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DEPARTMENT OF TRANSPORTATION Revision: 6
Date: 10/24/96
FEDERAL AVIATION ADMINISTRATION
WASHINGTON, D.C.
M A S T E R M I N I M U M E Q U I P M E N T L I S T
BRITISH AEROSPACE
BAE-ATP
/S/
JAMES H. KLING
CHAIRMAN, FLIGHT OPERATIONS
EVALUATION BOARD (FOEB)
Federal Aviation Administration
Flight Standards Division
AIRCRAFT EVALUATION OFFICE, ANM-270S
1601 Lind Ave. S.W.
Renton, Washington 98055-4056
TELEPHONE: (206) 227-2280
FAX: (206) 227-1270
FEDERAL AVIATION ADMINISTRATION Page: I
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Page 1
Baeatpr6.txt
Table of Contents
SYSTEM NO. SYSTEM PAGE
-- Table of Contents I
-- Log of Revisions II, III
-- Control Page IV, V, VI
-- Highlights of Change VII, VIII, IX
-- Definitions X, XI, XII, XIII
-- Definitions XIV, XV, XVI, XVII
-- Preamble XVIII, XIX
21 Air Conditioning 21-1, 2, 3, 4, 5
21 Air Conditioning 21-6
22 Auto Flight 22-1, 2
23 Communications 23-1, 2, 3
24 Electrical Power 24-1, 2, 3, 4, 5
25 Equipment/Furnishings 25-1, 2, 3, 4, 5
25 Equipment/Furnishings 25-6, 7, 8
26 Fire Protection 26-1, 2, 3, 4, 5
27 Flight Controls 27-1, 2, 3
28 Fuel 28-1, 2
29 Hydraulic Power 29-1
30 Ice and Rain Protection 30-1, 2, 3, 4
31 Indicating/Recording Systems 31-1
32 Landing Gear 32-1, 2, 3, 4
33 Lights 33-1, 2, 3, 4, 5
34 Navigation 34-1, 2, 3, 4, 5
34 Navigation 34-6, 7, 8, 9
35 Oxygen 35-1
38 Water/Waste 38-1
49 Airborne Auxiliary Power 49-1
52 Doors 52-1, 2
56 Windows 56-1
61 Propellers 61-1
73 Engine Fuel & Control 73-1
74 Ignition 74-1
77 Engine Indicating 77-1
79 Engine Oil 79-1, 2, 3
80 Starting 80-1
FEDERAL AVIATION ADMINISTRATION Page: II
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Log of Revisions
----------------------------------------------------------------------
| REV.NO. | DATE | PAGE NUMBERS | INITIALS |
----------------------------------------------------------------------
| ORIGINAL | 06/22/88 | Original | |
| 1 | 01/19/90 | ALL PAGES | |
| 1a | 10/12/90 | HIGHLIGHTS OF REV. | |
| 1a | 10/12/90 | 25-1,25-2 | |
| 2 | 10/19/90 | HIGHLIGHTS OF REV. | |
| 2 | 10/19/90 | 24-1,25-4,26-1,26-2,26-3 | |
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| 2 | 10/19/90 | 26-4,26-5,34-3,35-1,49-1 | |
| 2 | 10/19/90 | 79-1 | |
| 3 | 12/18/90 | HIGHLIGHTS OF REV. | |
| 3 | 12/18/90 | 32-2,79-1 | |
| 4 | 05/16/91 | HIGHLIGHTS OF REV. | |
| 4 | 05/16/91 | 21-2,21-3,21-4,21-5,21-6 | |
| 4 | 05/16/91 | 22-1,22-2,23-2,24-1,24-2 | |
| 4 | 05/16/91 | 24-3,24-4,24-5,25-4,25-5 | |
| 4 | 05/16/91 | 26-1,26-2,26-3,26-4,26-5 | |
| 4 | 05/16/91 | 26-6,27-1,27-2,27-3,29-1 | |
| 4 | 05/16/91 | 30-1,30-2,30-3,30-4,31-1 | |
| 4 | 05/16/91 | 32-1,32-2,32-3,32-4,33-4 | |
| 4 | 05/16/91 | 34-1,34-3,34-4,34-5,34-6 | |
| 4 | 05/16/91 | 34-7,35-1,49-1,52-1,52-2 | |
| 4 | 05/16/91 | 73-1,79-1,79-2 | |
| 5 | 01/27/93 | HIGHLIGHTS OF REV. | |
| 5 | 01/27/93 | 21-1,21-2,21-3,21-4,22-1 | |
| 5 | 01/27/93 | 23-2,23-3,25-1,25-4,26-2 | |
| 5 | 01/27/93 | 26-3,27-1,28-1,33-2,33-3 | |
| 5 | 01/27/93 | 34-2,34-3,34-4,34-6,34-7 | |
| 5 | 01/27/93 | 61-1,73-1,79-1,79-2,79-3 | |
| 5a | 03/17/94 | HIGHLIGHTS OF REV.,DEFINITIONS | |
| 5a | 03/17/94 | 26-3 | |
| 5b | 05/16/96 | HIGHLIGHTS OF REV.,DEFINITIONS | |
| 5b | 05/16/96 | 74-1 | |
| 6 | 10/24/96 | HIGHLIGHTS OF REV.,DEFINITIONS | |
| 6 | 10/24/96 | 21-1,21-2,21-3,21-4,21-5 | |
| 6 | 10/24/96 | 21-6,22-1,22-2,23-1,23-2 | |
| 6 | 10/24/96 | 23-3,24-1,24-2,24-3,24-4 | |
| 6 | 10/24/96 | 24-5,25-1,25-2,25-3,25-4 | |
| 6 | 10/24/96 | 25-5,25-6,25-7,25-8,26-1 | |
| 6 | 10/24/96 | 26-2,26-3,26-4,26-5,26-6 | |
| 6 | 10/24/96 | 27-1,27-2,27-3,28-1,28-2 | |
| 6 | 10/24/96 | 29-1,30-1,30-2,30-3,30-4 | |
| 6 | 10/24/96 | 31-1,32-1,32-2,32-3,32-4 | |
| 6 | 10/24/96 | 33-1,33-2,33-3,33-4,33-5 | |
| 6 | 10/24/96 | 34-1,34-2,34-3,34-4,34-5 | |
----------------------------------------------------------------------
FEDERAL AVIATION ADMINISTRATION Page: III
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Log of Revisions
----------------------------------------------------------------------
| REV.NO. | DATE | PAGE NUMBERS | INITIALS |
----------------------------------------------------------------------
| 6 | 10/24/96 | 34-6,34-7,34-8,34-9,35-1 | |
| 6 | 10/24/96 | 38-1,49-1,52-1,52-2,56-1 | |
| 6 | 10/24/96 | 61-1,73-1,74-1,77-1,79-1 | |
| 6 | 10/24/96 | 79-2,79-3,80-1 | |
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FEDERAL AVIATION ADMINISTRATION Page: IV
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Control Page
SYSTEM PAGE REV NO. CURRENT DATE
Cover Page - 6 10/24/96
Table of Contents I 6 10/24/96
Log of Revisions II 6 10/24/96
III 6 10/24/96
Control Page IV 6 10/24/96
V 6 10/24/96
VI 6 10/24/96
Highlights of Change VII 6 10/24/96
VIII 6 10/24/96
IX 6 10/24/96
Definitions X 6 01/31/95
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XI 6 01/31/95
XII 6 01/31/95
XIII 6 01/31/95
XIV 6 01/31/95
XV 6 01/31/95
XVI 6 01/31/95
XVII 6 01/31/95
Preamble XVIII 2 06/14/89
XIX 2 06/14/89
21 21-1 6 10/24/96
21-2 6 10/24/96
21-3 6 10/24/96
21-4 6 10/24/96
21-5 6 10/24/96
21-6 6 10/24/96
22 22-1 6 10/24/96
22-2 6 10/24/96
23 23-1 6 10/24/96
23-2 6 10/24/96
23-3 6 10/24/96
24 24-1 6 10/24/96
24-2 6 10/24/96
24-3 6 10/24/96
24-4 6 10/24/96
24-5 6 10/24/96
25 25-1 6 10/24/96
25-2 6 10/24/96
25-3 6 10/24/96
25-4 6 10/24/96
FEDERAL AVIATION ADMINISTRATION Page: V
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Control Page
SYSTEM PAGE REV NO. CURRENT DATE
25-5 6 10/24/96
25-6 6 10/24/96
25-7 6 10/24/96
25-8 6 10/24/96
26 26-1 6 10/24/96
26-2 6 10/24/96
26-3 6 10/24/96
26-4 6 10/24/96
26-5 6 10/24/96
27 27-1 6 10/24/96
27-2 6 10/24/96
27-3 6 10/24/96
28 28-1 6 10/24/96
28-2 6 10/24/96
29 29-1 6 10/24/96
30 30-1 6 10/24/96
30-2 6 10/24/96
30-3 6 10/24/96
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30-4 6 10/24/96
31 31-1 6 10/24/96
32 32-1 6 10/24/96
32-2 6 10/24/96
32-3 6 10/24/96
32-4 6 10/24/96
33 33-1 6 10/24/96
33-2 6 10/24/96
33-3 6 10/24/96
33-4 6 10/24/96
33-5 6 10/24/96
34 34-1 6 10/24/96
34-2 6 10/24/96
34-3 6 10/24/96
34-4 6 10/24/96
34-5 6 10/24/96
34-6 6 10/24/96
34-7 6 10/24/96
34-8 6 10/24/96
34-9 6 10/24/96
35 35-1 6 10/24/96
38 38-1 6 10/24/96
FEDERAL AVIATION ADMINISTRATION Page: VI
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Control Page
SYSTEM PAGE REV NO. CURRENT DATE
49 49-1 6 10/24/96
52 52-1 6 10/24/96
52-2 6 10/24/96
56 56-1 6 10/24/96
61 61-1 6 10/24/96
73 73-1 6 10/24/96
74 74-1 6 10/24/96
77 77-1 6 10/24/96
79 79-1 6 10/24/96
79-2 6 10/24/96
79-3 6 10/24/96
80 80-1 6 10/24/96
FEDERAL AVIATION ADMINISTRATION Page: VII
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Highlights of Change
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Effective above date, the BAe-ATP Master Minimum Equipment List has been
revised. Please replace affected pages of the previous list with
revision 6 for a complete up-to-date MMEL.
Deleted all asterisk (*) symbols in accordance with (IAW) Policy Letter
(PL) 61.
22 AUTO FLIGHT
10-1 Autopilot System
COMMENT: Added proviso c) to sub item 2) to include missing time
limitation required for category A designation.
23 COMMUNICATIONS
31-1 Passenger Address System
COMMENT: Updated IAW PL-9 (CG-13).
51-2 Boom Microphones
COMMENT: Added proviso b).
81-1 Touchtone Microphone (DFTM)
COMMENT: New item.
25 EQUIPMENT/FURNISHINGS
10-1 Observer Seat(s)
COMMENT: Updated IAW PL-56 (CG-25).
22-13 Underseat Baggage Restraining Bars
COMMENT: New item IAW PL-79 (CG-28).
40-2 Lavatory Door Ashtrays
COMMENT: New item IAW AD 74-08-09 R2 and draft policy letter.
60-4 First Aid Kits
COMMENT: Updated IAW PL-73 (CG-17).
FEDERAL AVIATION ADMINISTRATION Page: VIII
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Highlights of Change
26 FIRE PROTECTION
11-1 APU Fire Extinguisher System
COMMENT: New item.
22-1 Portable Fire Extinguishers
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COMMENT: Updated IAW PL-75 (CG-19).
32 LANDING GEAR
42-7 Brake Temperature Indicating System
COMMENT: Corrected sequential lettering of provisos c) through f).
33 LIGHTS
13-1 Cockpit/Flight Deck /Flight Compartment and Instrument Panel
Lighting Systems
COMMENT: Updated IAW PL-77 (CG-21).
44-1 Wing Illumination Lights
COMMENT: Revised to comply with Airworthiness Directive 96-09-17.
34 NAVIGATION
12-02 ATC Transponders and Automatic Altitude Reporting Systems
COMMENT: Updated IAW PL-76 (CG-20).
23-09 Vertical Speed Indication (Primary Flight Display only)
COMMENT: Added "(Primary Flight Display only)" for clarification.
42-01 Radio Altimeter System
COMMENT: Changed to category A and added proviso e).
43-01 Ground Proximity Warning System (GPWS)
COMMENT: Updated IAW PL-54 (CG-10).
44-01 Traffic Alert Collision Avoidance System (TCAS)
COMMENT: Updated IAW PL-32.
FEDERAL AVIATION ADMINISTRATION Page: IX
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 10/24/96
BAe-ATP
Highlights of Change
35 OXYGEN
31-1 Portable Oxygen Dispensing Units (Bottles, masks, lines,
gauges and fittings)
COMMENT: Revised title for clarification.
38 WATER/WASTE
10-1 Potable Water Systems
COMMENT: Updated IAW PL-83 (CG-32).
30-1 Lavatory Systems
COMMENT: New item IAW PL-83 (CG-32).
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52 DOORS
60-01 Forward Airstairs System
COMMENT: Added proviso c).
FEDERAL AVIATION ADMINISTRATION Page: X
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95
BAe-ATP
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
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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
FEDERAL AVIATION ADMINISTRATION Page: XI
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95
BAe-ATP
Definitions
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 which has a type design approval for ER operations and
complies with the provisions of Advisory Circular 120-42A. |
8. "Federal Aviation Regulations" (FAR) means the applicable
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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.
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
FEDERAL AVIATION ADMINISTRATION Page: XII
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95
BAe-ATP
Definitions
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
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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
FEDERAL AVIATION ADMINISTRATION Page: XIII
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95
BAe-ATP
Definitions
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.
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
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FEDERAL AVIATION ADMINISTRATION Page: XIV
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95
BAe-ATP
Definitions
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 messages 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, |
FEDERAL AVIATION ADMINISTRATION Page: XV
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95
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BAe-ATP
Definitions
do not affect dispatch and do not require action other than as |
addressed within an operators standard maintenance program. |
|
b. DOUGLAS (MD-11) |
|
Some Douglas 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. |
|
c. AIRBUS (A-300-600, A-310, A-320/319/321, 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-320/319/ |
321, A-330, and A-340 also provide MAINTENANCE status messages. |
|
Any message that effects airplane dispatchability will normally |
be at the WARNING, CAUTION or STATUS level. MAINTENANCE |
messages (A-320/319/321, 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-320/319/321) or CMS (A-330/A-340) interrogation. The systems |
are designed to be fault tolerant, however for any MAINTENANCE |
status (Class II) message, the A-320/319/321 MEL must be |
verified for dispatch capability. For the A-330 and A-340, |
MAINTENANCE status messages do not affect dispatch. |
d. FOKKER (FK-100) |
FEDERAL AVIATION ADMINISTRATION Page: XVI
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95
BAe-ATP
Definitions
|
Fokker aircraft are equipped with Multi Function Display System |
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(MFDS) which provides electronic message referring to the |
different priority levels of system information (WARNING (red), |
CAUTION (amber), AWARENESS (cyan) AND STATUS (white). Any |
messages 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. |
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
FEDERAL AVIATION ADMINISTRATION Page: XVII
Revision: 6
MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95
BAe-ATP
Definitions
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."
Page 15
Baeatpr6.txt
FEDERAL AVIATION ADMINISTRATION Page: XVIII
Revision: 2
MASTER MINIMUM EQUIPMENT LIST Date: 06/14/89
BAe-ATP
Preamble
(Effective 6/14/89)
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
Page 16
Baeatpr6.txt
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.
FEDERAL AVIATION ADMINISTRATION Page: XIX
Revision: 2
MASTER MINIMUM EQUIPMENT LIST Date: 06/14/89
BAe-ATP
Preamble
(Effective 6/14/89)
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
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
Page 17
Baeatpr6.txt
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 |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 21-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 21 AIR CONDITIONING | | | |
| | | | |
| | | | |
| 11-1 Nacelle Bleed C | 4 | 3 | (O)One may be inoperative provided: | |
| Air Valves | | | a) Pressurization system is |
| (HP & LP Bleeds) | | | operative. |
| | | | OR |
| C | | | b) If both ECS packs are |
| | | | inoperative, the operative |
| | | | nacelle bleed air supplies |
| | | | are selected on. |
| | | | |
| C | 4 | 2 | (O)Two may be inoperative provided: | |
| | | | a) Pressurization system is |
| | | | operative. |
| | | | OR |
| C | | | b) If both ECS packs are |
| | | | inoperative, the operative |
| | | | nacelle bleed air supplies |
| | | | are selected on, and |
| | | | c) Aircraft is not flown in |
| | | | known or forecast icing |
| | | | conditions. |
| | | | |
| 11-2 Boost Switch C | 1 | 0 | (M)(O)May be inoperative for | |
| | | | pressurized flight provided both |
| | | | ECS packs operate normally. |
| | | | |
| C | 1 | 0 | (O)May be inoperative provided the | |
| | | | airplane is flown in an |
| | | | unpressurized configuration. |
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Baeatpr6.txt
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 21-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 21 AIR CONDITIONING | | | |
| | | | |
| | | | |
| 11-3 ECS Pack Bleed Air A | 2 | 1 | (O)One may be inoperative provided: | |
| Leak Detection | | | a) Press to isolate switch |
| System | | | operates normally, |
| | | | b) Associated ECS pack is off, |
| | | | c) Other ECS pack operates |
| | | | normally, |
| | | | d) Pressurization system |
| | | | operates normally, and |
| | | | e) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| A | 2 | 0 | (O)Both may be inoperative | |
| | | | provided: |
| | | | a) Both ECS packs are off, |
| | | | b) The airplane is flown in an |
| | | | unpressurized configuration, |
| | | | and |
| | | | c) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 23-1 Avionics Cooling | | | Deleted, Rev 5. |
| Fan Indicator | | | |
| Switches | | | |
| | | | |
| 30-1 Cabin Pressure C | 1 | 0 | (O)May be inoperative provided: | |
| Control System | | | a) The airplane is flown in an |
| | | | unpressurized configuration, |
| | | | and |
| | | | b) Extended overwater |
Page 19
Baeatpr6.txt
| | | | operations are prohibited. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 21-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 21 AIR CONDITIONING | | | |
| | | | |
| | | | |
| 30-3 Cabin Pressure C | 2 | 1 | (M)One may be inoperative for | |
| Outflow Valves | | | pressurized flight provided: |
| | | | a) The failed valve is locked |
| | | | closed, and |
| | | | b) Remaining outflow valve |
| | | | operates normally. |
| | | | |
| C | 2 | 0 | (M)(O)Both may be inoperative | |
| | | | provided the airplane is flown in |
| | | | an unpressurized configuration. |
| | | | |
| 30-4 Cabin Altitude C | 1 | 0 | (O)May be inoperative for | |
| Indicator | | | pressurized flight provided: |
| | | | a) Cabin differential pressure |
| | | | indicator is operative, and |
| | | | b) A chart or table to convert |
| | | | cabin differential pressure |
| | | | to cabin altitude is |
| | | | available to the crew. |
| | | | |
| 30-5 Cabin Differential C | 1 | 0 | (O)May be inoperative for | |
| Pressure Indicator | | | pressurized flight provided: |
| | | | a) Cabin altitude indicator is |
| | | | operative, and |
| | | | b) A chart or table converting |
| | | | cabin altitude versus air- |
| | | | craft altitude to differen- |
| | | | tial pressure is available |
| | | | to the crew. |
| | | | |
| C | 1 | 0 | (O)May be inoperative provided the | |
| | | | airplane is flown in an |
| | | | unpressurized configuration. |
| | | | |
Page 20
Baeatpr6.txt
| | | | |
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| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 21-4 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 21 AIR CONDITIONING | | | |
| | | | |
| | | | |
| 30-6 Cabin Rate of C | 1 | 0 | (O)May be inoperative provided: | |
| Climb Indicator | | | a) Automatic cabin |
| | | | pressurization control |
| | | | system operates normally, |
| | | | and |
| | | | b) Cabin differential pressure |
| | | | indicator and cabin |
| | | | altimeter operate normally. |
| | | | |
| 51-1 Environmental C | 2 | 1 | (O)One may be inoperative provided: | |
| Control System | | | a) Pressurization system |
| Packs | | | operates normally, and |
| | | | b) Flight level does not exceed |
| | | | FL 250. |
| | | | |
| C | 2 | 0 | (O)Both may be inoperative | |
| | | | provided: |
| | | | a) The airplane is flown in an |
| | | | unpressurized configuration, |
| | | | b) Ram air system operates |
| | | | normally, |
| | | | c) Flight deck temperature can |
| | | | be maintained in a |
| | | | comfortable range (65-85 |
| | | | Degrees F), and |
| | | | d) HP bleed switches must both |
| | | | be selected ON during flight |
| | | | in icing conditions. |
| | | | |
| 51-2 Recirculation Fans C | 2 | 1 | (O)One may be inoperative provided | |
| | | | affected ECS System is operated in |
| | | | manual. |
| | | | |
| 51-3 Cabin Ram Air C | 1 | 0 | May be inoperative provided both | |
| System | | | ECS packs operate normally. |
| | | | |
| | | | |
Page 21
Baeatpr6.txt
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 21-5 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 21 AIR CONDITIONING | | | |
| | | | |
| | | | |
| 51-4 Bleed Air C | 1 | 0 | (M)May be inoperative with the | |
| Crossfeed Valve | | | crossfeed valve in the closed |
| | | | position provided both ECS packs |
| | | | operate normally. |
| | | | |
| C | 1 | 0 | (M)(O)May be inoperative with both | |
| | | | packs inoperative or considered |
| | | | inoperative provided: |
| | | | a) Aircraft is flown in an un- |
| | | | pressurized configuration, |
| | | | b) Ram air system operates |
| | | | normally, |
| | | | c) Flight deck temperature can |
| | | | be maintained in a |
| | | | comfortable range (65-85 |
| | | | degrees F), and |
| | | | d) HP bleed switches must both |
| | | | be selected ON during flight |
| | | | in icing conditions. |
| | | | |
| 60-1 ECS Pack Automatic C | 2 | 0 | (O)May be inoperative provided: | |
| Temperature | | | a) Manual temperature control |
| Control | | | for the affected pack |
| | | | operates normally, |
| | | | b) Cabin temperature gauge |
| | | | operates normally, and |
| | | | c) Both ECS pack duct |
| | | | temperatures operate |
| | | | normally. |
| | | | |
| 60-2 ECS Pack Manual C | 2 | 0 | May be inoperative provided | |
| Temperature | | | automatic temperature control on |
| Control | | | the affected ECS pack operates |
| | | | normally. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 22
Baeatpr6.txt
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 21-6 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 21 AIR CONDITIONING | | | |
| | | | |
| | | | |
| 60-3 Cabin Temperature C | 1 | 0 | | |
| Indicator | | | |
| | | | |
| 60-4 Flight Deck C | 1 | 0 | | |
| Temperature | | | |
| Indicator | | | |
| | | | |
| 60-5 Duct Temperature C | 2 | 1 | One may be inoperative provided the | |
| Indicators | | | associated ECS pack auto |
| | | | temperature control operates |
| | | | normally. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
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Page 23
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-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 22-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 22 AUTO FLIGHT | | | |
| | | | |
| | | | |
| 10-1 Autopilot System | | | |
| | | | |
| 1) CAT II Standard C | 2 | 1 | (M)(O)One may be inoperative | |
| | | | provided: |
| | | | a) Remaining autopilot operates |
| | | | normally, and |
| | | | b) AFM autopilot limitations |
| | | | are observed. |
| | | | |
| 2) CAT I Standard C | 2 | 1 | (M)One may be inoperative provided | |
| | | | basic mode operates normally on the |
| | | | remaining autopilot. |
| | | | |
| A | 2 | 0 | (M)(O)Both may be inoperative | |
| | | | provided: |
| | | | a) Operations are limited to |
| | | | not more than 2 flight days |
| | | | before repairs are made, and |
| | | | b) An SCS elevator, aileron, |
| | | | and rudder check is per- |
| | | | formed successfully on both |
| | | | autopilot systems at least |
| | | | once each flight day. |
| | | | OR |
| A | | | c) Operations are limited to | |
| | | | not more than 2 flight days | |
| | | | before repairs are made, and | |
| | | | d) An SCS elevator, aileron, | |
| | | | and rudder check is per- |
| | | | formed successfully on at |
| | | | least one autopilot system |
| | | | before each departure. |
| | | | |
| *** 3) CAT II Approach C | 1 | 0 | (O)May be inoperative provided | |
| Monitoring | | | approach minimums are not dependent |
| System | | | upon its use. |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
Page 24
Baeatpr6.txt
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 22-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 22 AUTO FLIGHT | | | |
| | | | |
| | | | |
| 10-13 Control Wheel C | 2 | 1 | One may be inoperative provided | |
| Disengage | | | autopilot is not engaged below |
| Switches | | | 1,500 feet AGL. |
| | | | |
| 10-15 PFD Autopilot C | 2 | 1 | One may be inoperative provided | |
| Warning | | | autopilot is not engaged below |
| Indication | | | 1,500 feet AGL. |
| | | | |
| 10-16 Autopilot C | 6 | 3 | (M)Filaments may be inoperative | |
| Controller- | | | provided: |
| Indicator | | | a) "AP", "SYS 1", and "SYS 2 |
| Filaments | | | selections are displayed on |
| | | | EFIS, and |
| | | | b) "TURB", "1/2 BANK", and "YD" |
| | | | selector filaments operate/ |
| | | | illuminate normally. |
| | | | |
| 10-17 Autopilot Mode C | 16 | 0 | (M)Filament(s) may be inoperative | |
| Controller Mode | | | in one or both controllers provided |
| Selector | | | the associated EFIS displays the |
| Filaments | | | selected mode. |
| | | | |
| 20-1 Yaw Damper C | 2 | 1 | | |
| | | | |
| A | 2 | 0 | (M)Both may be inoperative | |
| | | | provided: |
| | | | a) SCS rudder check operates |
| | | | normally on at least one |
| | | | system, and |
| | | | b) Operations are limited to |
| | | | not more than two flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
Page 25
Baeatpr6.txt
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 23-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 23 COMMUNICATIONS | | | |
| | | | |
| | | | |
| 11-1 Communications C | - | - | As required by FAR. | |
| System (VHF, HF, | | | |
| UHF) | | | |
| | | | |
| 11-2 Selective Call C | - | 0 | | |
| *** System (Selcal/ | | | |
| Calsel) | | | |
| | | | |
| 12-2 ARINC C | 1 | 0 | | |
| *** Communications | | | |
| Addressing and | | | |
| Reporting System | | | |
| (ACARS) | | | |
| | | | |
| 31-1 Passenger Address | | | | |
| System | | | | |
| | | | |
| 1) Passenger B | 1 | 0 | (O)May be inoperative provided: | |
| Configuration | | | a) Alternate normal and emer- | |
| | | | gency procedures and/or | |
| | | | operating restrictions are | |
| | | | established and used, and | |
| | | | b) Flight Deck/Cabin Interphone | |
| | | | system operates normally. | |
| | | | |
| 2) Cargo D | 1 | 0 | | |
| Configuration | | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
Page 26
Baeatpr6.txt
| BAe-ATP | DATE: 10/24/96 | 23-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 23 COMMUNICATIONS | | | |
| | | | |
| | | | |
| 31-2 Cabin Chimes C | - | 0 | (O)May be inoperative provided: | |
| | | | a) Passenger address system |
| | | | operates normally. |
| | | | OR |
| C | | | b) Alternate procedures are |
| | | | established and used. |
| | | | |
| 41-1 Service Interphone C | 1 | 0 | (O)May be inoperative provided: | |
| System (Flight | | | a) Alternate, normal and |
| Deck to Cabin) | | | emergency procedures and/or |
| (Cabin to Flight | | | operating restrictions are |
| Deck)(Flight Deck | | | established and used, and |
| to Ground) | | | b) PA System operates normally. |
| | | | |
| 41-2 Cabin Attendants C | 1 | 0 | (O)May be inoperative provided: | |
| Interphone System | | | a) Alternate, normal and |
| | | | emergency procedures are |
| | | | established and used |
| | | | (including those dependent |
| | | | upon call signal), and |
| | | | b) Passenger address system |
| | | | operates normally. |
| | | | |
| | | | NOTE: Not required for all-cargo |
| | | | operations. |
| | | | |
| 51-1 Flight Deck C | - | 0 | May be inoperative provided head- | |
| Speakers | | | sets for flight deck crewmembers |
| | | | (including official observer in |
| | | | forward observer's seat) are |
| | | | installed and operate normally. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 23-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
Page 27
Baeatpr6.txt
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 23 COMMUNICATIONS | | | |
| | | | |
| | | | |
| 51-2 Boom Microphones A | - | 0 | May be inoperative provided: | |
| | | | a) Flight Data Recorder (FDR) |
| | | | operates normally, |
| | | | b) Handheld microphone is | |
| | | | available and operates | |
| | | | normally at inoperative | |
| | | | location, and | |
| | | | c) Repairs are made within | |
| | | | three flight days. |
| | | | |
| 71-1 Cockpit Voice A | 1 | 0 | May be inoperative provided: | |
| Recorder (CVR) | | | a) Flight Data Recorder (FDR) |
| | | | operates normally, and |
| | | | a) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 81-1 Touchtone C | - | 0 | (O)May be inoperative provided | |
| *** Microphone (DFTM) | | | alternate procedures are | |
| | | | established and used. | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 24-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
Page 28
Baeatpr6.txt
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 24 ELECTRICAL POWER | | | |
| | | | |
| | | | |
| 10-2 APU Generator C | 1 | 0 | (M)May be inoperative provided APU | |
| *** | | | is considered inoperative and is |
| | | | not used. |
| | | | |
| C | 1 | 0 | (M)May be inoperative and APU air | |
| | | | used provided the quill drive is |
| | | | removed. |
| | | | |
| 17-1 Battery Heating C | 1 | 0 | (M)May be inoperative provided: | |
| System | | | a) Batteries are fully charged, |
| | | | b) Battery Overheat Warning |
| | | | System operates normally, |
| | | | and |
| | | | c) Aircraft is not flown in |
| | | | known or forecast ambient |
| | | | temperatures below -10 |
| | | | degrees C. |
| | | | |
| 21-1 Generator on Line C | 2 | 1 | One may be inoperative provided the | |
| OFF Indicators | | | associated generator failure |
| | | | warnings on the CWP are operating |
| | | | normally. |
| | | | |
| 21-2 Generator Failure C | 2 | 1 | One may be inoperative provided: | |
| Warnings on CWP | | | a) Both aural attention getters |
| | | | are operating normally, and |
| | | | b) Associated generator on line |
| | | | OFF indicator is operating |
| | | | normally. |
| | | | |
| 21-3 Generator Ammeter C | 1 | 0 | May be inoperative provided: | |
| | | | a) Both generator on line OFF |
| | | | indicators are operating |
| | | | normally, and |
| | | | b) Associated generator |
| | | | voltmeter is operating |
| | | | normally. |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 24-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 24 ELECTRICAL POWER | | | |
Page 29
Baeatpr6.txt
| | | | |
| | | | |
| 21-4 Generator C | 1 | 0 | May be inoperative provided: | |
| Voltmeter | | | a) Both generator on line OFF |
| | | | indicators are operating |
| | | | normally, and |
| | | | b) Associated generator ammeter |
| | | | is operating normally. |
| | | | |
| 22-1 Inverter Failure C | 2 | 1 | One may be inoperative provided: | |
| Warning Lights on | | | a) Both inverters are operating |
| CWP | | | normally, and |
| | | | b) Both attention getters are |
| | | | operating normally for this |
| | | | failure indication. |
| | | | |
| 22-2 Inverter On Line C | 2 | 1 | One may be inoperative provided: | |
| OFF Indicators | | | a) Both inverter failure |
| | | | warning lights on the CWP |
| | | | are operating normally, and |
| | | | b) Voltage and Frequency of |
| | | | associated inverter are |
| | | | indicating normally. |
| | | | |
| 22-3 Inverter Voltmeter C | 1 | 0 | May be inoperative provided: | |
| | | | a) Both inverters are operating |
| | | | normally, |
| | | | b) Associated frequency meter |
| | | | is operating normally, |
| | | | c) Both inverter failure |
| | | | warning lights on the CWP |
| | | | are operating normally, and |
| | | | d) Both inverter on line |
| | | | indicators are operating |
| | | | normally. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 24-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 24 ELECTRICAL POWER | | | |
| | | | |
| | | | |
| 22-4 Inverter Frequency C | 1 | 0 | May be inoperative provided: | |
Page 30
Baeatpr6.txt
| Meter | | | a) Both inverters are operating |
| | | | normally, |
| | | | b) Associated voltmeter is |
| | | | operating normally, |
| | | | c) Both inverter failure |
| | | | warning lights on the CWP |
| | | | are operating normally, and |
| | | | d) Both inverter on line |
| | | | indicators are operating |
| | | | normally. |
| | | | |
| 31-1 TRU On Line OFF C | 2 | 1 | (O)One may be inoperative provided: | |
| Indicators | | | a) The associated TRU failure |
| | | | warnings on the CWP are |
| | | | operating normally, |
| | | | b) Undervoltage indicators are |
| | | | operating normally, and |
| | | | c) Both attention getters |
| | | | associated with the failure |
| | | | signal operates normally. |
| | | | |
| 31-2 TRU Failure C | 2 | 1 | (O)One may be inoperative provided: | |
| Indication On The | | | a) Both attention getters are |
| CWP | | | operating normally for this |
| | | | failure signal, |
| | | | b) Both TRU on line OFF |
| | | | indicators are operating |
| | | | normally, |
| | | | c) Both undervoltage indicators |
| | | | are operating normally, and |
| | | | d) Both undervoltage warnings |
| | | | are operating normally. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 24-4 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 24 ELECTRICAL POWER | | | |
| | | | |
| | | | |
| 31-3 Battery/TRU C | 1 | 0 | (O)May be inoperative provided: | |
| Ammeter | | | a) Both battery on line OFF |
| | | | indicators are operating |
| | | | normally, |
Page 31
Baeatpr6.txt
| | | | b) Both TRU on line OFF |
| | | | indicators are operating |
| | | | normally, |
| | | | c) TRU voltmeter is operating |
| | | | normally, and |
| | | | d) Undervoltage warning system |
| | | | is operating normally. |
| | | | |
| 31-4 Battery/TRU C | 1 | 0 | (O)May be inoperative provided: | |
| Voltmeter | | | a) Both battery on line OFF |
| | | | indicators are operating |
| | | | normally, |
| | | | b) Both TRU on line OFF |
| | | | indicators are operating |
| | | | normally, |
| | | | c) TRU ammeter is operating |
| | | | normally, and |
| | | | d) Undervoltage warning system |
| | | | is operating normally. |
| | | | |
| 32-1 Battery On Line B | 2 | 1 | (M)(O)One may be inoperative | |
| OFF Indicator | | | provided it is determined that the |
| | | | associated battery functions |
| | | | normally on the bus bar before each |
| | | | departure. |
| | | | |
| 34-1 Low Voltage C | 2 | 1 | (O)One may be inoperative provided: | |
| Indicators | | | a) Both undervoltage detectors |
| | | | are operating normally, and |
| | | | b) Low Volts warning on the CWP |
| | | | is operating normally. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 24-5 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 24 ELECTRICAL POWER | | | |
| | | | |
| | | | |
| 40-1 Ground Power C | 1 | 0 | | |
| Supply (GPU) | | | |
| System 200 | | | |
| Volts AC | | | |
| | | | |
| 40-2 Ground Power C | 1 | 0 | | |
| Supply (GPU) | | | |
Page 32
Baeatpr6.txt
| System 28 Volt DC | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 25-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 25 EQUIPMENT/FURNISHINGS | | | |
| | | | |
| | | | |
| 10-1 Observer Seat(s) | | | | |
| | | | | |
| 1) Primary A | 1 | 0 | May be inoperative provided: | |
| Observer Seat | | | a) A passenger seat in the | |
| (Including | | | passenger cabin is made | |
| associated | | | available to an FAA | |
| equipment) | | | inspector for the | |
| | | | performance of official | |
| | | | duties, and | |
Page 33
Baeatpr6.txt
| | | | b) Repairs are made within two | |
| | | | flight days. | |
| | | | OR | |
| A | | | c) Second observer's seat is | |
| | | | available and acceptable to | |
| | | | an FAA inspector for the | |
| | | | performance of official | |
| | | | duties, and | |
| | | | d) Repairs are made within two | |
| | | | flight days. | |
| | | | OR | |
| A | | | e) Primary observer's seat is | |
| | | | available with the required | |
| | | | minimum safety equipment | |
| | | | (safety belt and oxygen) and | |
| | | | acceptable to an FAA | |
| | | | inspector for the | |
| | | | performance of official | |
| | | | duties, and | |
| | | | f) Repairs are made within two | |
| | | | flight days. | |
| | | | |
| | | | (Continued) |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 25-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 25 EQUIPMENT/FURNISHINGS | | | |
| | | | |
| | | | |
| 10-1 Observer Seat(s) | | | | |
| (Cont'd) | | | | |
| | | | | |
| 1) Primary | | | NOTE 1: These provisos are | |
| Observer Seat | | | intended to provide for | |
| (Including | | | occupancy of the above | |
| associated | | | seats by an FAA inspector | |
| equipment) | | | when the minimum safety | |
| (Cont'd) | | | equipment (oxygen and | |
| | | | safety belt) is functional | |
| | | | and the inspector | |
| | | | determines the conditions | |
Page 34
Baeatpr6.txt
| | | | to be acceptable. | |
| | | | |
| | | | NOTE 2: The pilot-in-command will | |
| | | | determine if the minimum | |
| | | | safety equipment is | |
| | | | functional for other | |
| | | | persons authorized to | |
| | | | occupy any observer | |
| | | | seat(s). | |
| | | | |
| *** 2) Additional D | - | 0 | | |
| Observer | | | NOTE: The Pilot-in-Command will | |
| Seat(s) | | | determine if the minimum | |
| (Including | | | safety equipment is | |
| associated | | | functional for other persons | |
| equipment) | | | authorized to occupy any | |
| | | | observer seat(s). | |
| | | | |
| 10-11 Pilot's Seat C | 2 | 0 | (M)May be inoperative provided: | |
| Adjustment | | | a) Position of the seat(s) |
| System | | | permits normal pilot |
| | | | visibility and full flight |
| | | | control movement, and |
| | | | b) Seat(s) is secured with |
| | | | mechanical stops. |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 25-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 25 EQUIPMENT/FURNISHINGS | | | |
| | | | |
| | | | |
| 10-12 Crewmember | | | DELETED, REV 1. |
| Shoulder Harness | | | |
| | | | |
| 20-1 "Fasten Seat Belt C | - | - | One or more signs or placards may | |
| While Seated" | | | be illegible or missing provided a |
| Signs or Placards | | | legible sign or placard is readable |
| | | | from each occupied passenger seat. |
| | | | |
| 21-1 Flight Attendant C | - | - | (M)(O)One single or one dual | |
| Seat Assembly | | | position seat may be inoperative |
| (Single or Dual | | | provided: |
| Position) | | | a) Affected seat position(s) is |
| | | | not occupied, |
| | | | b) Flight attendant(s) |
| | | | displaced by inoperative |
Page 35
Baeatpr6.txt
| | | | seat position(s) occupy the |
| | | | passenger seat(s) most |
| | | | accessible to their assigned |
| | | | exit, |
| | | | c) Alternate procedures are |
| | | | established for displaced |
| | | | flight attendant(s), |
| | | | d) Folding type seat(s) is |
| | | | stowed or secured in the |
| | | | retracted position, and |
| | | | e) Passenger seat(s) assigned |
| | | | to flight attendant(s) is |
| | | | placarded "FOR FLIGHT |
| | | | ATTENDANT USE ONLY". |
| | | | |
| | | | NOTE 1: A folding seat that will |
| | | | not stow automatically is |
| | | | considered inoperative. |
| | | | |
| | | | (Continued) |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 25-4 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 25 EQUIPMENT/FURNISHINGS | | | |
| | | | |
| | | | |
| 21-1 Flight Attendant | | | NOTE 2: A seat position with an |
| Seat Assembly | | | inoperative or missing lap |
| (Single or Dual | | | belt is considered |
| Position) (Cont'd) | | | inoperative. |
| | | | |
| | | | NOTE 3: The above provisos apply |
| | | | only to required flight |
| | | | attendant seats. Seats in |
| | | | excess of those required |
| | | | may be inoperative |
| | | | provided they are properly |
| | | | stowed or secured in the |
| | | | retracted position. |
| | | | Individual operators, when |
| | | | operating with inoperative |
| | | | seats, will consider the |
| | | | locations and combinations |
| | | | of seats to ensure that |
Page 36
Baeatpr6.txt
| | | | the proximity to exits and |
| | | | distribution requirements |
| | | | of the applicable FAR are |
| | | | met. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 25-5 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 25 EQUIPMENT/FURNISHINGS | | | |
| | | | |
| | | | |
| 22-12 Passenger Seats | | | |
| and Belts | | | |
| | | | |
| 1) Seat Backs C | - | - | (M)May be inoperative secured in | |
| | | | the upright position. |
| | | | |
| C | - | - | (M)May be inoperative in other than | |
| | | | the upright position provided: |
| | | | a) Does not block an Emergency |
| | | | Exit. |
| | | | b) Does not restrict any pass- |
| | | | enger from access to the |
| | | | main aircraft aisle, |
| | | | c) The affected seat(s) is |
| | | | blocked and placarded "Do |
| | | | Not Occupy", and |
| | | | d) May not be required by a |
| | | | Flight Attendant who needs |
| | | | to be moved due to an |
| | | | inoperative seat. |
| | | | |
Page 37
Baeatpr6.txt
| | | | NOTE 1: A seat position with an |
| | | | inoperative or missing lap |
| | | | belt is considered |
| | | | inoperative. |
| | | | |
| | | | NOTE 2: Inoperative seats do not |
| | | | affect the required number |
| | | | of Flight Attendants. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 25-6 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 25 EQUIPMENT/FURNISHINGS | | | |
| | | | |
| | | | |
| 22-13 Underseat C | - | - | (M)(O)May be inoperative provided: | |
| Baggage | | | a) Baggage is not stowed under | |
| Restraining Bars | | | seat with inoperative | |
| | | | restraining bar, | |
| | | | b) Associated seat is placarded | |
| | | | "DO NOT STOW BAGGAGE UNDER | |
| | | | THIS SEAT", and | |
| | | | c) Procedures are established | |
| | | | to alert Cabin Crew of inop- | |
| | | | erative restraining bar. | |
| | | | |
| 30-1 Passenger | - | 0 | Passenger convenience items, as | |
| *** Convenience | | | expressed in this MMEL, are those |
| Item(s) | | | items related to passenger comfort, |
| | | | convenience, or entertainment such |
| | | | as, but not limited to: galley |
| | | | equipment, movie equipment, ash |
| | | | trays, stereo, equipment, overhead |
| | | | reading lamps, etc. Items |
| | | | addressed elsewhere in this |
| | | | document shall not be included. (M) |
| | | | and (O) procedures may be required |
| | | | and included in the Air Carrier's |
| | | | appropriate document. |
Page 38
Baeatpr6.txt
| | | | |
| | | | NOTE: Lavatory door ash trays are |
| | | | not considered passenger |
| | | | convenience items. |
| | | | |
| 40-1 Lavatory Hot Water C | 1 | 0 | (M)May be inoperative provided | |
| Heater | | | heater is deactivated and secured. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 25-7 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 25 EQUIPMENT/FURNISHINGS | | | |
| | | | |
| | | | |
| 40-2 Lavatory Door | | | | |
| Ashtrays | | | | |
| | | | |
| 1) Airplanes with A | - | - | One may be missing provided it is | |
| more than one | | | replaced within 10 calendar days. | |
| lavatory door | | | | |
| ashtray | | | | |
| installed | | | | |
| | | | |
| 2) Airplanes with A | 1 | 0 | May be missing provided it is | |
| only one | | | replaced within 3 calendar days. | |
| lavatory door | | | | |
| ashtray | | | | |
| installed | | | | |
| | | | |
| 60-1 Emergency Locator C | - | - | As required by FAR. | |
| Transmitter | | | |
| | | | |
| 60-2 Megaphones C | - | 1 | Any in excess of those required by | |
| | | | FAR may be inoperative or missing |
| | | | provided: |
| | | | a) Inoperative megaphone is |
| | | | removed from the passenger |
| | | | cabin, and |
| | | | b) Required distribution is |
| | | | maintained. |
| | | | |
Page 39
Baeatpr6.txt
| 60-3 Cabin Emergency C | - | - | May be in operative or missing | |
| Flashlight Holder/ | | | provided the crewmember assigned to |
| Flashlights | | | the affected position has a |
| | | | normally operating flashlight |
| | | | readily available. |
| | | | |
| 60-4 First Aid Kits D | - | - | Any in excess of those required by | |
| | | | FAR may be incomplete or missing | |
| | | | provided required distribution is | |
| | | | maintained. | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 25-8 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 25 EQUIPMENT/FURNISHINGS | | | |
| | | | |
| | | | |
| 60-5 Emergency Medical | | | DELETED REV. 1. |
| Kits | | | |
| | | | |
| 60-6 Girt Bar Heater C | 3 | 0 | (M)May be inoperative provided: | |
| *** | | | a) Associated heater is |
| | | | deactivated and secured, and |
| | | | b) Associated girt bar and |
| | | | arming mechanism operate |
| | | | normally. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 40
Baeatpr6.txt
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 26-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 26 FIRE PROTECTION | | | |
| | | | |
| | | | |
| 10-1 Condition Lever A | 2 | 1 | One may be inoperative provided: | |
| Fire Warning | | | a) CWP warning and associated |
| Indicator | | | center roof panel fire |
| | | | warning PBSI's operate |
| | | | normally, and |
| | | | b) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 10-2 APU Fire C | 1 | 0 | (M)May be inoperative provided APU | |
| *** Detection System | | | is considered inoperative and is |
| | | | not used. |
| | | | |
| 10-3 APU Fire C | 1 | 0 | (M)May be inoperative provided APU | |
| *** Detection System | | | is considered inoperative and is |
| Test Function | | | not used. |
| | | | |
| 10-4 APU Fire C | 1 | 0 | (M)May be missing provided: | |
| *** Extinguisher | | | a) APU is considered inop- |
| Thermal Discharge | | | ertive and is not used, and |
| Disc | | | b) APU start control circuit |
| | | | breaker is pulled. |
| | | | OR |
| C | | | b) Another acceptable means of |
| | | | determining that the bottle |
| | | | is fully charged is used |
| | | | once each flight day. |
| | | | |
| 11-0 Engine Fire | | | DELETED, REV 1. |
| Detection Switch | | | |
| System | | | |
| | | | |
Page 41
Baeatpr6.txt
| 11-1 APU Fire C | 1 | 0 | (M)May be inoperative provided APU | |
| *** Extinguisher | | | is considered inoperative and is | |
| System | | | not used. | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 26-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 26 FIRE PROTECTION | | | |
| | | | |
| | | | |
| 12-1 APU Fire C | 1 | 0 | (M)May be inoperative provided: | |
| *** Detection Warning | | | a) Fire warning bell operates |
| Horn | | | normally, |
| | | | b) APU control panel fire |
| | | | warning indicators operate |
| | | | normally, |
| | | | c) Auto shut down system |
| | | | operates normally, and |
| | | | d) A qualified person remains |
| | | | on the flight deck any time |
| | | | the APU is running. |
| | | | |
| 12-2 Engine Fire A | 4 | 2 | (O)One loop on each engine may be |
| *** Detection Loops | | | inoperative provided: |
| (Dual Loop System) | | | a) Inoperative loop is |
| | | | isolated, and |
| | | | b) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 13-1 Nacelle Bleed Air C | 2 | 1 | (O)One may be inoperative provided: | |
| Supply Leak | | | a) Associated bleed air supply |
| Detection System | | | (both engine and HP bleeds) |
| | | | is off, and |
| | | | b) The airplane is not flown |
| | | | into known or forecast icing |
| | | | conditions. |
| | | | |
| 15-1 Forward Cargo C | 1 | 0 | (O)May be inoperative provided | |
| *** Compartment Smoke | | | airflow panel is verified closed. |
| Detection System | | | |
| | | | |
| 15-2 Aft Cargo C | 1 | 0 | (O)May be inoperative provided | |
| *** Compartment Smoke | | | airflow panel is verified closed. |
| Detection System | | | |
Page 42
Baeatpr6.txt
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 26-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 26 FIRE PROTECTION | | | |
| | | | |
| | | | |
| 17-1 Lavatory Smoke C | - | 0 | M)(O)For each lavatory, the | |
| Detection System | | | lavatory smoke detection system may |
| | | | be inoperative provided: |
| | | | a) Lavatory fire extinguisher |
| | | | system operates normally. |
| | | | OR |
| C | | | b) Lavatory waste receptacle is |
| | | | empty, |
| | | | c) Lavatory door is locked |
| | | | CLOSED and placarded, |
| | | | "INOPERATIVE - DO NOT |
| | | | ENTER", and |
| | | | d) Lavatory is not used for any |
| | | | purpose. |
| | | | |
| | | | NOTE 1: These provisos are not |
| | | | intended to prohibit |
| | | | lavatory inspections by |
| | | | crewmembers. |
| | | | |
| | | | NOTE 2: A lavatory fire |
| | | | extinguisher system is not |
| | | | required for all-cargo |
| | | | operations. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 43
Baeatpr6.txt
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 26-4 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 26 FIRE PROTECTION | | | |
| | | | |
| | | | |
| 20-1 Lavatory Fire C | 1 | 0 | (M)(O)For each lavatory, the | |
| Extinguisher | | | lavatory fire extinguisher system |
| System | | | may be inoperative provided: |
| | | | a) Lavatory smoke detector |
| | | | system operates normally. |
| | | | OR |
| C | | | b) Lavatory waste receptacle is |
| | | | empty, |
| | | | c) Lavatory door is locked |
| | | | CLOSED and placarded |
| | | | "INOPERATIVE - DO NOT |
| | | | ENTER", and |
| | | | d) Lavatory is not used for any |
| | | | purpose. |
| | | | |
| | | | NOTE 1: These provisos are not |
| | | | intended to prohibit |
| | | | lavatory inspections by |
| | | | crewmembers. |
| | | | |
| | | | NOTE 2: A lavatory fire |
| | | | extinguisher system is not |
| | | | required for all-cargo |
| | | | operations. |
| | | | |
| 21-1 Engine Fire C | 2 | 0 | (M)One or both may be missing | |
| Extinguisher | | | provided an accepted procedure is |
| Discharge | | | used to verify adequacy of bottle |
| Indicators (Discs) | | | charge before each departure. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
Page 44
Baeatpr6.txt
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 26-5 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 26 FIRE PROTECTION | | | |
| | | | |
| | | | |
| 21-2 Engine Fire C | 4 | 3 | (M)(O)One indicator may be inop- | |
| Extinguisher | | | erative on the No. 2 Shot system |
| Discharged Shot | | | only, provided: |
| Indicator | | | a) All remaining indicators |
| | | | operate normally before |
| | | | engine start, |
| | | | b) Discharge Disc is in place |
| | | | before each departure, and |
| | | | c) Fire extinguisher discharge |
| | | | indicator pin is checked |
| | | | once each flight day. |
| | | | |
| 22-1 Portable Fire D | - | - | (M)Any in excess of those required | |
| Extinguishers | | | by FAR may be inopertative or | |
| | | | missing provided: | |
| | | | a) Inoperative fire | |
| | | | extinguisher is tagged | |
| | | | inoperative, removed from | |
| | | | installed location, and | |
| | | | placed out of sight so it | |
| | | | cannot be mistaken for a | |
| | | | functional unit, and | |
| | | | b) Required distribution is | |
| | | | maintained. | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
Page 45
Baeatpr6.txt
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 27-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 27 FLIGHT CONTROLS | | | |
| | | | |
| | | | |
| 10-1 Trim Tab C | 3 | 1 | DELETED, REV 1. |
| Indicators | | | |
| (Aileron & Rudder) | | | |
| | | | |
| 21-1 Rudder Pedal C | 2 | 0 | (M)One or both may be inoperative | |
| Adjustment System | | | provided: |
| | | | a) Adjustments can be secured |
| | | | in a position which suits |
| | | | individual pilot(s) |
| | | | requirements, and |
| | | | b) Position of pedal(s) permits |
| | | | normal full flight control |
| | | | movement. |
| | | | |
| 30-1 Electric Trim C | 2 | 1 | (O)Trim switch assembly on one | |
| Switch(es) | | | pilots control column may be |
| (Elevator) | | | inoperative provided: |
| | | | a) Electric trim switch on the |
| | | | other control column |
| | | | operates normally, |
| | | | b) Manual trim system operates |
| | | | normally, |
| | | | c) Autotrim (autopilot) |
| | | | operates normally, |
| | | | d) Both autopilot disconnect |
| | | | buttons operate normally, |
| | | | and |
| | | | e) Trim indicator (SCS) on |
| | | | right hand instrument panel |
| | | | operates normally. |
| | | | |
| 34-1 Stall Warning C | 2 | 1 | (M)One may be inoperative provided | |
| System | | | remaining system and stick shaker |
| | | | operates normally and is checked |
| | | | before each departure. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
Page 46
Baeatpr6.txt
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 27-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 27 FLIGHT CONTROLS | | | |
| | | | |
| | | | |
| 34-2 Stall Warning A | 2 | 1 | (M)One stall warning vane heater | |
| De-Ice System | | | may be inoperative provided: |
| Vane Heaters | | | a) Remaining stall warning |
| | | | de-ice system channel |
| | | | operates normally, |
| | | | b) Remaining (non-associated) |
| | | | stall warning system |
| | | | operates normally, and is |
| | | | checked before each |
| | | | departure, and |
| | | | c) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 51-1 Flap Motor A | 1 | 0 | (M)(O)May be inoperative provided: | |
| Running Light | | | a) Flap motor is operating |
| | | | normally before each |
| | | | departure, |
| | | | b) Associated flap motor is |
| | | | monitored on the right hand |
| | | | TRU ammeter while flaps are |
| | | | running, and |
| | | | c) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 51-3 Wing Flap A | 1 | 0 | (M)(O)May be inoperative provided: | |
| Position | | | a) Flap position is verified |
| Indicator | | | before each takeoff, |
| | | | b) Flaps are verified to |
| | | | operate normally throughout |
| | | | the operating range at least |
| | | | once each flight day, and |
| | | | b) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
Page 47
Baeatpr6.txt
| | | |
| BAe-ATP | DATE: 10/24/96 | 27-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 27 FLIGHT CONTROLS | | | |
| | | | |
| | | | |
| 70-1 Control (Gust) A | 1 | 0 | (M)(O)May be inoperative provided: | |
| Locks System | | | a) System is inspected to |
| | | | ensure non-interference with |
| | | | throttle and primary flight |
| | | | control systems, |
| | | | b) Alternative methods of |
| | | | securing flight controls are |
| | | | used, |
| | | | c) Aircraft shall not be taxied |
| | | | in tailwind components |
| | | | greater than 25 knots, and |
| | | | d) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 28-1 |
Page 48
Baeatpr6.txt
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 28 FUEL | | | |
| | | | |
| | | | |
| 20-1 Fuel Boost Pumps C | 4 | 2 | (M)One may be inoperative in each | |
| | | | collector tank. |
| | | | |
| 20-4 Pressure C | 1 | 0 | (M)May be inoperative provided an | |
| Refueling System | | | alternate refueling procedure is |
| | | | used. |
| | | | |
| 41-1 Refueling Panel C | 2 | 0 | (M)May be inoperative provided fuel | |
| Quantity | | | in associated tank is verified by |
| Indicators | | | an alternate procedure before each |
| | | | departure. |
| | | | |
| 41-2 Refueling Panel C | 1 | 0 | (M)May be inoperative provided: | |
| Overfull System | | | a) Alternate procedures are |
| | | | used to prevent overfilling |
| | | | of tanks, and |
| | | | b) Fuel in tanks is verified by |
| | | | an alternate procedure |
| | | | before each departure. |
| | | | |
| 41-3 Main Tank Fuel C | 2 | 1 | (M)One may be inoperative provided: | |
| Quantity | | | a) Both fuel flow meters |
| Indicators | | | operate normally, |
| (Flight Deck) | | | b) Both fuel used indicators |
| | | | operate normally, and |
| | | | c) Fuel quantity in associated |
| | | | tank is determined by an |
| | | | alternate procedure before |
| | | | each departure. |
| | | | |
| 41-4 Fuel Indicator C | 1 | 0 | (M)May be inoperative provided fuel | |
| Test Switch | | | quantity is determined by an |
| | | | alternate procedure. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 28-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
Page 49
Baeatpr6.txt
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 28 FUEL | | | |
| | | | |
| | | | |
| 42-1 Magnetic Fuel C | 8 | 0 | (M)(O)May be inoperative provided | |
| Quantity | | | fuel quantity is determined by an |
| Indicators | | | alternate procedure. |
| (MFLI's) (Dripless | | | |
| Sticks) | | | |
| | | | |
| 43-1 Fuel Tank C | 1 | 0 | (O)May be inoperative provided: | |
| Temperature | | | a) Total Air Temperature or |
| Indicating System | | | Static Air Temperature is |
| | | | substituted for indication |
| | | | of fuel temperature, and |
| | | | b) AFM limitations are |
| | | | observed. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 29-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
Page 50
Baeatpr6.txt
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 29 HYDRAULIC POWER | | | |
| | | | |
| | | | |
| 10-1 Hydraulic Pump C | 2 | 0 | (M)(O)Both may be inoperative | |
| Depressurizing | | | provided the valve is in the full |
| Valve Solenoid | | | pressure position, solenoid |
| | | | de-energized. |
| | | | |
| 20-1 Ground Servicing C | 1 | 0 | (M)May be inoperative provided it | |
| Valve | | | is secured in the CLOSED position. |
| | | | |
| 31-1 Hydraulic LO LEVEL C | 1 | 0 | (M)May be inoperative provided | |
| Warning Light On | | | hydraulic quantity is verified |
| CWP | | | before each departure. |
| | | | |
| 31-2 Main Hydraulic C | 1 | 0 | (M)May be inoperative provided | |
| Quantity Low Level | | | hydraulic quantity is verified |
| Warning Light | | | before each departure. |
| | | | |
| 31-3 Auxiliary C | 1 | 0 | (M)May be inoperative provided | |
| Hydraulic Low | | | hydraulic quantity is verified |
| Level Warning | | | before each departure. |
| Light | | | |
| | | | |
| 33-1 Main Hydraulic C | 1 | 0 | (O)May be inoperative provided: | |
| Pressure Indicator | | | a) Both brake system pressure |
| | | | indicators are operating |
| | | | normally, and |
| | | | b) Associated hydraulic system |
| | | | pressure is verified before |
| | | | each departure. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 30-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 30 ICE AND RAIN | | | |
Page 51
Baeatpr6.txt
| PROTECTION | | | |
| | | | |
| 10-01 Airframe C | 1 | 0 | (M)(O)May be inoperative provided: | |
| De-Icing System | | | a) The airplane is not flown |
| (Wing and | | | into known or forecast icing |
| Empennage) | | | conditions, and |
| | | | b) De-icing boots are kept in |
| | | | the deflation cycle. |
| | | | |
| 10-02 Airframe C | 1 | 0 | (O)May be inoperative provided: | |
| De-Icing | | | a) Airframe de-icing pressure |
| Monitoring | | | indicator operates normally. |
| System (Wing and | | | OR |
| Empennage) C | | | b) The airplane is not flown |
| | | | into known or forecast icing |
| | | | conditions. |
| | | | |
| 10-03 Airframe C | 1 | 0 | (O)May be inoperative provided: | |
| De-Icing Timer | | | a) Manual de-icing system |
| | | | operates normally. |
| | | | OR |
| C | | | b) The airplane is not flown |
| | | | into known or forecast icing |
| | | | conditions, and |
| | | | c) De-icing boots are in a |
| | | | deflation cycle. |
| | | | |
| 10-04 Airframe C | 1 | 0 | May be inoperative provided: | |
| De-Icing | | | a) Airframe de-icing monitoring |
| Pressure | | | system operates normally. |
| Indicator | | | OR |
| C | | | b) The airplane is not flown |
| | | | into known or forecast icing |
| | | | conditions. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 30-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 30 ICE AND RAIN | | | |
| PROTECTION | | | |
| | | | |
| 20-00 Engine De-Icing C | 2 | 1 | One may be inoperative provided the | |
Page 52
Baeatpr6.txt
| Systems | | | airplane is not flown into known or |
| | | | forecast icing conditions. |
| | | | |
| 20-01 Engine and C | 2 | 0 | One or both may be inoperative | |
| Propeller | | | provided the airplane is not flown |
| De-Icing | | | into known or forecast icing |
| Transfer Switch | | | conditions. |
| | | | |
| 20-02 Engine De-Icing C | 1 | 0 | | |
| Phase Current | | | |
| Selector | | | |
| | | | |
| 30-01 Main Pitot Heat B | 2 | 1 | (M)May be inoperative provided the | |
| Systems | | | airplane is not flown into known or |
| | | | forecast icing conditions. |
| | | | |
| 30-02 Pitot Head B | 3 | 2 | (O)One may be inoperative provided: | |
| Heater Warning | | | a) Associated CWP warning |
| Lights | | | system operates normally, |
| | | | and |
| | | | b) All other components of the |
| | | | pitot heat system are |
| | | | functioning normally. |
| | | | |
| 30-03 Static Port B | 2 | 1 | One may be inoperative provided the | |
| Heaters | | | airplane is not flown into known or |
| | | | forecast icing conditions. |
| | | | |
| 41-01 Windshield C | 2 | 1 | One may be inoperative provided the | |
| Heating System | | | airplane is not flown into known or |
| | | | forecast icing conditions. |
| | | | |
| C | 2 | 0 | Both may be inoperative provided | |
| | | | the airplane is operated in Day VMC |
| | | | flight conditions, and temperatures |
| | | | remain 6 degrees C or above. |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 30-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 30 ICE AND RAIN | | | |
| PROTECTION | | | |
| | | | |
| 41-03 Windshield Heat C | 2 | 0 | (O)May be inoperative provided | |
| Master PBSI | | | associated windshield heat system |
| Lights | | | operates normally. |
| | | | |
Page 53
Baeatpr6.txt
| 41-04 Windshield Heat | | | |
| Overtemp Warning | | | |
| Lights | | | |
| | | | |
| 1) Main C | 2 | 1 | One may be inoperative provided: | |
| Windshield | | | a) Associated windshield master |
| | | | heat switch is selected OFF, |
| | | | and |
| | | | b) Airplane is not flown into |
| | | | known or forecast icing |
| | | | conditions. |
| | | | |
| 2) Side C | 2 | 1 | One may be inoperative provided: | |
| Windshield | | | a) Associated windshield master |
| | | | heat switch is selected OFF, |
| | | | and |
| | | | b) Airplane is not flown into |
| | | | known or forecast icing |
| | | | conditions. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 30-4 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 30 ICE AND RAIN | | | |
| PROTECTION | | | |
| | | | |
| 42-01 Windshield C | 2 | 0 | May be inoperative provided the | |
| Wipers System | | | airplane is not flown in |
| | | | precipitation within 5 nautical |
| | | | miles of the airport of takeoff or |
| | | | intended landing. |
| | | | |
| 1) Windshield C | 1 | 0 | (M)May be inoperative for all | |
Page 54
Baeatpr6.txt
| Wiper Park | | | flight conditions provided the |
| Function | | | blade(s) can be positioned in a |
| | | | location that will not obstruct |
| | | | forward vision. |
| | | | |
| 2) Windshield C | 2 | 2 | Slow function may be inoperative | |
| Wiper | | | provided fast function operates |
| Fast/Slow | | | normally. |
| Selection | | | |
| | | | |
| 43-00 Rain C | 1 | 0 | | |
| *** Repellent System | | | |
| | | | |
| 43-01 Windshield C | 2 | 0 | | |
| Washer System | | | |
| | | | |
| 60-01 Propeller C | 2 | 0 | May be inoperative provided the | |
| De-Icing Systems | | | airplane is not flown into known or |
| | | | forecast icing conditions. |
| | | | |
| 70-01 Drain Mast C | 1 | 0 | (M)May be inoperative provided: | |
| Heater | | | a) Heater is deactivated and |
| | | | secured, and |
| | | | b) Associated water supply is |
| | | | shut off. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 31-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 31 INDICATING/RECORDING | | | |
| SYSTEMS | | | |
| | | | |
| 21-01 Clock C | - | 1 | | |
| | | | |
| 22-01 Fatigue Meter C | 1 | 0 | | |
| | | | |
| 30-00 AIDS C | 1 | 0 | | |
| *** Maintenance | | | |
| Recorder | | | |
| | | | |
| 30-01 Hour Meter C | 1 | 0 | | |
Page 55
Baeatpr6.txt
| | | | |
| 31-01 Flight Data A | 1 | 0 | May be inoperative provided: | |
| Recorder (FDR) | | | a) Cockpit Voice Recorder (CVR) |
| | | | operates normally, and |
| | | | b) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 51-01 Red Flashing C | 2 | 1 | One may be inoperative provided | |
| Attention | | | master warning aural alert and all |
| Getting Lights | | | discrete warning lights operate |
| | | | normally. |
| | | | |
| 51-02 Amber Flashing C | 2 | 1 | One may be inoperative provided | |
| Attention | | | master warning aural alert and all |
| Getting Lights | | | discrete caution lights operate |
| | | | normally. |
| | | | |
| 51-03 Aural Attention C | 1 | 0 | May be inoperative provided: | |
| Warning Horn | | | a) Both flashing attention |
| (CWP) | | | getting lights operate |
| | | | normally, and |
| | | | b) All CWP warning lights |
| | | | operate normally. |
| | | | |
| 51-04 Central Warning C | 1 | 0 | May be inoperative so as to remain | |
| Panel Dimming | | | in the bright mode for day |
| System | | | operations only. |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 32-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 32 LANDING GEAR | | | |
| | | | |
| | | | |
| 42-1 Brake Isolation C | 2 | 0 | (M)One or both may be inoperative | |
| Cock (Valve) | | | provided isolation cock(s) are |
| Indicators | | | checked once each flight day for |
| | | | normal operation. |
| | | | |
| 42-2 Brake Pressure C | 2 | 1 | (O)One may be inoperative provided: | |
| Supply Indication | | | a) Main hydraulic pressure |
| System | | | indicator operates normally, |
| | | | b) All four brake line pressure |
| | | | indicators operate normally, |
| | | | c) Brake pressure low pressure |
Page 56
Baeatpr6.txt
| | | | warning light(s) operate |
| | | | normally. |
| | | | |
| 42-3 Brake Pressure A | 1 | 0 | May be inoperative provided: | |
| Low Pressure | | | a) Brake pressure supply |
| Warning Light | | | indicators operate normally, |
| | | | and |
| | | | b) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 32-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 32 LANDING GEAR | | | |
| | | | |
| | | | |
| 42-4 Brake Line A | 4 | 2 | One may be inoperative in the inner | |
| Pressure Indicator | | | system and one in the outer system |
| | | | provided: |
| | | | a) Associated brake low |
| | | | pressure lights operate |
| | | | normally, |
| | | | c) Inoperative indicators are |
| | | | not on the same side, and |
| | | | d) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 42-6 Brake Temperature A | 4 | 3 | (M)(O)One may be inoperative | |
| Sensor | | | provided: |
Page 57
Baeatpr6.txt
| | | | a) Brake temperature gauge |
| | | | (analogue) operates |
| | | | normally. |
| | | | b) Remaining three brake temp- |
| | | | erature channels indicate a |
| | | | temperature of less than 180 |
| | | | degrees C before flight, |
| | | | c) Landing Gear Bay Overheat |
| | | | detection system operates |
| | | | normally, |
| | | | d) Should a rejected take-off |
| | | | occur, the aircraft must be |
| | | | inspected before the next |
| | | | flight, and |
| | | | e) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 32-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 32 LANDING GEAR | | | |
| | | | |
| | | | |
| 42-7 Brake Temperature C | 1 | 0 | (M)(O)May be inoperative provided: | |
| Indicating System | | | a) Ambient temperatures are |
| | | | below 50 degrees C, |
| | | | b) A minimum of 20 minutes |
| | | | cooling time has elapsed |
| | | | before dispatch utilizing |
| | | | two engine taxi, |
| | | | c) A minimum of 35 minutes | |
| | | | cooling time has elapsed |
| | | | before dispatch utilizing |
| | | | single engine taxi, |
| | | | d) Landing gear bay overheat | |
| | | | detection system operates |
| | | | normally, |
| | | | e) It can be verified that a | |
| | | | rejected takeoff, high |
| | | | efficiency stop, or landing |
Page 58
Baeatpr6.txt
| | | | involving use of assymetric |
| | | | braking was not utilized on |
| | | | the prior leg, and |
| | | | f) Should a rejected takeoff | |
| | | | occur after dispatch, the |
| | | | aircraft must return for an |
| | | | inspection of wheels, tires, |
| | | | and brakes before the next |
| | | | flight. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 32-4 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 32 LANDING GEAR | | | |
| | | | |
| | | | |
| 42-8 Brake Temperature C | 1 | 0 | (M)(O)May be inoperative, not | |
| Indicator Overheat | | | illuminated, provided: |
| Light | | | a) Analogue gauge operates |
| | | | normally, |
| | | | OR |
| A | | | b) All operative brake temp- |
| | | | erature channels (analogue) |
| | | | indicate a temperature of |
| | | | less than 180 degrees C |
| | | | before TAXI, |
| | | | c) Landing gear bay overheat |
| | | | detection system operates |
| | | | normally, |
| | | | d) Should a rejected take-off |
| | | | occur, the aircraft must be |
| | | | inspected before flight, and |
| | | | e) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
Page 59
Baeatpr6.txt
| A | 1 | 0 | (M)(O)May be inoperative, | |
| | | | illuminated, provided: |
| | | | a) Analogue gauge operates |
| | | | normally, |
| | | | b) Light is masked, and |
| | | | c) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | OR |
| C | | | d) Light is masked, and |
| | | | e) Brake temperature indicating |
| | | | system is considered |
| | | | inoperative. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 33-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 33 LIGHTS | | | |
| | | | |
| | | | |
| 11-1 Flight Deck C | 1 | 0 | May be inoperative provided | |
| Overhead Flood | | | instrument and distribution panel |
| Lights | | | flood lights operate normally. |
| | | | |
| 13-1 Cockpit/Flight C | - | - | Individual lights may be | |
| Deck /Flight | | | inoperative provided remaining | |
| Compartment and | | | lights are: | |
| Instrument Panel | | | a) Sufficient to clearly | |
| Lighting Systems | | | illuminate all required | |
| | | | instruments, controls, and | |
| | | | other devices for which they | |
| | | | are provided, | |
| | | | b) Positioned so that direct | |
| | | | rays are shielded from | |
| | | | flight crewmembers' eyes, | |
| | | | and | |
| | | | c) Lighting configuration and | |
| | | | intensity is acceptable to | |
| | | | the flight crew. | |
| | | | | |
| | | | Note: When making above determin- | |
| | | | ation, consideration should | |
Page 60
Baeatpr6.txt
| | | | be given to lighting avail- | |
| | | | able with only the Emergency | |
| | | | busbar powered. | |
| | | | |
| 14-1 Distribution Panel C | 2 | 0 | All may be inoperative provided | |
| Flood Light(s) | | | overhead flood light(s) operate |
| | | | normally. |
| | | | |
| C | 2 | 0 | All may be inoperative for day | |
| | | | operations. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 33-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 33 LIGHTS | | | |
| | | | |
| | | | |
| 17-1 Filament Test C | 1 | 0 | (O)Master or individual push-to- | |
| System | | | test feature may be inoperative |
| | | | provided the lights intended |
| | | | purpose can be confirmed by |
| | | | operations or system test. |
| | | | |
| 17-2 Legend Dimming C | 1 | 0 | Dim function may be inoperative for | |
| System | | | day operations so as to remain in |
| | | | the bright mode. |
| | | | |
| 20-1 Passenger Interior C | 1 | 1 | Lights must be sufficient for cabin | |
| Illumination | | | attendants to perform their duties. |
| Lights | | | |
| | | | |
| 20-2 Passenger Notice | | | |
| System | | | |
| | | | |
| 1) "No Smoking/ C | - | - | (M)(O)A passenger seat from which a | |
| Fasten Seat | | | "No Smoking/Fasten Seat Belt" sign |
| Belt" Signs | | | is not readily legible is |
| | | | considered inoperative and must be |
| | | | blocked. |
| | | | |
| C | - | - | (O)If one or more "No Smoking/ | |
| | | | Fasten Seat Belt" signs are |
Page 61
Baeatpr6.txt
| | | | inoperative, the affected passenger |
| | | | seat(s) may be occupied provided: |
| | | | a) Passenger Address System |
| | | | operates normally, and can |
| | | | be heard clearly throughout |
| | | | the cabin during flight, and |
| | | | b) PA System is used to notify |
| | | | the passengers when seat |
| | | | belts should be fastened, |
| | | | and smoking is prohibited. |
| | | | |
| C | - | 0 | May be inoperative for all cargo | |
| | | | operations. |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 33-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 33 LIGHTS | | | |
| | | | |
| | | | |
| 31-1 Compartment Lights C | - | 0 | | |
| (Nose/Tail, Cargo | | | |
| and Lavatory) | | | |
| | | | |
| 32-1 Service Lights C | - | 0 | May be inoperative provided | |
| | | | procedures are not dependent upon |
| | | | its use. |
| | | | |
| 41-1 Position Lights C | - | 1 | One light on each wing and one | |
| System | | | light on the tail must operate |
| | | | normally for night operations. |
| | | | |
| C | - | 0 | All may be inoperative for day | |
| | | | operations. |
| | | | |
| 42-1 Anti-Collision C | 2 | 0 | One or both may be inoperative for | |
| Lights (Fuselage/ | | | night operations provided wing tip |
| Vertical Fin) | | | strobe lights operate normally. |
| | | | |
| 43-1 Landing Lights B | 2 | 1 | One may be inoperative for night | |
| | | | operations provided the associated |
| | | | taxi light operates normally. |
| | | | |
| C | 2 | 0 | One or both may be inoperative for | |
| | | | day operations. |
| | | | |
| 43-2 Taxi Lights C | 2 | 0 | | |
| | | | |
Page 62
Baeatpr6.txt
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 33-4 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 33 LIGHTS | | | |
| | | | |
| | | | |
| 44-1 Wing Illumination C | 2 | 0 | May be inoperative for night | |
| Lights | | | operations provided airplane is not | |
| | | | operated in known or forecast icing | |
| | | | conditions. | |
| | | | |
| C | 2 | 0 | May be inoperative for day | |
| | | | operations. |
| | | | |
| 45-1 Wing Strobe Light C | 1 | 0 | | |
| System | | | |
| | | | |
| 46-1 Logo Lights C | - | 0 | | |
| | | | |
| 52-1 Floor Proximity C | 1 | 1 | Individual lights may be | |
| Emergency Escape | | | inoperative provided FAA approved |
| Path Marking | | | minimum acceptable lighting levels |
| System | | | specified in one of the following |
| | | | documents are complied with: |
| | | | a) FAA engineering approval |
| | | | letter. |
| | | | OR |
| C | | | b) FAA approved report of the |
| | | | Type Design holder, |
| | | | OR |
| C | | | c) Limitations and Conditions |
| | | | section of the applicable |
| | | | Supplemental Type |
| | | | Certificate (STC), |
| | | | OR |
| C | | | d) An FAA approved report |
| | | | incorporated in the Master |
Page 63
Baeatpr6.txt
| | | | Drawing List for the |
| | | | applicable STC. |
| | | | |
| C | 1 | 0 | May be inoperative for all-cargo | |
| | | | operations. |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 33-5 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 33 LIGHTS | | | |
| | | | |
| | | | |
| 52-2 Exit Locator Sign C | 5 | 5 | Two filaments/bulbs may be | |
| System | | | inoperative in each light. |
| | | | |
| 52-3 Interior Emergency C | 1 | 0 | May be inoperative in cargo areas | |
| Exit Light System | | | for mixed or all-cargo |
| | | | configurations provided: |
| | | | a) No persons occupy that area, |
| | | | and |
| | | | b) Forward entrance door light |
| | | | must operate normally at all |
| | | | times. |
| | | | |
| 52-4 Exterior Emergency C | - | 0 | May be inoperative for day | |
| Lights | | | operations. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 64
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| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 12-01 TAS Indicator C | 1 | 0 | | |
| | | | |
| 12-02 ATC Transponders C | - | - | As required by FAR. | |
| and Automatic | | | | |
| Altitude D | - | - | Any in excess of those required by | |
| Reporting | | | FAR may be inoperative. | |
| Systems | | | | |
| | | | |
| 12-04 Total Air C | 1 | 0 | May be inoperative provided Static | |
| Temperature | | | Air Temperature (SAT) operates |
| Indicator | | | normally. |
| | | | |
| 13-01 Standby C | 1 | 0 | May be inoperative provided VMC | |
| Altimeter | | | exists at both departure and |
| Vibrator | | | arrival airports. |
| | | | |
| 21-00 RMI | | | |
| | | | |
| 1) Heading C | - | 1 | May be inoperative provided | |
| Indication | | | stabilized heading indication on |
| | | | the associated pilot's panel |
| | | | operates normally. |
| | | | |
| 2) VOR/ADF C | - | 1 | May be inoperative provided other | |
| Pointer | | | VOR/ADF system(s) operate normally |
| Indication | | | and meet FAR requirments. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 65
Baeatpr6.txt
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 21-02 Non-Stabilized B | 1 | 0 | (O)May be inoperative provided: | |
| Magnetic Compass | | | a) Any combination of two gyro |
| | | | stabilized or AHRS compass |
| | | | systems operate normally, |
| | | | and |
| | | | b) Airplane is operated with |
| | | | dual independent navigation |
| | | | capability, and under |
| | | | positive radar control by |
| | | | ATC on the en route portion |
| | | | of the flight. |
| | | | |
| C | 1 | 0 | (O)May be inoperative for flights | |
| | | | that are entirely within areas of |
| | | | magnetic unreliablity provided at |
| | | | least two stabilized directional |
| | | | gyro systems are installed, operate |
| | | | normally, and are used in |
| | | | conjunction with approved free gyro |
| | | | navigation techniques. |
| | | | |
| 23-00 Turn and Slip | | | DELETED, REV 1. |
| Indicators | | | |
| | | | |
| 23-01 EFIS Overspeed B | 2 | 1 | One may be inoperative provided VMO | |
| Warning | | | aural warning operates normally. |
| Indicator | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 66
Baeatpr6.txt
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 23-02 Flight Director C | - | 0 | May be inoperative provided | |
| System | | | approach minimums are not dependent |
| | | | upon its use. |
| | | | |
| 23-04 EFIS Low Speed | | | DELETED, REV 1. |
| Warning | | | |
| Indicator | | | |
| | | | |
| 23-05 EFIS Speed Trend C | 2 | 0 | | |
| Indicator | | | |
| | | | |
| 23-06 EFIS Airspeed A | 1 | 0 | May be inoperative provided | |
| Indicator (Bugs) | | | operations are limited to not more |
| System | | | than three flight days before |
| | | | repair is made. |
| | | | |
| 23-07 Instrument B | - | 0 | May be inoperative provided | |
| Comparator | | | approach minimums are not dependent |
| | | | upon its use. |
| | | | |
| 23-08 Altitude Alert A | - | 0 | (O)May be inoperative provided: | |
| System | | | a) Autopilot with altitude hold |
| | | | operates normally, and |
| | | | b) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
Page 67
Baeatpr6.txt
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-4 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 23-09 Vertical Speed C | 2 | 1 | One may be inoperative for day VMC | |
| Indication | | | only. |
| (Primary Flight | | | | |
| Display only) | | | | |
| | | | |
| 23-10 Voice C | 1 | 0 | May be inoperative provided | |
| Advisory/Flight | | | procedures are not dependent upon |
| Profile Advisory | | | its use. |
| | | | |
| 23-11 EFIS VOR/ADF A | 4 | 0 | May be inoperative provided: | |
| Bearing Pointer | | | a) Standby RMI and Standby RMI |
| Selector Switch | | | bearing pointers operate |
| | | | normally, and |
| | | | b) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 23-12 EFIS Nav. A | 2 | 0 | May be inoperative "stuck" in an | |
| Display (ND) | | | operational mode provided: |
| Mode Selector | | | a) Either Map, Map + Weather, |
| | | | or Rose modes are displayed, |
| | | | b) Test Mode operates normally, |
| | | | and |
| | | | c) Operations are limited to |
| | | | three flight days before |
| | | | repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
Page 68
Baeatpr6.txt
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-5 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 23-13 Attitude and A | 2 | 1 | (M)(O)May be inoperative provided: | |
| Heading | | | a) Each pilots panel has a full |
| Reference System | | | display of attitude and |
| (AHARS) | | | heading information from an |
| Switching | | | independent source, |
| | | | b) EFIS Display Copy switch is |
| | | | not moved during flight, |
| | | | c) Remaining EFIS panel |
| | | | switching operates normally, |
| | | | d) Standby instruments operate |
| | | | normally, and |
| | | | e) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 23-14 Air Data A | 2 | 0 | (M)(O)May be inoperative provided: | |
| Computer (ADC) | | | a) Each pilot's panel has |
| Switching | | | independent altitude, |
| | | | airspeed, and temperature |
| | | | indications, |
| | | | b) Both Air Data Computers are |
| | | | functioning normally, |
| | | | c) EFIS Display Copy switch is |
| | | | not moved during flight, |
| | | | d) Standby instruments operate |
| | | | normally, and |
| | | | e) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
Page 69
Baeatpr6.txt
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-6 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 30-00 Microwave C | - | 0 | As required by FAR. | |
| Landing System | | | |
| (MLS) | | | |
| | | | |
| 41-01 Weather Radar C | 1 | - | As required by FAR. | |
| | | | |
| 1) Auto Tilt C | 1 | 0 | (O)May be inoperative provided | |
| Function | | | manual tilt operates normally. |
| | | | |
| 41-02 Electronic Check C | 1 | 0 | | |
| List Display | | | |
| | | | |
| 42-01 Radio Altimeter A | 1 | 0 | May be inoperative provided: | |
| System | | | a) Approach minimums or |
| | | | operating procedures are not |
| | | | dependent upon its use, |
| | | | b) Coupled approach mode on the |
| | | | autopilot is not used, |
| | | | c) Both servo altimeter and |
| | | | standby altimeter operate |
| | | | normally, and |
| | | | d) GPWS is considered |
| | | | inoperative, and |
| | | | e) Repairs are made within two | |
| | | | flight days. | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-7 |
Page 70
Baeatpr6.txt
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 43-01 Ground Proximity | | | |
| Warning System | | | |
| (GPWS) | | | |
| | | | |
| 1) Modes 1 - 4 A | - | 0 | (O)May be inoperative provided: | |
| | | | a) Alternate Procedures are | |
| | | | established and used, and | |
| | | | b) Repairs are made within two | |
| | | | flight days. | |
| | | | |
| 2) Test Mode A | 1 | 0 | May be inoperative provided: | |
| | | | a) GPWS is considered |
| | | | inoperative, and |
| | | | b) Repairs are made within two | |
| | | | flight days. | |
| | | | |
| 3) Glideslope B | 2 | 0 | | |
| Deviation | | | | |
| (Mode 5) | | | | |
| | | | |
| *** 4) Advisory C | - | 0 | (O)May be inoperative provided | |
| Callouts | | | alternate procedures are | |
| | | | established and used. | |
| | | | |
| *** 5) Windshear C | - | 0 | (O)May be inoperative provided | |
| Mode | | | alternate procedures are | |
| | | | established and used. | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-8 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
Page 71
Baeatpr6.txt
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 44-01 Traffic Alert | | | | |
| Collision | | | | |
| Avoidance System | | | | |
| (TCAS) | | | | |
| | | | |
| 1) TCAS System C | - | 0 | (M)May be inoperative provided | |
| | | | system is deactivated and secured. | |
| | | | |
| *** 2) Combined TA C | 2 | 1 | (O)May be inoperative on the non- | |
| and RA Dual | | | flying pilot side provided: | |
| Displays | | | a) TA and RA elements and audio | |
| | | | functions operate normally | |
| | | | on the flying pilot side, | |
| | | | and | |
| | | | b) TA and RA display | |
| | | | indications are visible to | |
| | | | the non-flying pilot. | |
| | | | |
| 3) Resolution C | 2 | 1 | (O)One may be inoperative on the | |
| Advisory (RA) | | | non-flying pilot side. | |
| Display | | | | |
| System(s) C | - | 0 | (O)May be inoperative provided: | |
| | | | a) All Traffic Alert (TA) | |
| | | | display elements and voice | |
| | | | command audio functions are | |
| | | | operative, and | |
| | | | b) TA only mode is selected by | |
| | | | the crew. | |
| | | | |
| 4) TA Display C | - | 0 | (O)May be inoperative provided all | |
| System(s) | | | installed RA displays and audio | |
| | | | functions are operative. | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 34-9 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
Page 72
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| 34 NAVIGATION | | | |
| | | | |
| | | | |
| 51-01 Radio Compass C | - | - | As required by FAR. | |
| (ADF) System | | | |
| | | | |
| 52-01 Distance C | - | - | As required by FAR. | |
| Measuring | | | |
| Equipment (DME) | | | |
| | | | |
| 54-01 Navigation C | - | - | As required by FAR. | |
| Systems (LORAN. | | | |
| Omega/Area Nav | | | |
| VHF, VLF, INS, | | | |
| Doppler) | | | |
| | | | |
| 54-02 Marker Beacon C | - | 0 | May be inoperative provided | |
| System | | | approach procedures are not |
| | | | dependent upon its use. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
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| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 35-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 35 OXYGEN | | | |
| | | | |
Page 73
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| | | | |
| 10-1 Oxygen External C | 1 | 0 | (M)May be inoperative/missing | |
| Discharge | | | provided: |
| Indicator | | | a) Oxygen pressure is |
| | | | sufficient for planned |
| | | | flight, and |
| | | | b) Vent port is free from |
| | | | obstruction including ice. |
| | | | |
| 31-1 Portable Oxygen C | - | - | (M)Any in excess of those required | |
| Dispensing Units | | | by FAR may be unserviceable or | |
| (Bottles, masks, | | | missing provided: | |
| lines, gauges and | | | a) Required distribution is | |
| fittings) | | | maintained throughout the | |
| | | | aircraft, and |
| | | | b) Bottles not properly |
| | | | serviced are replaced, |
| | | | serviced, or removed at the |
| | | | next available maintenance |
| | | | facility. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
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| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 38-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 38 WATER/WASTE | | | |
| | | | |
| | | | |
| 10-1 Potable Water C | - | - | (M)May be inoperative provided | |
Page 74
Baeatpr6.txt
| Systems | | | appropriate procedures are | |
| | | | established to deactivate | |
| | | | applicable system components, | |
| | | | (i.e., tank drained), prevent its | |
| | | | servicing, inspect system for leaks | |
| | | | and to provide for crewmember | |
| | | | inspection. | |
| | | | |
| 30-1 Lavatory Systems C | - | - | (M)May be inoperative provided | |
| | | | appropriate procedures are | |
| | | | established applicable to | |
| | | | deactivate system components, | |
| | | | (i.e., drain waste), secure door | |
| | | | closed, placard inoperative and to | |
| | | | provide for crewmember inspection. | |
| | | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
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| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 49-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 49 AIRBORNE AUXILIARY | | | |
| POWER | | | |
| | | | |
| 00-1 Auxiliary Power C | 1 | 0 | (M)May be inoperative provided: | |
| *** Unit (APU) | | | a) APU Master Switch is |
| | | | selected OFF, and |
Page 75
Baeatpr6.txt
| | | | b) APU start control circuit |
| | | | breaker is pulled and |
| | | | collared, and |
| | | | c) Procedures are not dependent |
| | | | upon its use. |
| | | | |
| 00-2 APU Main Access C | 1 | 0 | (M)May be damaged or missing | |
| *** Door Fire Seal | | | provided: |
| | | | a) APU is considered |
| | | | inoperative, and |
| | | | b) APU start control circuit |
| | | | breaker is pulled and |
| | | | collared. |
| | | | |
| 50-1 APU Bleed Air C | 1 | 0 | (M)May be inoperative provided APU | |
| *** Control Valve | | | is considered inoperative. |
| | | | |
| C | 1 | 0 | (M)May be inoperative and the APU | |
| | | | used for electrical power provided: |
| | | | a) The valve is confirmed |
| | | | closed, and |
| | | | b) Bleed Valve PBSI remains |
| | | | selected OFF. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
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| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 52-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 52 DOORS | | | |
| | | | |
| | | | |
| 60-01 Forward C | 1 | 0 | (M)May be inoperative provided: | |
| Airstairs System | | | a) Cabin entry door opens, |
| | | | closes, latches, and locks |
| | | | normally, | |
| | | | b) No fluid leaks are observed, | |
Page 76
Baeatpr6.txt
| | | | and | |
| | | | c) Airstair is stowed and | |
| | | | locked in the flight stowed | |
| | | | position. | |
| | | | |
| 72-01 Cabin Entry Door A | 3 | 0 | (O)May be inoperative provided: | |
| Warning Light | | | a) It is determined by visual |
| System (Flight | | | inspection that the |
| Deck) | | | associated door is closed |
| | | | latched, and locked before |
| | | | each departure, and |
| | | | b) EXITS warning on the CWP |
| | | | operates normally, |
| | | | c) Individual cabin door |
| | | | warning light operates |
| | | | normally, and |
| | | | d) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| 72-02 Individual Cabin A | 3 | 0 | (O)May be inoperative provided: | |
| Door | | | a) Associated door is inspected |
| LOCKED/UNLOCKED | | | and verified closed, |
| Lights | | | latched, and locked before |
| (Passenger | | | each departure, |
| Cabin) | | | b) Cabin entry door warning |
| | | | light system in the cockpit |
| | | | operates normally, and |
| | | | c) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 52-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 52 DOORS | | | |
| | | | |
| | | | |
| 72-03 Forward Baggage C | 2 | 0 | (M)May be inoperative provided: | |
| Door Warning | | | a) It is determined by visual |
| Lights (Flight | | | inspection that the |
| Deck/ Cabin) | | | associated door is closed, |
| | | | latched, and locked before |
| | | | each departure, |
| | | | b) EXITS warning on the CWP |
| | | | operates normally, and |
Page 77
Baeatpr6.txt
| | | | c) Restraining net is fastened |
| | | | in place before each |
| | | | departure. |
| | | | |
| 73-00 Over Wing C | 2 | 0 | (O)May be inoperative provided: | |
| Emergency Exit | | | a) It is determined by visual |
| Warning Lights | | | inspection that the |
| (Flight Deck) | | | associated exit is closed |
| | | | and locked before each |
| | | | departure, and |
| | | | b) EXITS warning on the CWP |
| | | | operates normally. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
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| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 56-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 56 WINDOWS | | | |
| | | | |
| | | | |
| 10-1 Cockpit A | 2 | 2 | (M)Outer glass ply on one wind- | |
| Windshields | | | shield may be cracked provided: |
| | | | a) Vision through the wind- |
| | | | shield is acceptable to the |
| | | | pilot, |
| | | | b) Windshield heating system |
| | | | for the affected side is |
| | | | deactivated, |
| | | | c) Aircraft is not dispatched |
| | | | into known or forecast icing |
Page 78
Baeatpr6.txt
| | | | conditions, and |
| | | | d) Operations are limited to |
| | | | not more than 24 flight |
| | | | hours before repair is made. |
| | | | |
| 10-2 Fixed Side A | 2 | 2 | (M)Outer glass ply on one window | |
| Windows | | | may be cracked provided: |
| | | | a) Vision through the window is |
| | | | acceptable to the pilot, |
| | | | b) Windshield heating system |
| | | | for the affected side is |
| | | | deactivated, |
| | | | c) Aircraft is not dispatched |
| | | | into known or forecast icing |
| | | | conditions, and |
| | | | d) Operations are limited to |
| | | | not more than 24 flight |
| | | | hours before repair is made. |
| | | | |
| 20-1 Passenger B | 26 | 26 | Cracks in either the inner or outer | |
| Compartment | | | panel are allowable provided flight |
| Windows | | | is conducted unpressurized. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 61-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 61 PROPELLERS | | | |
| | | | |
| | | | |
| 22-1 Propeller Brake | | | DELETED, REV 1. |
| System | | | |
| | | | |
| 22-2 Synchronization C | 1 | 0 | (M)May be inoperative provided | |
| System | | | system has been deactivated. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 79
Baeatpr6.txt
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| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 73-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 73 ENGINE FUEL & CONTROL | | | |
| | | | |
| | | | |
| 30-1 Fuel Used C | 2 | 0 | Both may be inoperative provided | |
| Indicators | | | associated quantity gauge operates |
| | | | normally. |
| | | | |
| 31-1 Fuel Flow B | 2 | 1 | (O)One may be inoperative provided: | |
| Indicators | | | a) Associated fuel tank |
| | | | quantity indicator is |
| | | | operative, and |
| | | | b) Acceptable monitoring |
| | | | procedure is established and |
| | | | used. |
| | | | |
| 31-2 Fuel Pressure | | | DELETED, REV 1. |
| Indicators | | | |
Page 80
Baeatpr6.txt
| | | | |
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| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 74-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 74 IGNITION | | | |
| | | | |
| | | | |
| 01-1 Auto Ignition A | 2 | 0 | (M)(O)May be inoperative provided: |
| *** Systems | | | a) Continuous Ignition is |
| | | | verified to operate normally |
| | | | before engine start, |
| | | | b) Continuous Ignition is |
| | | | selected ON for all takeoffs |
| | | | and landings in turbulence |
| | | | and in conditions of icing, |
| | | | precipitation, standing |
| | | | water, snow or slush, and |
| | | | c) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
Page 81
Baeatpr6.txt
| | | | |
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| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 77-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 77 ENGINE INDICATING | | | |
| | | | |
| | | | |
| 10-10 NL Indicator B | 2 | 1 | One may be inoperative provided all | |
| | | | other engine indications on the |
| | | | respective engine operate normally. |
| | | | |
| 10-11 NH Indicator B | 2 | 1 | One may be inoperative provided all | |
| | | | other engine indications on the |
| | | | respective engine operate normally. |
| | | | |
| 10-20 Torque Target C | 2 | 1 | | |
| Bugs | | | |
| | | | |
| 20-01 ITT Indicators C | 2 | 2 | Digital counter(s) may be | |
| | | | inoperative. |
| | | | |
| 30-01 Engine Health C | 1 | 0 | | |
| Monitor | | | |
| | | | |
| 40-02 NP Indicators C | 2 | 2 | Digital counter(s) may be | |
Page 82
Baeatpr6.txt
| | | | inoperative. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
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| | | | |
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| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 79-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 79 ENGINE OIL | | | |
| | | | |
| | | | |
| 20-1 Oil Cooler | | | |
| Actuator | | | |
| | | | |
| 1) Pre Mod 35207A A | 4 | 2 | (M)(O)Non-modulating (Manually | |
| | | | Controlled) actuator may be inop- |
| | | | erative on one or both sides |
| | | | provided: |
| | | | a) Failed actuator control |
| | | | circuit breaker is pulled |
| | | | and collared, |
| | | | b) Modulating (Auto Controlled) |
| | | | actuator and its associated |
| | | | controller operate normally, |
| | | | c) Flap valve can be moved from |
| | | | half open to fully closed by |
| | | | the modulating (Auto Con- |
| | | | trolled) actuator. |
| | | | d) Associated oil temperature |
| | | | gauge operates normally, |
| | | | e) High engine power settings |
Page 83
Baeatpr6.txt
| | | | during ground operations are |
| | | | avoided, |
| | | | f) Aircraft shall not be oper- |
| | | | ated in ambient temperatures |
| | | | of ISA + 15 degrees C and |
| | | | above, and |
| | | | g) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | (Continued) |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 79-2 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 79 ENGINE OIL | | | |
| | | | |
| | | | |
| 20-1 Oil Cooler | | | |
| Actuator | | | |
| (Cont'd) | | | |
| | | | |
| 2) Post Mod 35207A A | 2 | 1 | (M)(O)May be inoperative on one |
| | | | side provided: |
| | | | a) Aircraft shall not be oper- |
| | | | ated with the associated |
| | | | flap valve in the 30 degree |
| | | | (closed) position in ambient |
| | | | temperatures of ISA +10 C |
| | | | degrees and above, |
| | | | b) Aircraft shall not be oper- |
| | | | ated with the associated |
| | | | flap valve in the fully open |
| | | | position in ambient tempera- |
| | | | tures of ISA -20 degrees C |
| | | | and below, |
| | | | c) Aircraft shall not be oper- |
| | | | ated with the associated |
| | | | flap valve at any position |
| | | | between the 30 degree |
| | | | (closed) and fully open pos- |
Page 84
Baeatpr6.txt
| | | | tion in ambient temperatures |
| | | | of above ISA +10 degrees C |
| | | | and below ISA -20 degrees C, |
| | | | d) Associated oil temperature |
| | | | gauge operates normally, |
| | | | e) High engine power settings |
| | | | during ground operations are |
| | | | avoided, and |
| | | | f) Operations are limited to |
| | | | not more than three flight |
| | | | days before repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 79-3 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 79 ENGINE OIL | | | |
| | | | |
| | | | |
| 31-1 Engine Oil | | | DELETED, REV 1. |
| Quantity | | | |
| Indicators | | | |
| (Cockpit) | | | |
| | | | |
| 31-2 Engine Low Oil B | 2 | 1 | (O)One may be inoperative provided | |
| Pressure Warning | | | the associated pressure and |
| Lights On CWP | | | temperature gauges operate |
| | | | normally. |
| | | | |
| 32-1 Engine Oil B | 2 | 1 | (M)One may be inoperative provided | |
| Filter Bypass | | | the three associated chip detectors |
| Warning on CWP | | | operate normally. |
| | | | |
| 33-1 Chip Detector B | 2 | 0 | (M)May be inoperative provided: | |
| Indicator System | | | a) Associated engine oil filter |
| | | | warning on CWP is operating |
| | | | normally, and |
| | | | b) Chip detectors are inspected |
| | | | once each flight day. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 85
Baeatpr6.txt
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
| U.S. DEPARTMENT OF TRANSPORTATION |
| |
| MASTER MINIMUM EQUIPMENT LIST |
| FEDERAL AVIATION ADMINISTRATION |
| --------------------------------------------------------------------------- |
| AIRCRAFT: | REVISION NO: 6 | PAGE: |
| | | |
| BAe-ATP | DATE: 10/24/96 | 80-1 |
| --------------------------------------------------------------------------- |
| 1. | 2. NUMBER INSTALLED |
| SYSTEM & | -------------------------------------------- |
| SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH |
| NUMBERS | | --------------------------------------- |
| ------------------------- | | | 4. REMARKS OR EXCEPTIONS |
| 80 STARTING | | | |
| | | | |
| | | | |
| 20-1 Ignition Exiter A | 4 | 3 | May be inoperative provided | |
| Units | | | operations are limited to not more |
| | | | than three flight days before |
| | | | repair is made. |
| | | | |
| 20-2 Ignition Plugs A | 4 | 3 | May be inoperative provided | |
| | | | operations are limited to not more |
| | | | than three flight days before |
| | | | repair is made. |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
Page 86
Baeatpr6.txt
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
| | | | |
-------------------------------------------------------------------------------
Page 87
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