

a) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
b) Operations are not conducted in known or
forecast icing conditions,
c) Both Ice Detection Systems are operative, and
d) Operations are conducted in day VMC.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
30-7

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

31-01

18

4.

REMARKS OR EXCEPTIONS

Probe Heaters
(cont'd)
4) TAT Probe
Heater
a)

600-2B19

(M) May be inoperative provided:

a) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
b) Operations are not conducted in known or
forecast icing conditions,
c) Both Ice Detection Systems are operative, and
d) Operations are conducted in day VMC only.

b)

600-2C10,
600-2D15,
600-2D24,
600-2E25

(M) May be inoperative provided:

a) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
b) Operations are not conducted in known or
forecast icing conditions,
c) Both Ice Detection Systems are operative,
d) Operations are conducted in day VMC only,
and
e) Both engines T2 sensors and T2 heaters are
operative.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

30-8

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

Probe Heaters
(cont'd)
5) Base Heaters
(600-2B19)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

31-01

18

4.

REMARKS OR EXCEPTIONS

(M) Both may be inoperative provided:

a) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
b) Operations are not conducted in known or
forecast icing conditions,
c) Both Ice Detection Systems are operative, and
d) Operations are conducted in day VMC only.

6) Standby Pitot
Head Heater

(M) May be inoperative provided:

a) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
b) Operations are not conducted in known or
forecast icing conditions,
c) Both Ice Detection Systems are operative, and
d) Operations are conducted in day VMC only.

7) Engine T2
Probe Heaters
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M) May be inoperative provided:

a) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
b) Operations are not conducted in known or
forecast icing conditions,
c) Both Ice Detection Systems are operative, and
d) Operations are conducted in day VMC
conditions only.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
30-9

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

4.

REMARKS OR EXCEPTIONS

31-02

Air Data Sensor

Heater Controllers

(M) One may be inoperative provided:

a) Operations are not conducted in visible
moisture (including standing water and slush)
in any form,
b) Operations are not conducted in known or
forecast icing conditions,
c) Both Ice Detection Systems are operative, and
d) Operations are conducted in day VMC only.

41-01

Windshield and Side

Window Anti-Ice
Systems

(M) One may be inoperative provided:

a) Affected anti-ice controller is deactivated,
b) Operations are not conducted in known or
forecast icing conditions, and
c) Pilot's (Left) Side window heating is operative.

(M) Two may be inoperative provided:

a) Affected anti-ice controllers are deactivated,
b) Operations are not conducted in known or
forecast icing conditions,
c) Pilot's (Left) Side window heating is operative,
and
d) Both Ice Detection Systems are operative.

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
30-10

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

4.

42-01

Windshield Wipers

71-01

Aft Waste Service

Panel Heater
(600-2B19)

REMARKS OR EXCEPTIONS

May be inoperative provided:

a) Position of the affected wiper blade is
acceptable to the associated pilot, and
b) Any function that operates normally may be
used.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

71-03

Potable Water
Freeze Protection
Systems
(600-2B19)

30-11

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

Drain Mast Heater

07/09/2012

PAGE:

NUMBER INSTALLED
3.

71-02

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Associated sink is not used, and
b) Sink and/or coffee water supply is turned off.

1) Galley Water
System Freeze
Protection
(excluding water
tank heater)

(M) May be inoperative provided the galley water tank

is drained.

2) Lavatory Water
System Freeze
Protection
(excluding water
tank heater)

(M) May be inoperative provided lavatory water tank is

drained.

3) Galley Water
Tank Heater

(M) May be inoperative provided:

a) Heater is deactivated, and
b) Galley water system is drained if ground
operations below 0 degrees Celsius (32
degrees Fahrenheit) ambient will exceed 3
hours.

4) Lavatory Water
Tank Heater

(M) May be inoperative provided:

a) Heater is deactivated, and
b) Lavatory water system is drained.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

1) 600-2C10,
600-2D15,
600-2D24,
600-2E25

30-12

NUMBER REQUIRED FOR DISPATCH

30 ICE AND RAIN PROTECTION

Ice Detection
Systems

07/09/2012

PAGE:

NUMBER INSTALLED
3.

81-01

18

4.

REMARKS OR EXCEPTIONS

(M) One may be inoperative provided wing and cowl

anti-ice systems are turned ON when icing conditions
as defined in the AFM exist or are anticipated.

(M) Both may be inoperative provided:

a) Operations are not conducted in known or
forecast icing conditions,
b) Wing and cowl anti-ice systems are turned ON
when icing conditions as defined in the AFM
exist or are anticipated, or when any ice buildup on the aircraft is observed, and
c) Repairs are made within one flight day.

(M) Both may be inoperative provided:

a) Operations are conducted during the day,
b) Wing and cowl anti-ice systems are turned ON
when icing conditions as defined in the AFM
exist or are anticipated, or when any ice buildup on the aircraft is observed, and
c) Repairs are made within one flight day.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
31-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

31 INDICATING/RECORDING
SYSTEMS

4.

REMARKS OR EXCEPTIONS

14-01

Master Warning
Switch Lights
(Glareshield)
(light function only)

14-02

Master Caution
Switch Lights
(Glareshield)
(light function only)

21-01

Clocks

As required by regulations.

(O) Both may be inoperative provided:

a) Both pilot and co-pilot have ready access to a
reliable timepiece which display seconds (a
wristwatch is acceptable),
b) Approach procedures do not require timing,
c) FDR is considered inoperative, and
d) Repairs are made within one flight day.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

31-2

NUMBER REQUIRED FOR DISPATCH

31 INDICATING/RECORDING
SYSTEMS
Flight Data
Recorder (FDR)
System

07/09/2012

PAGE:

NUMBER INSTALLED
3.

31-01

18

4.

REMARKS OR EXCEPTIONS

Any in excess of those required by regulation may be

inoperative.

May be inoperative provided:

a) Cockpit Voice Recorder (CVR) operates
normally,
b) Aircraft is not dispatched from a designated
airport as listed in the operator's MEL unless:
1. The FDR failure occurs after pushback but
prior to takeoff, or
2. The FDR repair was attempted but was not
successful.
c) In those cases where repair is attempted but
not successful, the aircraft may be dispatched
on a flight or series of flights until the next
designated airport where repair must be
accomplished prior to dispatch, and
d) Repairs are made within three flight days.

1) FDR Recording
Parameters
required by
regulations

May be inoperative provided:

a) Cockpit Voice Recorder (CVR) operates
normally, and
b) Repairs are made within 20 calendar days.

2) FDR Recording
Parameters not
required by
regulations

May be inoperative provided repairs are made prior to

the completion of the next heavy maintenance visit.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

41-01

Data Concentrator
Units (DCUs)
1) 600-2B19

07/09/2012

31-3

NUMBER REQUIRED FOR DISPATCH

31 INDICATING/RECORDING
SYSTEMS
Quick Access
Recorder (QAR)
***

PAGE:

NUMBER INSTALLED
3.

31-02

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Inoperative DCU is deactivated,
b) Associated AUDIO WARNING DISABLE
switch is selected, and
c) Two separate audio warning channels are
verified operative before each flight.
NOTE 1: In the event of a DCU1 failure both Master
Warning and Master Caution lights will not
test during the Lamp 1 test.
NOTE 2: In the event of a DCU2 failure, Master
Warning and Master Caution lights will not
test during the Lamp 2 test.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M) May be inoperative provided:

a) Inoperative DCU is deactivated, and
b) Associated AUDIO WARNING DISABLE
switch is selected.
NOTE 1: In the event of a DCU1 failure both Master
Warning and Master Caution lights will not
test during the Lamp 1 test.
NOTE 2: In the event of a DCU2 failure, Master
Warning and Master Caution lights will not
test during the Lamp 2 test.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18

PAGE:

07/09/2012

31-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

31 INDICATING/RECORDING
SYSTEMS

4.

REMARKS OR EXCEPTIONS

41-02

EICAS Control
Panel (ECP)
Discrete Buttons
a) ECS
b) HYD
c) ELEC
d) FUEL
e) F/CTL
f) A/ICE
g) DOORS
h) SEL
i) MENU
j) UP
k) DN

Each may be inoperative provided PRIM, STAT, CAS

and STEP buttons are verified operative.

41-03

Lamp Driver Unit

Channels

(M) One channel may be inoperative provided:

a) Affected channel is deactivated, and
b) Remaining channel is tested operative.

41-04

Data Concentration
Units (DCU) Fans

41-05

AUDIO WARNING
DCU Switch Guards

61-01

EICAS Display Units

(ED #1 or ED #2)

May be inoperative provided DCU associated with

operative switch guard is operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
32-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

32 LANDING GEAR
30-01

18

4.

REMARKS OR EXCEPTIONS

Landing Gear
Retraction System
1) 600-2B19

(M) May be inoperative provided:

a) Operations are conducted in accordance with
AFM Supplement (Flight with Landing Gear
Down),
b) Operations are not conducted in known or
forecast icing conditions,
c) Ground lock pins are installed to ensure that
all three landing gears are locked down
throughout flight,
d) In-flight performance information given in
Flight Planning and Cruise Control Manual is
used,
e) Extended overwater operations are prohibited,
f) Both headsets are worn,
g) Flight Compartment and Cabin Interphone
Systems are operative,
h) Both Flap Electronic Control Unit Channels
are operative,
i) Both Flap Power Drive Unit Motors are
operative,
j) Cat II and Cat III operations are prohibited,
and
k) Repairs are made within one flight day.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

32-2

NUMBER REQUIRED FOR DISPATCH

32 LANDING GEAR
Landing Gear
Retraction System
(cont'd)
2) 600-2C10
600-2D15,
600-2D24,
600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

30-01

18

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Operations are conducted in accordance with
AFM Supplement (Flight with Landing Gear
Down),
b) Operations are not conducted in known or
forecast icing conditions,
c) Ground lock pins are installed to ensure that all
three landing gears are locked down
throughout flight,
d) Inflight performance information given in the
Flight Planning and Cruise Control Manual
(FPCCM) or the Computerized InFlight
Performance (CIFP) is used,
e) Extended over water operations are prohibited,
f) Both headsets are worn,
g) Flight Compartment and Cabin Interphone
systems are operative,
h) Both Flap Channels of the Slat Flap Electronic
Control Unit are operative,
i) Both Flap Power Drive Unit Motors are
operative,
j) Both Slat Channels of the Slat Flap Electronic
Control Unit are operative,
k) Both Slat Power Drive Unit Motors are
operative,
l) Cat II and Cat III A operations are prohibited,
and
m) Repairs are made within one flight day.

|
|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18

PAGE:

07/09/2012

32-3

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

32 LANDING GEAR

4.

REMARKS OR EXCEPTIONS

31-01

Landing Gear
Selector Handle
Anti-Retraction
Mechanism

(M) May be inoperative in LOCKED position (down)

provided downlock release mechanism is verified
operative.

40-01

Tire Pressure
Indicator
***
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M)

42-01

Nose Wheel Spin

Down Straps
(600-2C10,
600-2D15,
600-2D24)

(M) May be inoperative provided:

a) Straps are removed, and
b) Nose wheel tires are visually checked for
damage.

43-01

Brake Accumulator
Pressure Gauges

(M) Both may be inoperative provided accumulator

pre-charge pressure is checked using a suitable
pressure gauge each flight day.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
32-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

32 LANDING GEAR
44-01

18

4.

REMARKS OR EXCEPTIONS

Anti-Skid System
Channels
1) 600-2B19,
600-2C10

(M)(O) Either the inboard or outboard channel may be

inoperative provided:
a) Nosewheel Steering is operative,
b) Both pairs of Ground Spoilers are operative,
c) Both Thrust Reversers are operative,
d) Both inboard and outboard wheel brakes are
verified operative,
e) Both EICAS Brake Temperature Monitoring
Readouts associated with the operative antiskid channel are operative,
f) Reduced thrust take-off operations are
prohibited,
g) Take-off or landing is not conducted from a
contaminated runway, and
h) Operations are conducted in accordance with
AFM Supplement (Operations with Anti-Skid
Inoperative).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

45-01

Parking Brake
Handle Locking
Positions
(clockwise and
counter-clockwise)

4.

32-5

NUMBER REQUIRED FOR DISPATCH

32 LANDING GEAR
Anti-Skid System
Channels
(contd)
2) 600-2D15,
600-2D24,
600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

44-01

18

REMARKS OR EXCEPTIONS

(M)(O) Either the inboard or outboard channel may be

inoperative provided:
a) Nosewheel Steering is operative,
b) Both pairs of Ground Spoilers are operative,
c) Both Thrust Reversers are operative,
d) Both inboard and outboard wheel brakes are
verified operative,
e) Both EICAS Brake Temperature Monitoring
Readouts associated with the operative antiskid channel are operative,
f) Reduced thrust take-off operations are
prohibited,
g) Take-off is not conducted from a wet runway,
h) Take-off or landing is not conducted from a
contaminated runway, and
i) Operations are conducted in accordance with
AFM Supplement (Operations with Anti-Skid
Inoperative).
(O) May be inoperative provided:
a) Parking brake system is verified operative,
b) Remaining locking position is verified
operative before each flight, and
c) Inoperative locking position is legibly
placarded.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

46-02

47-01

32-6

NUMBER REQUIRED FOR DISPATCH

32 LANDING GEAR
EICAS Brake
Temperature
Monitoring
Readouts

07/09/2012

PAGE:

NUMBER INSTALLED
3.

46-01

18

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative for indication ---- provided:

a) AFM quick turn-around landing weight charts
are used, and
b) Minimum brake cooling times (AFM
Performance) are observed.

One per each side may be inoperative for

indication ----.

(M)(O) May be inoperative for inaccurate indication

provided:
a) Affected sensor is deactivated,
b) AFM quick turn-around landing weight charts
are used, and
c) Minimum brake cooling times (AFM
Performance) are observed.

(M) One per each side may be inoperative for

inaccurate indication provided affected sensor is
deactivated.

A/SKID
Sub-system
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M)(O) May be inoperative as indicated by A/SKID

FAULT status message on EICAS.

EICAS Brake
Pressure Readouts

|
2

(M) Both may be inoperative provided:

a) Brake accumulator(s) nitrogen pressure is
verified prior to the first flight of the day,
b) Capability of brake accumulators to retain
adequate hydraulic fluid for brakes is verified
prior to the first flight of the day, and
c) EICAS Hydraulic Pressure Readouts are
operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
32-7

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

32 LANDING GEAR
50-01

18

4.

REMARKS OR EXCEPTIONS

Nosewheel Steering
1) 600-2B19

(M) May be inoperative provided:

a) Solenoid selector valve is not failed OPEN,
b) Landing gear selector valve is verified
operative,
c) Nosewheel steering system is selected OFF,
d) Take-off or landing is not conducted from a
contaminated runway,
e) Aircraft is towed from ramp/gate to initial
taxiway and from final taxiway to ramp/gate,
f) Flight/Ground Spoiler Systems are operative,
g) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems inoperative), and
h) Repairs are made after one flight.
NOTE:

Asymmetric brakes rather than asymmetric

thrust should be used to maintain directional
control as required at low speed end of the
roll.
(cont'd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

Proximity Sensing
System
(600-2C10,
600-2D15,
600-2D24,
600-2E25
with Modsum
670T31999)

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Solenoid selector valve is not failed OPEN,
b) Landing gear selector valve is verified
operative,
c) Nosewheel steering system is selected OFF,
d) Take-off or landing on contaminated runway is
prohibited,
e) Aircraft is towed from ramp/gate to initial
taxiway and from final taxiway to ramp/gate,
f) Both pairs of Ground Spoilers are operative,
g) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems inoperative), and
h) Repairs are made after one flight.
NOTE:

60-01

32-8

NUMBER REQUIRED FOR DISPATCH

32 LANDING GEAR
Nosewheel Steering
(cont'd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

50-01

18

|
|

Asymmetric brakes rather than asymmetric

thrust should be used to maintain directional
control as required at low speed end of the
roll.

System redundancy may be degraded as indicated by

PROX SYS FAULT 2 status message.

|
|
|
|
|
|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

13-01

33-1

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Cockpit/Flight
Deck/Flight
Compartment and
Instrument Lighting
Systems
(excluding EFIS)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-01

18

4.

REMARKS OR EXCEPTIONS

Individual lights may be inoperative provided

remaining lights are:
a) Sufficient to clearly illuminate all required
instruments, controls and other devices for
which it is provided,
b) Positioned so that direct rays are shielded from
flight crew members eyes, and
c) Lighting configuration and intensity is
acceptable to flight crew.

May be inoperative provided:

a) Aircraft is not operated at night, and
b) Lighting configuration and intensity is
acceptable to the flight crew.

1) 600-2B19

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

Cockpit Dome
Lights

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
33-2

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
21-01

18

4.

REMARKS OR EXCEPTIONS

Cabin Interior Lights

1) 600-2B19
a) A/c without
ModSum

May be inoperative provided:

a) Sufficient lighting is operative for cabin crew to
perform required duties, and
b) Lighting configuration at dispatch is acceptable
to the flight crew.

(O) Up to 25% of galley light individual lamps, up to

25% of sidewall downwash lights and up to 25% of
ceiling lights may be inoperative provided:
a) No more than two adjacent and no opposite
ceiling lights may be inoperative,
b) No more than two adjacent and no opposite
sidewall downwash lights may be inoperative,
c) Cabin interior light brightness control is
operative or failed in a bright state,
d) Sufficient lighting is operative for cabin crew to
perform required duties,
e) Lighting configuration at dispatch is acceptable
to the flight crew, and
f) Procedures for charging the Photoluminescent
Floor Proximity Emergency Escape Path
Marking System before the first flight of the day
are observed.

TC601R101452,

or
TC601R101462,

or
TC601R101520

b) A/c with or
without
ModSum
TC601R101576

and either
ModSum
TC601R101452,

or
TC601R101462,

or
TC601R101520

(cont'd)

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

TC601R101576

with either
ModSum
TC601R101452,
TC601R101462,

or
TC601R101520

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25
a) A/c with
Fluorescent
Lights

33-3

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Cabin Interior Lights
(contd)
1) 600-2B19
(contd)
c) A/c with
ModSum

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-01

18

REMARKS OR EXCEPTIONS

(O) Up to 25% of galley light individual lamps, up to

25% of sidewall downwash lights may be inoperative
provided:
a) All ceiling lights are operative,
b) No more than two adjacent and no opposite
sidewall downwash lights may be inoperative,
c) Cabin interior light brightness control is
operative or failed in a bright state,
d) Sufficient lighting is operative for cabin crew to
perform required duties,
e) Lighting configuration at dispatch is acceptable
to the flight crew, and
f) Procedures for charging the Photoluminescent
Floor Proximity Emergency Escape Path
Marking System before the first flight of the day
are observed.

|
C

All sidewall downwash lights and up to 50% of ceiling

lights may be inoperative provided:
a) No more than two adjacent and no opposite
ceiling lights may be inoperative,
b) Cabin interior light brightness control is
operative or failed in a bright state,
c) Sufficient lighting is operative for cabin crew to
perform required duties, and
d) Lighting configuration at dispatch is acceptable
to the flight crew.

(cont'd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

33-4

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Cabin Interior Lights
(contd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25
b) A/c with LED
Lights

PAGE:

NUMBER INSTALLED
3.

21-01

18

4.

REMARKS OR EXCEPTIONS

|
C

(O) Up to 50% of total length of ceiling upwash lights

and up to 50% of sidewall downwash lights may be
inoperative provided:
a) Inoperative lighting configuration is verified
acceptable,
b) Brightest state of cabin interior light brightness
control is available,
c) Sufficient lighting is operative for cabin crew to
perform required duties, and
d) Lighting configuration at dispatch is acceptable
to the flight crew.

21-02

Stair Lights

23-01

Boarding Lights
(600-2B19)

23-02

Entrance Lights
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

Passenger Notice
System (No
Smoking / Fasten
Seat Belts)

(O) May be inoperative provided:

a) PA system is operative, and
b) Procedures are established and used to alert
flight attendants and notify passengers when
seat belts are to be fastened and smoking is
prohibited.

1) Automatic
function

(O) May be inoperative provided:

a) Manual control function is verified operative,
and
b) Alternate procedures are established and
used.

24-01

May be inoperative provided sufficient lighting for

cabin crew is available to perform required duties.

(cont'd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

33-5

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Passenger Notice
System (No
Smoking / Fasten
Seat Belts)
(contd)
2) No Smoking/
Fasten Seat
Belt Signs

07/09/2012

PAGE:

NUMBER INSTALLED
3.

24-01

18

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) PA system is operative, and
b) Procedures are established and used to alert
flight attendants and notify passengers when
seat belts are to be fastened and smoking is
prohibited.

(O) One or more may be inoperative provided

passenger or flight attendant seats from which a sign
is illegible or missing shall not be occupied and must
be blocked and placarded "DO NOT OCCUPY".

31-01

Service Lights

32-01

Maintenance Lights

41-01

Landing Lights
C

Two may be inoperative provided:

a) Both Taxi/Recognition Lights are operative,
and
b) Taxi/Recognition Lights are switched OFF
whenever airplane is stationary in excess of 10
minutes.

All may be inoperative provided aircraft is not operated

at night.

1) 600-2B19

(cont'd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

REMARKS OR EXCEPTIONS

Landing Lights
(contd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25
a) Nose Light

|
C

May be inoperative provided:

a) Both Wing Landing Lights are operative, and
b) Both Taxi/Recognition Lights are operative.

May be inoperative provided aircraft is not operated at

night.

One may be inoperative provided the associated

Taxi/Recognition Light is operative.

Both may be inoperative provided aircraft is not

operated at night.

Taxi/Recognition
Lights

Both may be inoperative provided aircraft is not

operated at night.

1) 600-2B19

Both may be inoperative provided two Landing Lights

are operative.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

Both may be inoperative provided all Landing Lights

are operative

Pulsating Landing
Lights System
***
(600-2B19)

b) Wing Lights

41-03

33-6

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS

41-02

07/09/2012

PAGE:

NUMBER INSTALLED
3.

41-01

18

|
1

(M) May be inoperative provided:

a) System is deactivated, and
b) Landing Light System is verified operative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

33-7

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS

4.

REMARKS OR EXCEPTIONS

Navigation Lights
1) Wing Tip
Position Light
Bulbs

2) Aft Position
Light Bulbs

43-01

07/09/2012

PAGE:

NUMBER INSTALLED
3.

42-01

18

Wing Inspection
Lights

One light bulb may be inoperative at each wing tip.

All may be inoperative provided aircraft is not operated

at night.

Both may be inoperative provided aircraft is not

operated at night.

Both may be inoperative provided:

a) Ground de-icing procedures do not require
their use, and
b) A portable lamp/light of adequate capacity for
wing and/or control surface inspection is
available for night operations in icing
conditions.

Both may be inoperative provided aircraft is not

operated at night.

44-01

High Intensity AntiCollision Strobe

Lights

May be inoperative provided aircraft is not operated at

night.

44-02

Low Intensity Red

Beacon Lights

Bottom light may be inoperative.

45-01

Sterile Light System

***

(O) May be inoperative provided alternate procedures

are established and used.

46-01

Tail Flood Lights

(Logo Lights)
***

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

33-8

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS

4.

Cabin Emergency
Lights

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) Assigned aircraft crew are the only occupants
of the aircraft,
b) No crew occupies area of affected lights,
c) Alternate procedures are established and
used, and
d) Repairs are made within one flight.

a) Ceiling Level
Emergency
Floodlights

Two ceiling floodlights may be inoperative provided

they are not adjacent to each other.

b) Floor Level
Emergency
Floodlights
A/c without
ModSum

Three out of five light bulbs within each floor floodlight

may be inoperative.

Three out of five bulbs within each floodlight may be

inoperative.

1) 600-2B19

TC601R101462,

or
TC601R101470,

or
TC601R101520

c) Floor Level
Emergency
Floodlights
A/c with
ModSum
TC601R101462,

or
TC601R101470,

or
TC601R101520

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

33-9

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS

4.

Cabin Emergency
Lights
(cont'd)
1) 600-2B19
(cont'd)
d) Ceiling Level
Lighted Exit
Signs
(Curved Signs)

PAGE:

NUMBER INSTALLED
3.

51-01

18

REMARKS OR EXCEPTIONS

Each exit sign may have 50% of its internal lights

inoperative, except that both tip lights in exit sign must
be operative.

e) Lighted Exit
Signs

Each exit sign may have 50% of it's internal lights

inoperative.

f) Floor Level
Lighted Exit
Signs
A/c with
ModSum

Three out of five bulbs within each sign may be

inoperative.

TC601R101462,

or
TC601R101470,

or
TC601R101520

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

33-10

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Cabin Emergency
Lights
(contd)
1) 600-2B19
(cont'd)
g) Electroluminescent Floor
Proximity
Emergency
Escape Path
Marking
System
A/c without
ModSum

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

REMARKS OR EXCEPTIONS

Up to 50% of the individual floor- mounted lighting

strips may be inoperative provided they are not
adjacent to each other. Strips with orange overlays at
the Service Door must be operative.

TC601R101462,

or
TC601R101452,

or
TC601R101520

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
33-11

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
51-01

18

4.

REMARKS OR EXCEPTIONS

Cabin Emergency
Lights
(cont'd)
1) 600-2B19
(cont'd)
h) Photoluminescent Floor
Proximity
Emergency
Escape Path
Marking
System
Strip/Tape
***
A/c with
ModSum
TC601R101462,
or
TC601R101452,
or
TC601R101520

|
|
C

May be damaged or segment(s) missing provided:

a) Length of the affected section(s) does not
exceed 8 in. (20 cm),
b) Affected section(s) is not attached to the
overwing exit marker cross sections,
c) Overwing exit marker cross sections are not
affected,
d) Aft cabin cross-aisle section is not affected,
e) Interval between affected sections on the same
side is not less than 128 in. (326 cm.),
f) Interval between affected sections on the
opposite side is not less than 60 in. (153 cm.),
and
g) Maximum total length of the affected sections
on both sides does not exceed 48 in. (120 cm).
NOTE:

For the purpose of this item, the term

"damaged" implies a degradation of the path
marking system strip/tape that prevents the
system to perform its intended functions
(permanent stain masking the path marking
system strip/tape).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

PAGE:

07/09/2012

33-12

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
51-01

18

4.

REMARKS OR EXCEPTIONS

Cabin Emergency
Lights
(cont'd)
2) 600-2C10
a) Ceiling Level
Emergency
Floodlights

b) Floor Level
Emergency
Floodlights

c) Ceiling Level
Lighted Exit
Signs (Curved
Signs)

Each exit locator may have 50% of its internal lights

inoperative, except that tip lights in exit sign must be
operative.

d) Lighted Exit
Signs

Each exit sign may have 50% of its internal lights

inoperative.

e) Floor Level
Lighted Exit
Signs

Each floor proximity exit sign may have 50% of its

internal lights inoperative.

Two lights may be inoperative provided they are not

adjacent to each other.

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

33-13

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS

07/09/2012

PAGE:

NUMBER INSTALLED
3.

Cabin Emergency
Lights
(cont'd)
2) 600-2C10
(cont'd)
f) Photoluminescent Floor
Proximity
Emergency
Escape Path
Marking
System
Strip/Tape

18

REMARKS OR EXCEPTIONS

May be damaged or segment(s) missing provided:

a) Length of the affected section(s) does not
exceed 8 in. (20 cm),
b) Affected section(s) is not attached to the
overwing exit marker cross sections,
c) Overwing exit marker cross sections are not
affected,
d) Interval between affected sections on the same
side is not less than 128 in. (326 cm.),
e) Interval between affected sections on the
opposite side is not less than 60 in. (153 cm.),
and
f) Maximum total length of the affected sections
on both sides does not exceed 72 in. (180 cm).
NOTE:

For the purpose of this item, the term

"damaged" implies a degradation of the path
marking system strip/tape that prevents the
system to perform its intended functions
(permanent stain masking the path marking
system strip/tape).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

PAGE:

07/09/2012

33-14

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
51-01

18

4.

REMARKS OR EXCEPTIONS

Cabin Emergency
Lights
(cont'd)
3) 600-2D15,
600-2D24
a) Ceiling Level
Emergency
Flood Lights

b) Floor Level
Emergency
Floodlights

c) Ceiling Level
Lighted Exit
Signs (Curved
Signs)

Each exit locator may have 50% of its internal lights

inoperative, except that tip lights in exit sign must be
operative.

d) Lighted Exit
Signs

Each exit sign may have 50% of its internal lights

inoperative.

e) Floor Level
Lighted Exit
Signs

Each floor proximity exit sign may have 50% of its

internal lights inoperative.

Three lights may be inoperative provided they are not

adjacent to each other.

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

33-15

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Cabin Emergency
Lights
(cont'd)
3) 600-2D15,
600-2D24
(cont'd)
f) Photoluminescent Floor
Proximity
Emergency
Escape Path
Marking
System
Strip/Tape

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

REMARKS OR EXCEPTIONS

May be damaged or segment(s) missing provided:

a) Length of the affected section(s) does not
exceed 8 in. (20 cm),
b) Affected section(s) is not attached to the
overwing exit marker cross sections,
c) Overwing exit marker cross sections are not
affected,
d) Interval between affected sections on the same
side is not less than 128 in. (326 cm.),
e) Interval between affected sections on the
opposite side is not less than 60 in. (153 cm.),
and
f) Maximum total length of the affected sections
on both sides does not exceed 88 in. (220 cm).
NOTE:

For the purpose of this item, the term

"damaged" implies a degradation of the path
marking system strip/tape that prevents the
system to perform its intended functions
(permanent stain masking the path marking
system strip/tape).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

33-16

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Cabin Emergency
Lights
(cont'd)
4) 600-2E25
a) Ceiling Level
Emergency
Floodlights

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

4.

REMARKS OR EXCEPTIONS

Up to five lights may be inoperative provided they are

not adjacent to each other.

|
|
|
|

b) Floor Level
Emergency
Floodlights

c) Ceiling Level
Lighted Exit
Signs
(Curved Signs)

Each exit locator may have 50% of its internal lights

inoperative, except that tip lights in exit sign must be
operative.

|
|
|
|

d) Lighted Exit
Signs

Each exit sign may have 50% of its internal LED lights
inoperative.

|
|

e) Floor Level
Lighted Exit
Signs

Each floor proximity exit sign may have 50% of its

internal LED lights inoperative.

|
|
|

|
|
|

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

33-17

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Cabin Emergency
Lights
(cont'd)
4) 600-2E25
(contd)
f) Photoluminescent Floor
Proximity
Emergency
Escape Path
Marking
System
Strip/Tape

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-01

18

4.

REMARKS OR EXCEPTIONS

|
C

May be damaged or segment(s) missing provided:

a) Length of the affected section(s) does not
exceed 8 in. (20 cm),
b) Affected section(s) is not attached to the
overwing exit marker cross sections,
c) Overwing exit marker cross sections are not
affected,
d) Interval between affected sections on the same
side is not less than 128 in. (326 cm),
e) Interval between affected sections on the
opposite sides is not less than 60 in. (153 cm),
and
f) Maximum total length of the affected sections
on both sides does not exceed 88 in. (220 cm).

|
|
|
|
|
|
|
|
|
|
|
|
|
|

NOTE:

|
|
|
|
|
|

For the purpose of this item, the term

damaged implies a degradation of the path
marking system strip/tape that prevents the
system to perform its intended functions
(permanent stain masking the path marking
system strip/tape).

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

51-03

33-18

NUMBER REQUIRED FOR DISPATCH

33 LIGHTS
Exterior Emergency
Lights

07/09/2012

PAGE:

NUMBER INSTALLED
3.

51-02

18

4.

REMARKS OR EXCEPTIONS

All may be inoperative provided aircraft is not operated

at night.

(O) May be inoperative provided:

a) Assigned aircraft crew are the only occupants
of the aircraft,
b) Alternate procedures are established and
used, and
c) Repairs are made within one flight day.

1) 600-2B19

One of two rearward overwing lights on each side of

the aircraft may be inoperative.

2) 600-2D15,
600-2D24,
600-2E25

The forward overwing emergency light on each side of

the aircraft may be inoperative.

Emergency Lights
"OFF" Light
(light function only)
(600-2B19)

|
1

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

14-01

21-01

34-1

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION

4.

Integrated Standby
Instruments (ISI)
(600-2B19***,
600-2C10,
600-2D15,
600-2D24,
600-2E25)
1) NAV Function

07/09/2012

PAGE:

NUMBER INSTALLED
3.

12-01

18

REMARKS OR EXCEPTIONS

|
C

2) Attitude
Function

May be inoperative provided:

a) Operations are conducted in day VMC only,
b) Operations are not conducted into known or
forecast VFR- on-Top conditions, and
c) Source selector is selected to NORMAL with
each side fed from its on-side AHRS/IRS.

Altitude Alerting
System

(O) May be inoperative provided:

a) Autopilot with altitude hold, and altitude
capture operates normally,
b) Enroute operations, i.e. RVSM, do not require
its use,
c) Aircraft does not depart from a designated
airport (as listed in the operators MEL) where
repair or replacement can be made, and
d) Repairs are made within three flight days.

1) Aural Alert

2) Visual Alert

Attitude Heading
Reference System
(AHRS) Fans

May be inoperative provided:

a) Visual alert operates normally, and
b) Auto-pilot with altitude hold and altitude
capture operates normally.
May be inoperative provided:
a) Aural alert operates normally, and
b) Auto-pilot with altitude hold and altitude
capture operates normally.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

23-01

Standby Attitude
Indicator
(600-2B19)

34-2

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION
Non-stabilized
Magnetic Compass
(Standby Compass)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

22-01

18

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) Any combination of two Gyro or INS (IRU)
Stabilized Compass Systems operate
normally, and
b) Operations are conducted with Dual
Independent Navigation Capability and under
Positive Radar Control by ATC on the enroute
portion of the flight.

(O) May be inoperative for flights that are entirely

within areas of magnetic unreliability provided at least
two Stabilized Directional Gyro Systems are installed,
operate and used in conjunction with approved Free
Gyro Navigation Techniques.

May be inoperative provided:

a) Operations are conducted in day VMC only,
b) Operations are not conducted into known or
forecast over-the-top conditions, and
c) Source selector is selected to NORMAL with
each side fed from its on-side AHRS/IRS.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
34-3

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION
25-01

18

4.

REMARKS OR EXCEPTIONS

Source Select Panel

Switches
1) ATTD/HDG,
DSPL CONT

Both may be inoperative provided:

a) PFD/MFD are not selected to a common
source,
b) Standby Attitude Indicator/ISI Attitude function
is operative, and
c) Standby Magnetic Compass Indicator is
operative.

2) AIR DATA

Except where enroute operations require its use, may

be inoperative.

30-01

Microwave Landing
System (MLS)
Receiver
(600-2B19)

As required by regulations.

32-01

Head-up Guidance
System
***

(M) May be inoperative provided approach procedures

are not dependent on its use.

41-01

Weather Radar
System

As required by regulations.

41-02

Weather Radar
Control Panels

As required by regulations.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

PAGE:

07/09/2012

34-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION
42-01

18

4.

REMARKS OR EXCEPTIONS

Ground Proximity
Warning System

(O) May be inoperative provided:

a) Alternate Procedures are established and
used, and
b) Repairs are made within two flight days.

1) Modes 1 4
(Terrain
Avoidance)

(O) May be inoperative provided:

a) Alternate procedures are established and
used, and
b) Repairs are made within two flight days.

2) Test Mode

May be inoperative provided:

a) GPWS is considered inoperative, and
b) Repairs are made within two flight days.

3) Glideslope
Deviation
(Mode 5)

4) Advisory
Callouts
(Mode 6)

(O) May be inoperative provided alternate procedures

are established and used.

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
34-5

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION
42-01

18

4.

REMARKS OR EXCEPTIONS

Ground Proximity
Warning System
(cont'd)
5) Windshear
Mode (Mode 7)
a) 600-2B19
(a/c without

(M)(O) May be inoperative provided:

a) Alternate procedures are established and
used,
b) Flap position transmitters are verified
operative, and
c) Takeoffs and landings are not conducted in
known or forecast windshear conditions.

(O) May be inoperative provided:

a) Alternate procedures are established and
used, and
b) Takeoffs and landings are not conducted in
known or forecast windshear conditions.

ModSum
TC601R15984
and without
ModSum
TC601R17138)

b) 600-2B19
(a/c with
ModSum
TC601R15984
or
TC601R17138)

600-2C10,
600-2D15,
600-2D24,
600-2E25

6) TAWS
(EGPWS)
***

42-02

GRND PROX
TERRAIN Switch
Guard
***

42-03

GRND PROX FLAP

Switch Guard
***

May be inoperative provided the switch is verified

pressed out or not illuminated prior to each departure
and approach.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

34-6

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION
Traffic Alert and
Collision Avoidance
System (TCAS II)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

43-01

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) System is deactivated and secured, and
b) Enroute or approach procedures do not require
its use.

(M)(O) May be inoperative provided:

a) Not required by regulations,
b) System is deactivated and secured, and
c) Enroute or approach procedures do not require
its use.

1) Combined
Traffic Alert (TA)
and Resolution
Advisory (RA)
Dual Display
Systems(s)

May be inoperative on the non-flying pilot side

provided:
a) TA and RA visual display is operative on the
flying pilot side, and
b) TA and RA audio function is operative on flying
pilot side.

2) Resolution
Advisory (RA)
Display
System(s)

May be inoperative on non-flying pilot side.

(O) May be inoperative provided:

a) Traffic Alert (TA) visual display and audio
functions are operative,
b) TA only mode is selected by the crew, and
c) Enroute or approach procedures do not require
its use.

(O) May be inoperative provided:

a) RA visual display and audio functions are
operative, and
b) Enroute or approach procedures do not require
its use.

3) Traffic Alert
(TA) Display
System(s)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

REMARKS OR EXCEPTIONS

Radio Altimeter
1) 600-2B19

(M) May be inoperative provided approach minimums

are not dependent on its use.

2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M) May be inoperative provided:

a) Approach minimums are not dependent on its
use, and
b) Spoiler/Stabilizer Subsystem of SSCS is
considered inoperative.
NOTE:

45-01

34-7

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION

44-02

07/09/2012

PAGE:

NUMBER INSTALLED
3.

44-01

18

SPLR/STAB FAULT status message will

be displayed on EICAS.

Radio Altimeter Test

Switches
1) Single Radio
Altimeter
Installation

One may be inoperative provided RAD ALT test

function on the operative side is performed prior to
each flight.

2) Dual Radio
Altimeter
Installation
***

One may be inoperative provided:

a) RAD ALT test function on the operative side is
performed prior to each flight, and
b) Associated Radio Altimeter with the operative
test switch is operative.

IRS Fan
***
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
34-8

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION
50-01

18

4.

REMARKS OR EXCEPTIONS

Long Range
Navigation Systems
1) INS/IRS
(Navigation
Function only)

(O) May be inoperative provided:

a) Procedures do not require its use,
b) Affected IRS Navigation Function is disabled
through FMS, and
c) For any IRS is in ATT mode, the associated
Flight Director Modes are considered
inoperative.

2) LORAN, GPS,
etc.

As required by regulations.

51-01

Marker Beacon
Systems

May be inoperative provided approach procedures do

not require its use.

51-02

VHF Navigation
Systems
(VOR/ILS)

As required by regulations.

52-01

Automatic Direction
Finding (ADF)
System

As required by regulations.

53-01

Distance Measuring
Equipment Systems
(DME)

As required by regulations.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

61-01

61-02

34-9

NUMBER REQUIRED FOR DISPATCH

34 NAVIGATION
ATC Transponders
and Automatic
Altitude Reporting
Systems

07/09/2012

PAGE:

NUMBER INSTALLED
3.

54-01

18

4.

REMARKS OR EXCEPTIONS

May be inoperative provided:

a) Enroute operations do not require its use, and
b) Prior to flight, approval is obtained from ATC
facilities having jurisdiction over the planned
route of flight.

Any in excess of those required by regulations may be

inoperative.

1) Elementary and
Enhanced
Downlink
Aircraft
Reportable
Parameters not
required by
regulations

May be inoperative provided:

a) Enroute operations do not require its use, and
b) Repairs are made prior to completion of the
next heavy maintenance visit.

Flight Management
Systems
(600-2B19,
600-2C10,
600-2D15,
600-2D24
***),
(600-2E25)

(O) Except where enroute operations require its use,

all may be inoperative provided:
a) Alternate procedures are established and
used,
b) Alternate means for initializing IRS is available
for IRS equipped aircraft, and
c) Both RTUs are operative.

1) Navigation
Databases

FMS/MDC Data
Loader
***

(O) May be out of currency provided:

a) Current Aeronautical Charts are used to verify
Navigation Fixes prior to dispatch,
b) Procedures are established and used to verify
status and suitability of Navigation Facilities
used to define route of flight, and
c) Approach Navigation Radios are manually
tuned and identified.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

34 NAVIGATION

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
34-10

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18

PAGE:

07/09/2012

35-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

35 OXYGEN

4.

REMARKS OR EXCEPTIONS

10-01

Observers Oxygen
System

May be inoperative provided:

a) Observers Seat is considered inoperative, and
b) Repairs are made within two flight days.

10-02

OXY LO PRESS
Caution Message

(O) May be displayed provided:

a) Oxygen pressure is checked to be above
minimum required oxygen pressure before
each flight,
b) EICAS Crew Oxygen Pressure Readout is
operative,
c) Crew oxygen pressure is monitored during
flight, and
d) Repairs are made within one flight day.

11-02

Oxygen Pressure
Switch
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M) May be inoperative provided:

a) Oxygen cylinder pre-charged pressure is
checked prior to each flight,
b) Oxygen cylinder control valve is verified OPEN
prior to each flight, and
c) Pilot and Copilot Masks are verified operative
prior to each flight.

12-01

Flight Crew Oxygen

Pressure Indications
1) EICAS Readout

(M)(O) May be inoperative provided Ground Service

Panel Pressure Gauge or Bottle Pressure Gauge is
operative and checked prior to each flight.

May be inoperative provided EICAS Readout is

operative and checked prior to each flight.

(M) May be inoperative provided Bottle Pressure

Gauge is operative and checked prior to each flight.

3) Bottle Pressure
Gauge

High Pressure
Discharge Indicator

2) Ground Service
Panel Pressure
Gauge

12-02

(O) May be damaged or missing provided:

a) At least two pressure indications are verified
operative after failure occurrence, and
b) Crew oxygen bottle pressure is checked within
limits before each flight.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

20-02

35-2

NUMBER REQUIRED FOR DISPATCH

35 OXYGEN
Passenger Oxygen
System

07/09/2012

PAGE:

NUMBER INSTALLED
3.

20-01

18

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) All components of cabin pressurization warning
and indicating systems are operative,
b) Operations are conducted so that minimum
enroute altitude is at or below 14,000 feet
MSL,
c) Operations are conducted at or below FL 250,
d) Portable oxygen units are provided for all crew
members and for 10 percent of the passengers
for half an hour (supplemental oxygen),
e) Operational procedures are established to
ensure that passengers are appropriately
briefed to accommodate revised equipment,
and
f) Both Air Conditioning Packs are verified
operative.

May be inoperative provided flight is conducted at or

below 10,000 feet MSL.

1) Automatic
Deployment

(M) May be inoperative provided:

a) Manual deployment is operative, and
b) Operations are conducted at or below FL 300.

2) Passenger
Service Units
(PSU)

(M)(O) Individual PSUs may be inoperative with no

flight altitude restriction provided:
a) Associated seats are blocked and placarded to
prevent occupancy,
b) PSUs for flight attendant locations operate
normally, and
c) If two or more inoperative PSUs are adjacent
(forward and aft, left and right), seat rows
forward and aft of the inoperative PSUs are
blocked and placarded to prevent occupancy.

Passenger Oxygen
(Masks Deployed)
"ON" Light

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|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

35-3

NUMBER REQUIRED FOR DISPATCH

35 OXYGEN
Lavatory Passenger
Oxygen System

PAGE:

NUMBER INSTALLED
3.

20-03

18

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) Lavatory is not used for any purpose, and
b) Lavatory door is locked and placarded
"INOPERATIVE DO NOT ENTER"

(O) May be inoperative provided flight is conducted at

or below FL250.
NOTE:

These provisos are not intended to preclude

lavatory inspections by a crew member.

31-01

Portable Oxygen
Dispensing Units

Any in excess of those required by regulations may be

inoperative provided:
a) Inoperative unit is removed from passenger
cabin, and
b) Required distribution is maintained.

31-02

Protective Breathing
Equipment

Any in excess of those required by regulations may be

inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

35 OXYGEN

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
35-4

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

36-1

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
Pressure Regulating
SOV (PRSOV)
1) 600-2C10

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-02

18

4.

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative provided:

a) Associated PRSOV is secured CLOSED,
b) Opposite HPV is operative,
c) Opposite Engine Cowl Anti- Ice SOV is
operative,
d) APU is operative,
e) APU Load Control Valve is operative,
f) Operations are conducted at or below FL 310,
g) Operations are not conducted in known or
forecast icing conditions, and
h) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

2) 600-2D15,
600-2D24

(M)(O) May be inoperative provided:

a) Associated PRSOV is secured CLOSED,
b) Opposite HPV is operative,
c) Opposite Engine Cowl Anti- Ice SOV is
operative,
d) APU is operative,
e) APU Load Control Valve is operative,
f) Operations are conducted at or below FL 250,
g) Operations are not conducted in known or
forecast icing conditions, and
h) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

3) 600-2E25

(M)(O) May be inoperative provided:

a) Associated PRSOV is secured CLOSED,
b) Opposite HPV is operative,
c) Opposite Engine Cowl Anti-Ice SOV is
operative,
d) Operations are conducted at or below FL 250,
e) Ground operation for Air Conditioning is
conducted using APU bleed,
f) Operations are not conducted in known or
forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplements (Operations with Airplane
Systems Inoperative).

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U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
36-2

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
11-03

18

4.

REMARKS OR EXCEPTIONS

High Pressure Valve

(HPV)
1) 600-2C10

(M)(O) May be inoperative provided:

a) Associated HPV is secured CLOSED,
b) Opposite Engine Cowl Anti- Ice SOV is
operative,
c) APU is operative,
d) APU Load Control Valve is operative,
e) Operations are conducted at or below FL310,
f) Operations are not conducted in known or
forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

2) 600-2D15,
600-2D24

(M)(O) May be inoperative provided:

a) Associated HPV is secured CLOSED,
b) Opposite Engine Cowl Anti- Ice SOV is
operative,
c) APU is operative,
d) APU Load Control Valve is operative,
e) Operations are conducted at or below FL 250,
f) Operations are not conducted in known or
forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

3) 600-2E25

(M)(O) May be inoperative provided:

a) Associated HPV is secured CLOSED,
b) Opposite Engine Cowl Anti-Ice SOV is
operative,
c) Operations are conducted at or below FL 250,
d) Ground operation for Air Conditioning is
conducted using APU bleed,
e) Operations are not conducted in known or
forecast icing conditions, and
f) Operations are conducted in accordance with
AFM Supplements (Operations with Airplane
Systems Inoperative).

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U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
36-3

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
11-04

18

4.

REMARKS OR EXCEPTIONS

Pack Inlet Pressure

Sensors
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

12-01

Bleed Air L/R 14th

Stage SOVs
(600-2B19)

(M) One may be inoperative provided:

a) Affected valve is secured CLOSED,
b) Both Ice Detection Systems are operative,
c) Associated Thrust Reverser is deactivated,
stowed, and LOCKED in forward thrust
position,
d) Operations are not conducted in known or
forecast icing conditions, and
e) Operations are conducted in accordance with
AFM performance data for one Thrust
Reverser inoperative.

12-02

Bleed Air ISOL

Valve (Cross-Bleed
Valve)
C

(M)(O) May be inoperative OPEN provided:

a) ISOL valve is secured OPEN,
b) Bleed source selector switch is selected either
to L ENG or R ENG,
c) Bleed valves selector switch is selected to
MANUAL,
d) PRSOV and HPV on selected side are
operative,
e) Operations are conducted at or below FL310,
f) Operations are not conducted in known or
forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

1) 600-2C10

0
|

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

3) 600-2E25

36-4

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
Bleed Air ISOL
Valve (Cross-Bleed
Valve)
(contd)
2) 600-2D15,
600-2D24

07/09/2012

PAGE:

NUMBER INSTALLED
3.

12-02

18

4.

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative OPEN provided:

a) ISOL valve is secured OPEN,
b) Bleed source selector switch is selected either
to L ENG or R ENG,
c) Bleed valves selector switch is selected to
MANUAL,
d) PRSOV and HPV on selected side are
operative,
e) Operations are conducted at or below FL 250,
f) Operations are not conducted in known or
forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).

(M)(O) May be inoperative OPEN provided:

a) ISOL valve is secured OPEN,
b) Bleed valves selector switch is selected to
MANUAL,
c) PRSOV and HPV on selected side are
operative,
d) Operations are conducted at or below FL 250,
e) Ground operation for Air Conditioning is
conducted using APU,
f) Operations are not conducted in known or
forecast icing conditions, and
g) Operations are conducted in accordance with
AFM Supplements (Operations with Airplane
Systems Inoperative).

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|
|
|
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|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

36-5

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC

21-02

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-01

18

4.

REMARKS OR EXCEPTIONS

Bleed Air Leak

Detection System
(600-2B19)
1) 10th Stage
Sensing Loops
(A & B)

(O) Either loop A or B may be inoperative provided

neither loop is failed OPEN.

2) 14th Stage
Sensing Loops

(M) May be inoperative provided affected Bleed Air

14th Stage SOV is considered inoperative.

3) Anti-Ice Sensing
Loop

(M) May be inoperative provided:

a) Wing ANTI-ICE switch is selected OFF,
b) Both Ice Detection Systems are operative,
and
c) Operations are not conducted in known or
forecast icing conditions.

BLEED AIR 14th

Stage "L/R DUCT
FAIL/CLOSED"
Switch Lights
(light function only)
(600-2B19)

21-03

RESERVED

21-04

BLEED AIR 10th

Stage "DUCT
FAIL/CLOSED"
Switch Lights
(light function only)
(600-2B19)

21-05

BLEED AIR 10th

Stage ISOL "OPEN"
Switch Light
(light function only)
(600-2B19)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
36-6

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
21-06

18

4.

REMARKS OR EXCEPTIONS

Air Leak Detection

System
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

1) Anti-Ice Loops

Both Loops (A and B) may be inoperative provided:

a) Wing ANTI-ICE switch is selected OFF, and
b) Operations are not conducted in known or
forecast icing conditions.

a) Left

Both Loops (A and B) may be inoperative provided:

a) At least one Right Cowl Loop is operative,
b) Right Cowl Anti-Ice SOV is operative,
c) Right PRSOV is operative,
d) Right HPV is operative,
e) Left cowl ANTI-ICE switch is selected OFF,
and
f) Operations are not conducted in known or
forecast icing conditions.

b) Right

Both Loops (A and B) may be inoperative provided:

a) At least one Left Cowl Loop is operative,
b) Left Cowl Anti-Ice SOV is operative,
c) Left PRSOV is operative,
d) Left HPV is operative,
e) Right cowl ANTI-ICE switch is selected OFF,
and
f) Operations are not conducted in known or
forecast icing conditions.

System redundancy may be degraded as indicated by

DUCT MON FAULT status message.

2) Cowl Loops

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

36-7

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
Air Leak Detection
System
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
(contd)
3) Bleed Loops
(contd)
a) Left
(600-2C10)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-06

18

4.

REMARKS OR EXCEPTIONS

(O) Both loops (A and B) may be inoperative provided:

a) At least one Right Bleed Loop (A or B) is
operative,
b) Right PRSOV is operative,
c) Right HPV is operative,
d) Right Air Conditioning Pack is operative,
e) Bleed source selector switch is selected to the
R ENG,
f) Bleed Air ISOL Valve is operative and selected
CLOSED,
g) Bleed valves selector switch is selected to
MANUAL,
h) APU is operative,
i) APU Load Control Valve is operative,
j) Cross bleed start procedure is not used for
engine start,
k) Operations are conducted at or below FL 310,
l) Operations are not conducted in known or
forecast icing conditions, and
m) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

36-8

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
Air Leak Detection
System
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
(contd)
3) Bleed Loops
(contd)
b) Left
(600-2D15,
600-2D24)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-06

18

4.

REMARKS OR EXCEPTIONS

(O) Both loops (A and B) may be inoperative provided:

a) At least one Right Bleed Loop (A or B) is
operative,
b) Right PRSOV is operative,
c) Right HPV is operative,
d) Right Air Conditioning Pack is operative,
e) Bleed source selector switch is selected to the
R ENG,
f) Bleed Air ISOL Valve is operative and selected
CLOSED,
g) Bleed valves selector switch is selected to
MANUAL,
h) APU is operative,
i) APU Load Control Valve is operative,
j) Cross bleed start procedure is not used for
engine start,
k) Operations are conducted at or below FL 250,
l) Operations are not conducted in known or
forecast icing conditions, and
m) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

36-9

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
Air Leak Detection
System
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
(contd)
3) Bleed Loops
(contd)
c) Left
(600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-06

18

4.

REMARKS OR EXCEPTIONS

(O) Both loops (A and B) may be inoperative provided:

a) At least one Right Bleed Loop (A or B) is
operative,
b) Both PRSOV are operative,
c) Both HPV are operative,
d) Both Engine Cowl Anti-Ice SOV are operative,
e) Right Air Conditioning Pack is operative,
f) Operations are conducted at or below FL 250,
g) Ground operation for Right Air Conditioning
Pack is conducted using engine bleed,
h) Operations are not conducted in known or
forecast icing conditions, and
i) Operations are conducted in accordance with
AFM Supplements (Operations with Airplane
Systems Inoperative) and (Air Conditioning
Single Pack Operation).
(contd)

|
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|
|
|
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|
|
|
|
|
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|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

36-10

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
Air Leak Detection
System
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
(contd)
3) Bleed Loops
(contd)
d) Right
(600-2C10)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-06

18

4.

REMARKS OR EXCEPTIONS

(O) Both loops (A and B) may be inoperative provided:

a) At least one Left Bleed Loop (A or B) is
operative,
b) Left PRSOV is operative,
c) Left HPV is operative,
d) Left Air Conditioning Pack is operative,
e) Bleed source selector switch is selected to the
L ENG,
f) Bleed Air ISOL Valve is operative and selected
CLOSED,
g) Bleed valves selector switch is selected to
MANUAL,
h) APU is operative,
i) APU Load Control Valve is operative,
j) Cross bleed start procedure is not used for
engine start,
k) Operations are conducted at or below FL 310,
l) Operations are not conducted in known or
forecast icing conditions, and
m) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

36-11

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
Air Leak Detection
System
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
(contd)
3) Bleed Loops
(contd)
e) Right
(600-2D15,
600-2D24)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-06

18

4.

REMARKS OR EXCEPTIONS

(O) Both loops (A and B) may be inoperative provided:

a) At least one Left Bleed Loop (A or B) is
operative,
b) Left PRSOV is operative,
c) Left HPV is operative,
d) Left Air Conditioning Pack is operative,
e) Bleed source selector switch is selected to the
L ENG,
f) Bleed Air ISOL Valve is operative and selected
CLOSED,
g) Bleed valves selector switch is selected to
MANUAL,
h) APU is operative,
i) APU Load Control Valve is operative,
j) Cross bleed start procedure is not used for
engine start,
k) Operations are conducted at or below FL 250,
l) Operations are not conducted in known or
forecast icing conditions, and
m) Operations are conducted in accordance with
AFM Supplement (Operations with Airplane
Systems Inoperative).
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

36-12

NUMBER REQUIRED FOR DISPATCH

36 PNEUMATIC
Air Leak Detection
System
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
(contd)
3) Bleed Loops
(contd)
f) Right
(600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

21-06

18

4.

REMARKS OR EXCEPTIONS

(O) Both loops (A and B) may be inoperative provided:

a) At least one Left Bleed Loop (A or B) is
operative,
b) Both PRSOV are operative,
c) Both HPV are operative,
d) Both Engine Cowl Anti-Ice SOV are operative,
e) Left Air Conditioning Pack is operative,
f) Operations are conducted at or below FL 250,
g) Ground operation for Left Air Conditioning
Pack is conducted using APU or engine bleed,
h) Operations are not conducted in known or
forecast icing conditions, and
i) Operations are conducted in accordance with
AFM Supplements (Operations with Airplane
Systems Inoperative) and (Air Conditioning
Single Pack Operation).

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|
|
|
|
|
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|
|
|
|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
C

38-1

REMARKS OR EXCEPTIONS

(M) Individual components may be inoperative

provided:
a) Associated components are deactivated or
isolated, and
b) Associated system components are verified
not to have leaks.
NOTE:

07/09/2012

NUMBER REQUIRED FOR DISPATCH

38 WATER/WASTE
Potable Water
Systems

PAGE:

NUMBER INSTALLED
3.

10-01

18

Any portion of system which operates

normally may be used.

(M) May be inoperative provided:

a) System is drained, and
b) Procedures are established to ensure that
system is not serviced.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

38-2

NUMBER REQUIRED FOR DISPATCH

38 WATER/WASTE

4.

REMARKS OR EXCEPTIONS

Lavatory Waste
System
C

(M) Individual components may be inoperative

provided:
a) Associated components are deactivated or
isolated, and
b) Associated system components are verified
not to have leaks.
NOTE:

Lavatory Service
Indicator Lights

Any portion of system which operates

normally may be used.

(M) Associated lavatory system(s) may be inoperative

provided:
a) Associated components are deactivated or
isolated to prevent leaks,
b) Pilot-in-command will determine if flight
duration is acceptable with a forward lavatory
unusable, and
c) Associated lavatory door(s) is secured
CLOSED and placarded inoperative.
NOTE:

30-02

07/09/2012

PAGE:

NUMBER INSTALLED
3.

30-01

18

These provisos are not intended to prohibit

inspections by crewmembers.

May be inoperative provided alternate procedures are

established and used.
NOTE:

Waste tanks require a precharge of 8.7 L

(2.3 US gallons).

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18
07/09/2012

PAGE:
45-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

45 CENTRAL MAINTENANCE
COMPUTER

4.

REMARKS OR EXCEPTIONS

45-01

Maintenance
Diagnostic
Computer (MDC)

(M) May be inoperative provided alternate procedures

are established and used.

45-02

MAINT Switch
Guard

May be inoperative, broken or missing.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

45 CENTRAL MAINTENANCE
COMPUTER

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
45-2

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

2) Power
Connection

3) Mounting
Device

46-1

NUMBER REQUIRED FOR DISPATCH

46 INFORMATION SYSTEMS

Electronic Flight
Bag Systems
(EFBs)
(Class 2)
***
1) Data
Connectivity

07/09/2012

PAGE:

NUMBER INSTALLED
3.

20-01

18

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided alternative

procedures are established and used.

May be inoperative provided procedures do not require

its use.

(O) May be inoperative provided alternative

procedures are established and used.

May be inoperative provided procedures do not require

its use.

(M)(O) May be inoperative provided:

a) Associated EFB and hardware is secured by
an alternate means or removed from the
aircraft, and
b) Alternative procedures are established and
used.

(M) May be inoperative provided:

a) Associated EFB and hardware is secured by
an alternate means or removed from the
aircraft, and
b) Procedures do not require its use.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

46 INFORMATION SYSTEMS

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
46-2

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

(M) May be inoperative provided:

a) APU is deactivated,
b) Intake door is visually verified CLOSED, and
c) Both Integrated Drive Generators (IDG) are
operative.
NOTE:

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

(M) May be inoperative provided:

a) APU is deactivated,
b) Aircraft speed is limited to 300 knots, and
c) Both Integrated Drive Generators (IDG) are
operative.
NOTE:

2) 600-2C10,
600-2D15,
600-2D24

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) APU is deactivated,
b) Intake door is visually verified CLOSED, and
c) Both Integrated Drive Generators (IDG) are
operative.
NOTE:

49-1

NUMBER REQUIRED FOR DISPATCH

49 AIRBORNE AUXILIARY
POWER
Auxiliary Power Unit
(APU)
1) 600-2B19

07/09/2012

PAGE:

NUMBER INSTALLED
3.

10-01

18

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

(M) May be inoperative provided:

a) APU is deactivated,
b) Aircraft speed is limited to 220 knots, and
c) Both Integrated Drive Generators (IDG) are
operative.
NOTE:

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

49-2

NUMBER REQUIRED FOR DISPATCH

49 AIRBORNE AUXILIARY
POWER
Auxiliary Power Unit
(APU)
(contd)
3) 600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

10-01

18

REMARKS OR EXCEPTIONS

(M)(O) May be inoperative provided:

a) APU is deactivated,
b) Intake door is visually verified CLOSED,
c) Both Integrated Drive Generators (IDG) are
operative, and
d) Cabin occupants limited per table.

|
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|

NOTE:

|
|
|

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

(M)(O) May be inoperative provided:

a) APU is deactivated,
b) Aircraft speed is limited to 220 knots,
c) Both Integrated Drive Generators (IDG) are
operative, and
d) Cabin occupants limited per table.

|
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NOTE:

|
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IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

07/09/2012

49-3

NUMBER REQUIRED FOR DISPATCH

49 AIRBORNE AUXILIARY
POWER
APU Air Intake Door
Linear Actuator
1) 600-2B19

PAGE:

NUMBER INSTALLED
3.

14-01

18

REMARKS OR EXCEPTIONS

May be inoperative provided:

a) APU is not used,
b) Aircraft speed is limited to 300 knots, and
c) Both Integrated Drive Generators are
operative.
NOTE:

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

(M) May be inoperative provided:

a) Intake door is deactivated CLOSED and
b) APU is considered inoperative.

(M)(O) May be inoperative provided:

a) Intake door is deactivated OPEN,
b) APU is operated continuously during flight or
aircraft speed is limited to 300 knots if APU is
OFF,
c) AFM performance corrections for APU ON are
applied, and
d) APU Battery and APU Battery Charger System
is operative.
(contd)

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

REMARKS OR EXCEPTIONS

(O) May be inoperative provided:

a) APU is not used,
b) Aircraft speed is limited to 220 knots, and
c) Both Integrated Drive Generators (IDG) are
operative.
NOTE:

43-01

49-4

NUMBER REQUIRED FOR DISPATCH

49 AIRBORNE AUXILIARY
POWER
APU Air Intake Door
Linear Actuator
(contd)
2) 600-2C10,
600-2D15,
600-2D24,
600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

14-01

18

IDG is considered inoperative when either

the Generator/GCU System or the CSD
System is inoperative.

(M)(O) May be inoperative provided:

a) Intake door is deactivated OPEN,
b) APU is operated continuously during flight or
aircraft speed is limited to 220 knots if APU is
OFF, and
c) AFM performance corrections for APU ON are
applied.

3) 600-2C10,
600-2D15,
600-2D24

(M) May be inoperative provided:

a) Intake door is deactivated CLOSED, and
b) APU is considered inoperative.

4) 600-2E25

(M)(O) May be inoperative provided:

a) Intake door is deactivated CLOSED, and
b) APU is considered inoperative.

|
|
|

APU START/STOP
"START/AVAIL"
Switch Light
(light function only)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

49-5

NUMBER REQUIRED FOR DISPATCH

49 AIRBORNE AUXILIARY
POWER

4.

REMARKS OR EXCEPTIONS

APU Load Control

Valve (LCV)
1) 600-2B19

(M) May be inoperative provided it is secured

CLOSED.
NOTE:

2) 600-2C10,
600-2D15,
600-2D24

3) 600-2E25

APU Surge Control

Valve
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

51-03

APU LCV
"FAIL/OPEN"
Switch Light
(light function only)
(600-2B19)

61-01

Electronic Control
Unit (ECU)

APU is available as source of electrical

power only, if required.

(M) May be inoperative provided:

a) APU LCV is secured CLOSED, and
b) Bleed Valves are selected to "Manual" on the
Bleed Air Control Panel.
NOTE:

51-02

PAGE:

NUMBER INSTALLED
3.

51-01

18

APU is available as a source of electrical

power only, if required.

(M)(O) May be inoperative provided:

a) APU LCV is secured CLOSED, and
b) Bleed Valves are selected to "Manual" on the
Bleed Air Control Panel.

|
|
|
|

NOTE:

|
|

APU is available as a source of electrical

power only, if required.

May be inoperative CLOSED provided:

a) APU is not operated above 17,000 feet, and
b) Operations are not dependent on use of APU.
|

May be inoperative provided APU is considered

inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
49-6

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

49 AIRBORNE AUXILIARY
POWER
61-02

18

4.

REMARKS OR EXCEPTIONS

APU Sub-system
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

1) EGT Sensors

One may be inoperative provided:

a) APU is operative (start and shutdown
normally), and
b) Operations are not dependent on use of APU.

2) Speed Sensors

One may be inoperative provided:

a) APU is operative (start and shutdown
normally), and
b) Operations are not dependent on use of APU.

3) Fuel Filter Delta

Pressure Switch

May be inoperative provided:

a) APU is operative (start and shutdown
normally), and
b) Operations are not dependent on use of APU.

4) APU Oil Filter

Delta Pressure
Switch

May be inoperative provided:

a) APU is operative (start and shutdown
normally), and
b) Operations are not dependent on use of APU.

5) Generator Oil
Filter Bypass
Indicator

May be inoperative provided:

a) APU is operative (start and shutdown
normally), and
b) Operations are not dependent on use of APU.

6) Oil Temperature
Sensor

May be inoperative provided:

a) APU is operative (start and shutdown
normally), and
b) Operations are not dependent on use of APU.

7) Time Totalizing
Meter

(O) May be inoperative provided alternate procedures

are established and used.

|
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

52-1

NUMBER REQUIRED FOR DISPATCH

52 DOORS
Passenger Door
Assist System
1) Power Assist
Sub-system
(Motor,
Control Switch,
Cables, Pulleys,
Fitting)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-01

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided:

a) Door is verified manually operative (opens and
closes) without any interference, and
b) Alternate procedures are established and
used.

|
|
|
|
|
|

2) Counterbalance
Sub-system
(Gas Springs,
Cables, Pulleys,
Fittings)

(O) May be inoperative provided:

a) Door is verified manually operative (opens and
closes) without any interference, and
b) Alternate procedures are established and
used.

|
|
|
|
|

Passenger Door
Handrail QuickRelease Pins
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

(M) May be missing provided the associated cable is

stowed.

11-06

Passenger Door
Support Wheel
Assembly

(M)(O) May be inoperative or missing provided:

a) Support Wheel Assembly is deactivated,
b) Alternate procedures to support door with cable
kit are established and used, and
c) Placarded stairway loading limitations are
maintained.

21-01

Doors and Overwing

Emergency Exits

(O) One overwing emergency exit or one door may be

inoperative provided:
a) No passengers are carried except aircraft
crew,
b) Affected door or emergency exit is verified
CLOSED, LATCHED, and LOCKED before
each departure, and
c) Repairs are made within three flight days.

11-05

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

2) Aft Cargo
Compartment
Door
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
35-01

4.

REMARKS OR EXCEPTIONS

May be inoperative provided door is verified operative

(opens and closes) without interference.
NOTE:

52-2

NUMBER REQUIRED FOR DISPATCH

52 DOORS
Balance Springs
1) Cargo
Compartment
Door
(600-2B19)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

31-01

18

Door may close faster.

May be inoperative provided door is verified operative

(opens and closes) without any interference.
NOTE:

Door may close faster.

|

Forward Cargo
Compartment
Protector Kits
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
1) A/c without
ModSum
LE670T11781
(Door Protector
Kit)

|
D

(M) May be inoperative provided:

a) Affected protector kit is removed,
b) Associated cargo compartment door is visually
inspected for damage and checked for correct
operation, and
c) Associated cargo compartment or subcompartment remains empty.

(M) May be inoperative provided:

a) Affected protector kit is removed,
b) Associated cargo compartment door is visually
inspected for damage and checked for correct
operation, and
c) Associated Cargo Compartment Door
Restraint Nets are verified operative and
properly installed after every cargo/baggage
loading.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

52-3

NUMBER REQUIRED FOR DISPATCH

52 DOORS
Forward Cargo
Compartment
Protector Kits
(600-2C10,
600-2D15,
600-2D24,
600-2E25)
(contd)
2) A/c with
ModSum
LE670T11781
(Vent Flap
Protector Kit)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

35-01

18

4.

REMARKS OR EXCEPTIONS

|
D

(M) May be inoperative provided:

a) Affected protector kit is removed,
b) Associated vent flap mechanism is visually
inspected for damage and checked for correct
operation, and
c) Associated cargo compartment or subcompartment remains empty.

(M) May be inoperative provided:

a) Affected protector kit is removed,
b) Associated vent flap mechanism is visually
inspected for damage and checked for correct
operation, and
c) Associated Cargo Compartment Door
Restraint Nets are verified operative and
properly installed after every cargo/baggage
loading.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
52-4

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

52 DOORS
51-01

18

4.

REMARKS OR EXCEPTIONS

Flight Deck Security

Door
(FAR 25.795
Compliant)
1) Door Latch

May be inoperative provided:

a) Door Dead Bolt is operative,
b) Door Dead Bolt is used to lock and unlock the
door, and
c) Repairs are made within two flight days.

2) Flight Deck
Door Panel
Pressure Relief
Latches

May be inoperative in the latched position provided

repairs are made within two flight days.

3) Dead Bolt

May be inoperative provided repairs are made within

two flight days.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
52-5

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

52 DOORS
70-01

18

4.

REMARKS OR EXCEPTIONS

Passenger Door
Indication System
1) 600-2B19
without
ModSum
TC601R13193
(Phase IV Door)

(O) May be inoperative provided before each flight:

a) Door is CLOSED, LATCHED and LOCKED,
b) Internal green witness marks on six door latch
pins are aligned,
c) Green witness marks on two upper roll latches
are aligned,
d) Door lock flag indicator indicates LOCKED,
e) Inner knob is verified STOWED,
f) External handle is verified STOWED,
g) External pressure vent flap is verified fully
CLOSED,
h) No door warning EICAS messages are
displayed, and
i) Repairs are made within three flight days.

2) 600-2B19 with
ModSum
TC601R13193
(Phase IV Door)

(O) May be inoperative provided before each flight:

a) Door is CLOSED, LATCHED and LOCKED,
b) Internal green witness marks on four door latch
pins are aligned,
c) Green witness marks on two upper roll latches
are aligned,
d) Green witness mark on upper lock on upper
roll shaft is aligned,
e) Door lock flag indicator indicates LOCKED,
f) External handle is verified STOWED,
g) External pressure vent flap is verified fully
CLOSED,
h) No door warning EICAS messages are
displayed, and
i) Repairs are made within three flight days.
(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

52-6

NUMBER REQUIRED FOR DISPATCH

52 DOORS
Passenger Door
Indication System
(contd)
3) 600-2C10,
600-2D15,
600-2D24,
600-2E25

07/09/2012

PAGE:

NUMBER INSTALLED
3.

70-01

18

REMARKS OR EXCEPTIONS

(O) May be inoperative provided before each flight:

a) Door is CLOSED, LATCHED and LOCKED,
b) Internal green witness marks on four door latch
pins are aligned,
c) Green witness marks on two upper roll latches
are aligned,
d) Green witness mark on upper lock on upper
roll shaft is aligned,
e) Door lock flag indicator indicates LOCKED,
f) External handle is verified STOWED,
g) External pressure vent flap is verified fully
CLOSED,
h) No door warning EICAS messages are
displayed,
i) Ground Valve (Avionics Cooling) is considered
inoperative, and
j) Repairs are made within three flight days.

70-02

Avionic
Compartment Door
Indication System

May be inoperative provided before each flight:

a) Door is CLOSED, LATCHED and LOCKED,
and
b) Handle is verified STOWED.

70-03

Overwing
Emergency Exit
Indication Systems

(O) May be inoperative provided before each flight:

a) Affected door is CLOSED, LATCHED and
LOCKED, and
b) External push plate is verified FLUSH.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

2) CTR
(600-2D15,
600-2D24
with modsum
670T31862),
(600-2E25)

3) AFT

52-7

NUMBER REQUIRED FOR DISPATCH

52 DOORS
Cargo Compartment
Door Indication
System
1) FWD
(600-2C10,
600-2D15,
600-2D24
with modsum
670T31862),
(600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

70-04

18

REMARKS OR EXCEPTIONS

May be inoperative provided before each flight:

a) Door is verified CLOSED, LATCHED and
LOCKED,
b) Handle is verified STOWED,
c) External pressure vent flap is verified
CLOSED, and
d) Gap between door and fuselage is verified not
present.
May be inoperative provided before each flight:
a) Door is verified CLOSED, LATCHED and
LOCKED,
b) Handle is verified STOWED,
c) External pressure vent flap is verified
CLOSED, and
d) Gap between door and fuselage is verified not
present.
May be inoperative provided before each flight:
a) Door is verified CLOSED, LATCHED and
LOCKED, and
b) Handle is verified STOWED.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
52-8

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

52 DOORS
70-05

18

4.

REMARKS OR EXCEPTIONS

Service Door
Indication System
1) 600-2B19

May be inoperative provided before each flight:

a) Door is CLOSED, LATCHED and LOCKED,
b) Internal green witness marks are aligned at
viewing window,
c) Internal handle is verified at LOCKED position,
and
d) External handle is verified STOWED.

2) 600-2C10

May be inoperative provided before each flight:

a) Door is CLOSED, LATCHED and LOCKED,
b) Handle is verified STOWED,
c) External pressure vent flap is verified
CLOSED, and
d) Ground Valve (Avionics Cooling) is considered
inoperative.

3) 600-2D15,
600-2D24,
600-2E25

a) FWD

May be inoperative provided before each flight:

a) Door is CLOSED, LATCHED and LOCKED,
b) Handle is verified STOWED,
c) External pressure vent flap is verified
CLOSED, and
d) Ground Valve (Avionics Cooling) is considered
inoperative.

b) AFT
***

May be inoperative provided before each flight:

a) Door is CLOSED, LATCHED and LOCKED,
b) Handle is verified STOWED,
c) External pressure vent flap is verified
CLOSED, and
d) Ground Valve (Avionics Cooling) is considered
inoperative.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
73-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

73 ENGINE FUEL & CONTROL

21-01

18

4.

REMARKS OR EXCEPTIONS

Full Authority Digital

Engine Control
System
(FADEC)
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

|
A

System redundancy may be degraded as indicated by

L FADEC FAULT 1 status message provided:
a) R FADEC FAULT 1 status message is not
displayed, and
b) Repairs are made within 10 days.

System redundancy may be degraded as indicated by

R FADEC FAULT 1 status message provided:
a) L FADEC FAULT 1 status message is not
displayed, and
b) Repairs are made within 10 days.

(M) System redundancy may be degraded as indicated

by L FADEC FAULT 1 and R FADEC FAULT 1
status messages provided:
a) Not-dispatchable FADEC failures are verified
not present on both engines, and
b) Repairs are made within 10 days.

System redundancy may be degraded as indicated by

L FADEC FAULT 2 status message provided repairs
are made within 30 days.

System redundancy may be degraded as indicated by

R FADEC FAULT 2 status message provided repairs
are made within 30 days.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

18

PAGE:

07/09/2012

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

73 ENGINE FUEL & CONTROL

4.

REMARKS OR EXCEPTIONS

31-01

EICAS Fuel Flow

"FF" Readouts
(600-2B19)

May be inoperative provided all EICAS Fuel Tank

Quantity Readouts are operative.

31-02

EICAS Fuel Used

Readout
(600-2B19)

May be inoperative provided all EICAS Fuel Tank

Quantity Readouts are operative.

31-03

Fuel Low Pressure

Indicating Systems
(600-2B19)

(O) One may be inoperative provided:

a) Both Fuel Boost Pumps are operative, and
b) Repairs are made within ten days.
NOTE:

31-04

Fuel Feed
Temperature
Indicating System

73-2

Fuel system check valve test (First flight of

day - Before Engine Shutdown) is waived for
the inoperative fuel low pressure indication.

One may be inoperative provided icing inhibitor is

added to the fuel.

May be inoperative provided EICAS oil temperature

readout is checked to be stable within limits prior to
each flight.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
74-1

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

74 IGNITION
11-01

18

4.

REMARKS OR EXCEPTIONS

Ignition Systems
1) 600-2B19
a) A Systems

One may be inoperative provided both B Systems are

operative.

b) B Systems

Both may be inoperative provided both A Systems are

operative.
NOTE:

Although the Continuous Ignition System

remains operative, the CONT IGNITION
status message and CONT IGNITION ON
light on overhead panel are inhibited.

(contd)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

PAGE:
74-2

NUMBER INSTALLED
3.

NUMBER REQUIRED FOR DISPATCH

74 IGNITION
11-01

18

4.

REMARKS OR EXCEPTIONS

Ignition Systems
(cont'd)
2) 600-2C10,
600-2D15
600-2D24,
600-2E25

a) A Systems

(O) One may be inoperative provided both B Systems

are operative.

b) B Systems

(O) Both may be inoperative provided both A Systems

are operative.

30-01

IGNITION A/B
"ARM/ON" Switch
Lights
(light function only)
(600-2B19)

30-02

IGNITION CONT
"ON" Switch Light
(light function only)

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

11-01

4.
C

L & R Engine Speed

Control Systems
(600-2B19)

13-01

76-1

REMARKS OR EXCEPTIONS

|
2

(O) Both may be inoperative provided:

a) ENG SPEED CONTROL switches are selected
OFF for both engines,
b) APR is selected OFF, and,
c) Operations are conducted in accordance with
AFM APR inoperative performance data.
NOTE:

11-03

07/09/2012

NUMBER REQUIRED FOR DISPATCH

76 ENGINE CONTROLS
SYNC SEL Switch
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

PAGE:

NUMBER INSTALLED
3.

10-01

18

Throttle Lever
(FADEC) RVDTs
(600-2C10,
600-2D15,
600-2D24,
600-2E25)

Automatic
Performance
Reserve System
(APR)
(600-2B19)

Thrust levers will not always be aligned

when fan speeds are matched.

One per throttle lever may be inoperative.

|
1

(O) May be inoperative provided:

a) APR is selected OFF, and
b) Operations are conducted in accordance with
AFM APR inoperative performance data.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

76 ENGINE CONTROLS

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
76-2

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
B

07/09/2012

NUMBER REQUIRED FOR DISPATCH

77 ENGINE INDICATING
Engine Vibration
Monitoring
Indications

PAGE:

NUMBER INSTALLED
3.

31-01

18

REMARKS OR EXCEPTIONS

One may be inoperative provided:

a) Operations are not conducted in known or
forecast icing conditions, and
b) Both Ice Detection Systems are operative.

77-1

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

77 ENGINE INDICATING

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
77-2

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
C

78-1

NUMBER REQUIRED FOR DISPATCH

78 ENGINE EXHAUST
Thrust Reverser
Systems

07/09/2012

PAGE:

NUMBER INSTALLED
3.

30-01

18

REMARKS OR EXCEPTIONS

(M) One may be inoperative provided:

a) There is no structural damage to thrust
reverser system beyond approved acceptable
damage limits,
b) Inoperative thrust reverser is deactivated,
stowed and locked in forward thrust position,
and
c) Operations are conducted in accordance with
AFM performance data.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

78 ENGINE EXHAUST

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
78-2

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

21-01

Engine Oil Filter

Impending Bypass
and Chip Detector
Panel (Engine Oil
Detection Panel)
1) 600-2B19
Pre-SB
GE 72-0109

30-01

79-1

NUMBER REQUIRED FOR DISPATCH

79 ENGINE OIL
Oil Replenishment
System
***

07/09/2012

PAGE:

NUMBER INSTALLED
3.

12-01

18

4.

REMARKS OR EXCEPTIONS

(M) May be inoperative provided alternate method for

checking engine oil levels and servicing engine oil is
established and used.

(M) May be inoperative provided an alternate

maintenance procedure is accomplished and does not
exceed 30 flight hours interval(s).

|
|
|

2) 600-2B19
Post-SB
GE 72-0109

(M) May be inoperative provided an alternate

maintenance procedure is accomplished and does not
exceed 100 flight hours interval(s).

|
|
|

3) 600-2C10,
600-2D15,
600-2D24,
600-2E25

(M) May be inoperative provided an alternate

maintenance procedure is accomplished and does not
exceed 100 flight hours interval(s).

Low Oil Pressure

Switch
(600-2C10,
600-2D15
600-2D24,
600-2E25)

|
|

(O) May be inoperative OPEN provided:

a) Both oil pressure readouts are verified
operative, and
b) Repairs are made within one flight.
|

(M)(O) May be inoperative CLOSED provided:

a) Both oil pressure readouts are verified
operative,
b) Inoperative Low Oil Pressure Switch is
deactivated, and
c) Repairs are made within one flight.
NOTE:

Aural warning "Engine Oil" will not be

functional.

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.
C

79-2

NUMBER REQUIRED FOR DISPATCH

79 ENGINE OIL
Engine Oil Level
Indications
(600-2B19***,
600-2C10,
600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

30-03

18

REMARKS OR EXCEPTIONS

(M) Both may be inoperative provided:

a) Engine oil reservoir is refilled within the
permissible time interval, and
b) There is no evidence of excessive oil
consumption.
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

4.

10-01

Engine L/R "STOP"

Switch Lights
(light function only)

10-02

Engine "START"
Switch Lights
(light function only)

10-03

Air Turbine Starter

Speed Cutout
Switches
(600-2B19)

REMARKS OR EXCEPTIONS

Both may be inoperative provided N2 is monitored.

(O) May be inoperative CLOSED provided:

a) Associated Engine STOP Switch Light is
operative,
b) Engine start is manually terminated, and
c) Starter disengagement is confirmed.
NOTE:

80-1

NUMBER REQUIRED FOR DISPATCH

80 STARTING

Starter Air Valves

(600-2C10,
600-2D15,
600-2D24,
600-2E25)

07/09/2012

PAGE:

NUMBER INSTALLED
3.

11-01

18

The Air Turbine Starter will be damaged if it

is left engaged at or above engine idle
speed.

(M)(O) One may be inoperative CLOSED provided

alternate starting procedures are established and
used.
|

U.S. DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT:

REVISION NO:

BOMBARDIER CL-600-2B19/-2C10/-2D15/-2D24/-2E25

DATE:

SYSTEM &
SEQUENCE
NUMBERS

1.
ITEM

2.

07/09/2012

NUMBER INSTALLED
3.

80 STARTING

18

NUMBER REQUIRED FOR DISPATCH

4.

REMARKS OR EXCEPTIONS

THIS PAGE IS INTENTIONALLY LEFT BLANK

PAGE:
80-2