Textron Aviation

European Aviation Safety Agency

Master Minimum Equipment List (MMEL)

Revision: 01
Date: 08/19/2014

Cessna 525
CE/525
(CitationJet, CJ1, CJ1+, M2)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 I
TABLE OF CONTENTS / CONTROL PAGE
SYSTEM PAGES REVISION DATE
-- Cover Page - 01 08/19/2014
-- Signature Page - 01 08/19/2014
-- Table of Contents / Control Page I 01 08/19/2014
-- Highlights of Change II 01 08/19/2014
-- Definitions III thru VII 01 08/19/2014
-- Preamble VIII thru IX 01 08/19/2014
-- Guidelines for (M) & (O) X 01 08/19/2014
Procedures
21 ENVIRONMENTAL CONTROL 21-1 thru 21-10 01 08/19/2014
22 AUTO FLIGHT 22-1 thru 22-7 01 08/19/2014
23 COMMUNICATIONS 23-1 thru 23-8 01 08/19/2014
24 ELECTRICAL POWER 24-1 01 08/19/2014
25 EQUIPMENT/FURNISHINGS 25-1 thru 25-10 01 08/19/2014
26 FIRE PROTECTION 26-1 01 08/19/2014
27 FLIGHT CONTROLS 27-1 01 08/19/2014
28 FUEL 28-1 thru 28-3 01 08/19/2014
30 ICE AND RAIN PROTECTION 30-1 thru 30-3 01 08/19/2014
31 INDICATING / RECORDING 31-1 thru 31-4 01 08/19/2014
SYSTEMS
32 LANDING GEAR 32-1 01 08/19/2014
33 LIGHTS 33-1 thru 33-4 01 08/19/2014
34 NAVIGATION 34-1 thru 34-15 01 08/19/2014
35 OXYGEN 35-1 thru 35-2 01 08/19/2014
38 WATER/WASTE 38-1 01 08/19/2014
45 CENTRAL MAINT. SYSTEM 45-1 01 08/19/2014
46 INFORMATION SYSTEMS 46-1 01 08/19/2014
52 DOORS 52-1 thru 52-3 01 08/19/2014
73 ENGINE FUEL AND CONTROL 73-1 01 08/19/2014
76 ENGINE CONTROLS 76-1 01 08/19/2014
78 ENGINE EXHAUST 78-1 01 08/19/2014

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CESSNA 525 DATE: 08/19/2014 II
HIGHLIGHTS OF CHANGE
NOTE This revision is a reissuance of the CE-525 MMEL. All relief should be considered
changed. This revision is based on the FAA MMEL CE-525 Rev 3A, dated 07 April
2014 with changes appropriate to EASA regulatory policy and the revisions listed
below. This revision incorporates a new numbering system. Items may not be listed
in consecutive order. This is by intention.
ATA 21
-30-02-00A (Units -0800 and on) Revised Remarks and Exceptions.
-30-02-00B (Units -0800 and on) Revised Remarks and Exceptions.
ATA 30
-10-02 Revised Remarks and Exceptions.
-10-04 Added separate relief for Units -0800 and on.
-40-01 Removed serialization.
-40-02 Deleted Windshield Electric Anti-Ice System. Not installed on M2.
-40-02 Removed serialization.
-40-03 Removed serialization.
-70-01 Consolidated drain heaters. Revised relief.
ATA 31
-50-01 Revised serialization.
-50-01-07 (Units -0001 thru -0558) Revised Remarks and Exceptions.
-50-01-07 (Units -0600 thru -0701) Revised serialization.
-50-01-14 Revised serialization.
ATA 32
-41-01 Added NOTE.
ATA 33
-40-10 Revised Remarks and Exceptions.
ATA 38
-30-01 Revised Item and Remarks and Exceptions.
ATA 78
-30-02 Added NOTE.

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CESSNA 525 DATE: 08/19/2014 III
DEFINITIONS
1. ‘Airplane/Rotorcraft Flight Manual’ (AFM/RFM) means the document required for type
certification and approved by the Agency. The AFM/RFM for the specific aircraft is listed on
the applicable Type Certificate Data Sheet.

2. ‘Alternate procedures are established and used’ or similar statement, means that alternate
procedures (if applicable), to the affected process, must be drawn up by the operator as part
of the MEL approval process, so that they have been established before the MEL document
has been approved. Such alternate procedures are normally included in the associated
operations (O) procedure.

3. ‘Any in excess of those required by regulations’ means that the listed item is required by
applicable legislation (e.g. Part OPS, Single European Sky legislation or the applicable
airspace requirements) must be operative and only excess items may be inoperative. When
the item is not required, it may be inoperative for the time specified by its rectification
interval category. Whenever this condition is used in the MMEL, the applicable regulations
for the intended flight routes and the resulting dispatch restrictions need to be clarified at the
operator’s MEL level.

4. ‘As required by (operational) regulations’ means that the listed item of equipment is
subject to certain provisions (restrictive or permissive) expressed in the applicable legislation
(e.g. regulation Air Operations, Single European Sky legislation or the applicable airspace
requirements). When the equipment is not required, it may be inoperative for the time
specified by its rectification interval category.

5. ‘Calendar Day’ means a 24-hour period from midnight to midnight based on either UTC or
local time, as selected by the operator. All calendar days are considered to run consecutively.

6. ‘Combustible Material’ means the material which is capable of catching fire and burning. In
particular: if a MEL item prohibits loading of combustible (or flammable or inflammable)
material, no material may be loaded except the following:

1) Cargo handling equipment (unloaded, empty or with ballast);

2) Fly away kits (excluding e.g. cans of hydraulic fluid, cleaning solvents, batteries,
capacitors, chemical generators, etc.); Note: If serviceable tyres are included, they
should only be inflated to a minimum pressure that preserves their serviceability; and

3) Inflight service material (return catering — only closed catering trolleys/boxes, no

newspapers, no alcohol or duty free goods).

7. ‘Commencement of flight’ is the point when an aircraft begins to move under its own power
for the purpose of preparing for take-off.

8. ‘Considered Inoperative’ as used in the dispatch conditions, means that item must be treated
for dispatch, taxiing and flight purposes as though it were inoperative. The item shall not be

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CESSNA 525 DATE: 08/19/2014 IV
DEFINITIONS
used or operated until the original deferred item is repaired. Additional actions include:
documenting the item on the dispatch release (if applicable), placarding, and complying with
all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures
and observing the rectification interval.

9. ‘Daylight’ means the period between the beginning of morning civil twilight and the end of
evening civil twilight relevant to the local aeronautical airspace; or such other period, as may
be prescribed by the appropriate authority.

10. ‘Day of discovery’ means the calendar day that a malfunction was recorded in the aircraft
maintenance record/log book.

11. ‘Flight’ for the purposes of this MMEL, means the period of time between the moment when
an aircraft begins to move under its own power, for the purpose of preparing for take-off,
until the moment the aircraft comes to a complete stop on its parking area, after the first
landing.

12. ‘Flight Day’, a 24-hour period from midnight to midnight based on either UTC or local time,
as selected by the operator, during which at least one flight is initiated for the affected
aircraft. ‘ETOPS’ or ‘ER operations’ refers to extended range operations of a two engine
airplane as defined by Part-SPA.

13. ‘Icing Conditions’ means an atmospheric environment that may cause ice to form on the
aircraft or in the engine(s) as defined in the AFM/RFM.

14. ‘If installed’ means that the item is either optional or is not required to be installed on all
aircraft covered by the MMEL.

15. ‘Inoperative’ means that the item does not accomplish its intended purpose or is not
consistently functioning within its approved operating limits or tolerances.

16. ‘Is not used’ in the provisions, remarks or exceptions for an MMEL item may specify that
another item relieved in the MMEL ‘is not used’. In such cases, crew members should not
activate, actuate, or otherwise utilise that item under normal operations. It is not necessary for
the operators to accomplish the (M) procedures associated with the item. However,
operations-related provisions, (O) procedures must be complied with. An additional placard
must be affixed, to the extent practical, adjacent to the control or indicator for the item that is
not used to inform crew members that an item is not to be used under normal operations.

17. ‘Intended flight route’ corresponds to any point on the route including diversions to reach
alternate aerodromes required to be selected by the operational rules.

18. ‘Item’ means component, instrument, equipment, system or function.

19. ‘(M)’ indicates a requirement for a specific maintenance procedure which must be

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DEFINITIONS
accomplished prior to operation with the listed item inoperative. Normally these procedures
are accomplished by maintenance personnel, however, other personnel may be qualified and
authorised to perform certain functions. 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.

20. ‘Master Minimum Equipment List’ means a document approved by the Agency that
establishes the aircraft equipment allowed to be inoperative under conditions specified therein
for a specific type of aircraft.

21. ‘Maximum distance from an adequate aerodrome for two-engine aeroplanes’ as defined
in SPA.ETOPS and CAT.OP.AH.140.

22. ‘Minimum Equipment List’ means a document established as specified under 8.a.3. of
Annex IV to Regulation (EC) No 216/2008 and approved by the competent authority, in
accordance with ORO.MLR.105, that authorises an operator to dispatch an aircraft with
aircraft equipment inoperative as per CAT.IDE.A/H.105 or NCC.IDE.A/H.105 under the
conditions specified therein.

23. ‘Night” means the period between the end of evening civil twilight and the beginning of
morning civil twilight relevant to the local aeronautical airspace; or such other period, as may
be prescribed by the appropriate authority. Opposite of ‘Daylight’.

24. ‘Notes’ provide additional information for flight crew 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 dispatch conditions.

25. ‘Number Installed’ 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), or not applicable, a number is not
required; a ‘-’ is then inserted. Note: Where the MMEL shows a variable number installed,
the MEL should reflect the actual number installed, as far as practical.

26. ‘Number required for dispatch’ is the minimum number (quantity) of items required for
operation provided the conditions specified are met. Should the number be a variable (e.g.
passenger cabin items) or not applicable, a number is not required; a ‘-’ is then inserted. Note:
Where the MMEL shows a variable number required for dispatch, the MEL should reflect the
actual number required for dispatch, as far as practical, or an alternate means of configuration
control approved by the competent authority.

27. ‘-’ in the Number Installed Column (respectively Number Required for Dispatch Column)
indicates a variable number (quantity) of the item installed (respectively item required) or not

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CESSNA 525 DATE: 08/19/2014 VI
DEFINITIONS
applicable. Note: Where the MMEL shows a variable number installed, the MEL should
reflect the actual number installed, as far as practical.

28. ‘(O)’ indicates a requirement for a specific operational procedure which must be
accomplished in planning for and/or operating with the listed item inoperative. Normally
these procedures are accomplished by the flight crew; however, other personnel may be
qualified and authorised to perform certain functions. The satisfactory accomplishment of all
procedures, regardless of who performs them, is the responsibility of the operator.
Appropriate procedures are required to be published as a part of the operator’s manual or
MEL. Note: The (M) and (O) symbols are required in the operator’s MEL.

29. ‘Operating minima’ means the set of requirements associated to operations requiring a
specific approval (refer to Part-SPA).

30. ‘Placarding’ Each inoperative item must be placarded, as applicable, to inform and remind
the crew members and maintenance personnel of the item’s 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.

31. ‘Rectification intervals’ Inoperative items or components, deferred in accordance with the
MEL, must be rectified at or prior to the rectification intervals established by the following
letter designators:

Category A

No standard interval is specified. However, items in this category shall be rectified in

accordance with the conditions stated in the MMEL.

(i) Where a time period is specified in calendar days or flight days, the interval excludes the
day of discovery.

(ii) Where a time period is specified other than in calendar days or flight days, it shall start at
the point when the defect is deferred in accordance with the operator’s approved MEL.

Category B

Items in this category shall be rectified within three (3) calendar days, excluding the day of
discovery.
Category C

Items in this category shall be rectified within ten (10) calendar days, excluding the day of
discovery.

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CESSNA 525 DATE: 08/19/2014 VII
DEFINITIONS
Category D

Items in this category shall be rectified within one hundred and twenty (120) calendar days,
excluding the day of discovery.

32. ‘Remarks or Exceptions’ include statements either prohibiting or allowing operation with a
specific number of items inoperative, provisos (conditions and limitations), notes, (M) and/or
(O) symbols, as appropriate for such operation.

33. ‘Required Cabin Crew Seat’ is a seat in the aircraft cabin which meets the following
conditions:

1) Where the certification of the cabin requires this seat to be occupied by a qualified
cabin crew member as specified in the Operations Manual;

2) This seat is a part of the station to which a qualified cabin crew member is assigned
for the flight; and

3) The qualified cabin crew member assigned to the station is a member of the
minimum cabin crew designated for the flight.

34. ‘Visible Moisture’ means an atmospheric environment containing water in any form that can
be seen in natural or artificial light; for example, clouds, fog, mist, rain, sleet, hail, or snow.

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CESSNA 525 DATE: 08/19/2014 VIII
PREAMBLE
Introduction

The following is applicable for operators under European air operations regulations (Regulation
Air Operations). Paragraph 1.c.2 of Annex I to Article 5 (essential requirements for airworthiness)
of Regulation (EC) No 216/2008 (the ‘Basic Regulation’) requires that all equipment installed on
an aircraft required for type certification or by operating rules shall be operative. However,
paragraph 2.a.3 of Annex IV to Article 8 (essential requirements for air operations) of the Basic
Regulation also allows the use 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 items may not be necessary when the remaining operative
equipment can provide an acceptable level of safety.

Purpose and limitations

This Master Minimum Equipment List (MMEL) is developed by the applicant and holders of
(Supplemental) Type Certificate and approved by the European Aviation Safety Agency to
improve aircraft use and thereby providing more convenient and economic air transportation for
the public. This MMEL includes those items related to airworthiness, air operations, airspace
requirements and other items the Agency finds may be inoperative and yet maintain an acceptable
level of safety by appropriate conditions and limitations; it does not contain obviously required
items such as wings, flaps, and rudders. In order to maintain an acceptable level of safety, the
MMEL establishes limitations on the duration of and conditions for operation with inoperative
items. Unless specifically allowed by this MMEL, an inoperative item may not be removed from
the aircraft.

Utilisation

The MMEL is the basis for the development of individual operator’s MEL which take into
consideration the operator’s particular aircraft equipment configuration and operational conditions.
An operator’s MEL may differ in format from the MMEL, but shall not be less restrictive than the
MMEL. The individual operator’s MEL, when approved, allows operation of the aircraft with
inoperative items of equipment for a certain period of time until rectification can be accomplished.

The MEL cannot deviate from Airworthiness Directives, or any other additional mandatory
requirements. It is important to remember that all items related to the airworthiness and the
operational regulations of the aircraft not listed on the MMEL shall be operative.
Suitable conditions and limitations in the form of placards, maintenance procedures, crew
operating procedures and other restrictions as prescribed in this MMEL shall be specified in the
MEL to ensure that an acceptable level of safety is maintained. It is important that rectifications be
accomplished at the earliest opportunity.

When an item is discovered to be inoperative, it is reported by making an entry in the continuing

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CESSNA 525 DATE: 08/19/2014 IX
PREAMBLE
airworthiness record system or the operator’s technical log, as applicable. Following sufficient fault
identification, the item is then either rectified or deferred following the MEL or other approved
means of compliance acceptable to the competent authority and the Agency prior to further
operation. MEL conditions and limitations do not relieve the operator from determining that the
aircraft is in a condition for safe operation with items inoperative.

Prior to operation with any item inoperative acceptance by the crew is required in accordance with
the continuing airworthiness management procedures.

Operators shall establish a controlled and sound rectification programme including the parts,
personnel, facilities, procedures and schedules to ensure timely rectification.

Operators should include guidance in the MEL to deal with any failures which occur between
the commencement of the flight and the start of the take-off.

When developing the MEL, compliance with the stated intent of the preamble, definitions
and the conditions and limitations specified in this MMEL is required.

Multiple inoperative items

Operators are responsible for exercising the necessary operational control to ensure that an
acceptable level of safety is maintained. The exposure to additional failures during continued
operation with inoperative items shall also be considered. Wherever possible, account has been
taken in this MMEL of multiple inoperative items. However, it is unlikely that all possible
combinations of this nature have been accounted for. Therefore, when operating with multiple
inoperative items, the inter-relationships between those items and the effect on aircraft operation
and crew workload shall be considered.

Rectification interval extension

The operator may be permitted, by its competent authority, to extend the rectification intervals of
the MEL.

This MMEL has been evaluated taking into account a one-time extension of the rectification
intervals of category B, C and D.

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CESSNA 525 DATE: 08/19/2014 X
GUIDELINES FOR (M) & (O) PROCEDURES

The OEB has identified a need for certain procedures to provide an adequate level of safety while
providing relief for some items. These procedures must be established by the operator and may be
based on the aircraft manufacturer’s recommended procedures, Supplemental Type Certificate
modifier’s recommended procedures, or equivalent operator procedures. When recommended
procedures are published the operator should comply with these procedures. If recommended
procedures are not published, the following guidelines delineate the aspects to be considered by the
operator in the development of required procedures.

Cessna has developed recommended (M) maintenance and (O) operational procedures for the Cessna
525 Master Minimum Equipment List (P/N 525COMPEU-01-00, or later revision). Operator’s MEL
procedures should be based on the Cessna procedures.

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CESSNA 525 DATE: 08/19/2014 21-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-20-01 Cabin Overhead Air Outlet C - 0

-20-02 Cockpit Overhead Air Outlet C 2 0

-21-06 Glareshield Fan C - 1

(Units -0001 thru -0359
excluding G1000-equipped
aircraft)

-21-06 Glareshield Fan C 2 1 One may be inoperative provided aircraft

(Units -0001 thru -0359 is operated in accordance with G1000
G1000-equipped aircraft) AFM supplement temperature limitations.

-21-06 Glareshield Fan C 2 1 One may be inoperative.

(Units -0360 thru -0701)

-21-07 Instrument Panel Cooling B 2 0 NOTE: Radio service life may be

Fan extended by selecting unused radios
(CNI-5000 communications OFF.
rack)
(Units -0001 thru -0359
excluding G1000-equipped
aircraft and Units -0360 thru
-0558)

-01 FAN 1 Amber Light C 1 0 (M) May be inoperative provided both

cooling fans are verified operative.

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CESSNA 525 DATE: 08/19/2014 21-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-21-08 Nose Avionics Cooling Fan

-01 Radome Bulkhead C 1 0 May be inoperative provided aircraft is

(RH FS 43) operated in accordance with AFM NOSE
(Units -0001 thru -0359 AVIONICS COOLING FAN abnormal
excluding G1000-equipped procedure.
aircraft)

-01 Radome Bulkhead C 1 0 May be inoperative provided aircraft is

(RH FS 43) operated in accordance with G1000 AFM
(Units -0001 thru -0359 supplement temperature limitations.
G1000-equipped aircraft)

-01 Radome Bulkhead C 1 0 May be inoperative provided ground

(LH FS 43) operations with avionics ON are limited to
(Units -0360 and on) 30 minutes.

-02 Vaneaxial Snorkel C 1 0

(MN001)
(Units -0001 thru -0359)

-21-10 Ported Cooling Fan

-01 Radio C 1 0 May be inoperative provided aircraft is

(KA 33 Panel Fan) operated in accordance with G1000 AFM
(Units -0001 thru -0359 supplement temperature limitations.
G1000-equipped aircraft)

-02 Integrated Avionics Unit C 2 1 May be inoperative provided aircraft is

(GIA FAN 1/2) operated in accordance with G1000 AFM
(Units -0001 thru -0359 supplement temperature limitations.
G1000-equipped aircraft)

-21-11 Display Fan C 3 0 May be inoperative provided aircraft is

(Units -0001 thru -0359 operated in accordance with G1000 AFM
G1000-equipped aircraft) supplement temperature limitations.

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CESSNA 525 DATE: 08/19/2014 21-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-30-01 Cabin Dump Function C 1 0 (M) May be inoperative provided:
(Unpressurized) a) One outflow valve is removed,
and
b) Cabin pressurization system is
considered inoperative (Refer to
item 21-30-02).

-30-02 Cabin Pressurization

System

-00A (Unpressurized with cabin C 1 0 (O) May be inoperative provided:

occupants) a) PRESS SYSTEM SELECT is
(Units -0001 thru -0558) selected to MANUAL,
b) CABIN DUMP is selected ON,
c) Aircraft is operated at 10,000 feet
cabin altitude or below, and
d) Flight crew oxygen system is used
as required by operating rule.

NOTE: CAB ALT 10,000 FT red

annunciator may illuminate at 10,000 feet
cabin altitude.

-00A (Unpressurized with cabin C 1 0 (O) May be inoperative provided:

occupants) a) PRESS SYSTEM SELECT is
(Units -0600 thru -0701) selected to MANUAL,
b) CABIN DUMP is selected ON,
c) Aircraft is operated at 10,000 feet
cabin altitude or below, and
d) Flight crew oxygen system is used
as required by operating rule.

NOTE: CABIN ALT red annunciator may

illuminate at 10,000 feet cabin altitude.

(Continued)

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CESSNA 525 DATE: 08/19/2014 21-4
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-30-02 Cabin Pressurization
System
(Continued)

-00A (Unpressurized with cabin C 1 0 (O) May be inoperative provided:

occupants) a) PRESSURIZATION is selected to
(Units -0800 and on) STBY,
b) CABIN DUMP is selected ON,
c) Aircraft is operated at 10,000 feet
cabin altitude or below, and
d) Flight crew oxygen system is used
as required by operating rule.

NOTE: PRESSURIZATION CTRL amber

message may appear. CABIN ALTITUDE
red message may appear and CABIN
ALTITUDE aural warning may sound at
9,500 feet cabin altitude.

-00B (Unpressurized without C 1 0 (O) May be inoperative provided:

cabin occupants) a) PRESS SYSTEM SELECT is
(Units -0001 thru -0558) selected to MANUAL,
b) CABIN DUMP is selected ON,
c) OXYGEN CONTROL VALVE is
selected to CREW ONLY,
d) No cabin occupants are carried,
e) Aircraft is operated at FL250 or
below, and
f) Flight crew oxygen system is used
as required by operating rule.

NOTE: CAB ALT 10,000 FT red

annunciator may illuminate at 10,000 feet
cabin altitude.

(Continued)

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CESSNA 525 DATE: 08/19/2014 21-5
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-30-02 Cabin Pressurization
System
(Continued)

-00B (Unpressurized without C 1 0 (O) May be inoperative provided:

cabin occupants) a) PRESS SYSTEM SELECT is
(Units -0600 thru -0701) selected to MANUAL,
b) CABIN DUMP is selected ON,
c) OXYGEN CONTROL VALVE is
selected to CREW ONLY,
d) No cabin occupants are carried,
e) Aircraft is operated at FL250 or
below, and
f) Flight crew oxygen system is used
as required by operating rule.

NOTE: CABIN ALT red annunciator may

illuminate at 10,000 feet cabin altitude.

-00B (Unpressurized without C 1 0 (O) May be inoperative provided:

cabin occupants) a) PRESSURIZATION is selected to
(Units -0800 and on) STBY,
b) CABIN DUMP is selected ON,
c) OXYGEN CONTROL VALVE is
selected to CREW ONLY,
d) No cabin occupants are carried,
e) Aircraft is operated at FL250 or
below, and
f) Flight crew oxygen system is used
as required by operating rule.

NOTE: PRESSURIZATION CTRL amber

message may appear. CABIN ALTITUDE
red message may appear and CABIN
ALTITUDE aural warning may sound at
9,500 feet cabin altitude.

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CESSNA 525 DATE: 08/19/2014 21-6
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-30-03 Emergency Pressurization C 1 0 (O) May be inoperative provided:
System a) Emergency pressurization valve is
(Failed closed) verified closed, and
b) Aircraft is operated at FL250 or
below.

-31-02 Cabin Pressurization

System Mode

-01 Automatic Schedule Mode C 1 0 May be inoperative provided:

(Units -0001 thru -0701) a) Isobaric mode is operative,
b) Cabin differential pressure gauge /
indication is operative,
c) Cabin altitude gauge / indication is
operative, and
d) Cabin vertical speed gauge /
indication is operative.

-01 Automatic Schedule Mode C 1 0 May be inoperative provided cabin

(NORM) pressurization system is considered
(Units -0800 and on) inoperative (Refer to item 21-30-02).

-03 Isobaric Mode C 1 0 May be inoperative provided automatic

(Units -0001 thru -0701) schedule mode is operative.

-04 Any Mode C 2 0 May be inoperative provided cabin

(Excluding manual) pressurization system is considered
(Units -0001 thru -0701) inoperative (Refer to item 21-30-02).

-04 Any Mode C 1 0 May be inoperative provided cabin

(Excluding manual) pressurization system is considered
(Units -0800 and on) inoperative (Refer to item 21-30-02).

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 21-7
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-32-01 Cabin Altitude
Gauge/Indication

-00A (Pressurized) C 1 0 (O) May be inoperative provided:

a) Cabin pressurization system
automatic schedule mode is
operative and used,
b) Cabin differential pressure
gauge/indication is operative, and
c) A chart is provided to convert
differential pressure and aircraft
altitude to cabin altitude.

-00B (Unpressurized) C 1 0 May be inoperative provided cabin

pressurization system is considered
inoperative (Refer to item 21-30-02).

-01 Gauge Lighting C 1 0 May be inoperative provided flight crew

(Units -0001 thru -0701) determines adequate natural or artificial
lighting exists to read gauge.

-32-02 Cabin Differential Pressure

Gauge/Indication

-00A (Pressurized) C 1 0 (O) May be inoperative provided:

a) Cabin pressurization system
automatic schedule mode is
operative and used,
b) Cabin altitude gauge/indication is
operative, and
c) A chart is provided to convert
cabin and aircraft altitude to
differential pressure.

-00B (Unpressurized) C 1 0 May be inoperative provided cabin

pressurization system is considered
inoperative (Refer to item 21-30-02).

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 21-8
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-32-03 Cabin Vertical Speed
Gauge/Indication

-00A (Pressurized) C 1 0 May be inoperative provided:

a) Cabin pressurization system
automatic schedule mode is
operative and used, and
b) Cabin altitude gauge/indication is
operative.

-00B (Unpressurized) C 1 0 May be inoperative provided cabin

pressurization system is considered
inoperative (Refer to item 21-30-02).

-33-01 Cabin Outflow Valve C 2 0 (M) May be inoperative provided:

a) One outflow valve is removed,
and
b) Cabin pressurization system is
considered inoperative (Refer to
item 21-30-02).

-50-02 Vapor-cycle Air Conditioning C 1 0 (M) May be inoperative provided:

System a) Air conditioning system is
deactivated,
b) Cabin and cockpit temperature
control systems are operative,
c) All glareshield fans are operative,
and
d) Aircraft is operated in accordance
with AFM temperature limitations.

-01 Compressor Hour Meter C 1 0 (O) May be inoperative provided

*** compressor hours are tracked by
alternate means.

-02 Compressor Light C 1 0

(COMPRESSOR ON)
(Units -0001 thru -0701)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 21-9
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-50-03 Evaporator Fan

-05 Forward C 1 0 (M) May be inoperative provided:

(FWD) a) Aft evaporator fan is operative,
(Units -0001 thru -0359 b) Forward evaporator fan is
excluding G1000-equipped deactivated,
aircraft and Units -0360 and c) DEFOG FAN is selected OFF,
on) d) Windshield anti-ice system is
operative, and
e) Crew has a means to clear the
windshield of moisture.

-05 Forward C 1 0 (M) May be inoperative provided:

(FWD) a) Aft evaporator fan is operative,
(Units -0001 thru -0359 b) Forward evaporator fan is
G1000-equipped aircraft) deactivated,
c) DEFOG FAN is selected OFF,
d) Windshield anti-ice system is
operative,
e) Crew has a means to clear the
windshield of moisture, and
f) Aircraft is operated in accordance
with G1000 AFM supplement
temperature limitations with air
conditioning off.

-06 Aft C 1 0 (M) May be inoperative provided:

(AFT) a) Forward evaporator fan is
operative,
b) Aft evaporator fan is deactivated,
and
c) Cockpit and cabin temperature
control system manual mode is
operative and used.

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 21-10
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENVIRONMENTAL
21
CONTROL
-60-01 Cockpit and Cabin C 2 0 May be inoperative provided cabin
Temperature Control pressurization system is considered
System inoperative (Refer to item 21-30-02).

-01 Automatic Mode C 1 0 May be inoperative provided temperature

control system manual mode is operative
and used.

-02 Manual Mode C 1 0 May be inoperative provided temperature

control system automatic mode is
operative and used.

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 22-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

-10-01 Autopilot Disconnect Button

(AP TRIM DISC)
(Failed deselected)
(Units -0001 thru -0359
excluding G1000-equipped
aircraft)

-10-01 Autopilot Disconnect Button

(AP YD DISC/TRIM INT)
(Failed deselected)
(Units -0001 thru -0359
G1000-equipped aircraft)

-10-01 Autopilot Disconnect Button

(AP TRIM DISC)
(Failed deselected)
(Units -0360 thru -0701)

-10-01 Autopilot Disconnect Button

(AP DISC)
(Failed deselected)
(Units -0800 and on)

-00A Left Control Wheel B 1 0 May be inoperative provided:

a) Right control wheel button is
operative,
b) Pilot remains seated in right seat
with seat belt fastened during all
autopilot operations,
c) Autopilot system is not used
below AFM cruise minimum use
height, and
d) Approach minimums do not
require use of autopilot system.

-00B Right Control Wheel C 1 0 May be inoperative for single-pilot

operations.

(Continued)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 22-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

-10-01 Autopilot Disconnect Button

(Failed deselected)
(Continued)

-00C (All buttons failed) B 2 0 May be inoperative provided:

a) Autopilot system is considered
inoperative (Refer to item 22-10-
03), and
b) Electric elevator trim is considered
inoperative (Refer to item 27-31-
01).

-10-02 Autopilot Interrupt/Flight C 2 0

Director Sync Button
(A/P TCS)
(Units -0001 thru -0359
excluding G1000-equipped
aircraft)

-10-02 Autopilot Interrupt/Flight C 2 0

Director Sync Button
(A/P CWS)
(Units -0001 thru -0359
G1000-equipped aircraft)

-10-02 Autopilot Interrupt/Flight C 2 0

Director Sync Button
(A/P TCS)
(Units -0360 thru -0558)

-10-02 Autopilot Interrupt/Flight C 2 0

Director Sync Button
(A/P SYNC)
(Units -0600 thru -0701)

-10-02 Autopilot Interrupt/Flight C 2 0

Director Sync Button
(CWS)
(Units -0800 and on)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 22-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

-10-03 Autopilot System B 1 0 (M) May be inoperative provided:

a) Autopilot system is deactivated,
b) Enroute procedures and approach
minimums do not require use of
autopilot system,
c) Cabin pressurization system is not
operated in manual mode,
d) Aircraft is not operated RVSM,
e) Aircraft is not operated single-
pilot, and
f) Yaw damper is considered
inoperative (Refer to item 22-10-
05).

-10-04 Takeoff/Go-Around Button C 1 0 May be inoperative provided:

(GA) a) Flight director is not used during
takeoff or go-around,
b) Autopilot system is disconnected
for go-around, and
c) Autopilot interrupt/flight director
sync button is operative on pilot
flying side.

NOTE: FMS missed approach procedure

must be manually advanced.

-10-05 Yaw Damper B 1 0 (M) May be inoperative provided:

(Units -0001 thru -0701) a) Yaw damper is deactivated, and
b) Autopilot system is considered
inoperative (Refer to item 22-10-
03).

-10-05 Yaw Damper B 1 0 (M) May be inoperative provided:

(Units -0800 and on) a) Yaw damper is deactivated,
b) Autopilot system is considered
inoperative (Refer to item 22-10-
03), and
c) Aircraft is operated at FL280 or
below.

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 22-4
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

-13-03 Flight Guidance Controller

Annunciator
(GMC 710)
(Failed to illuminate)
(Units -0001 thru -0359
G1000-equipped aircraft
and Units -0800 and on)

-01 Altitude C 1 0 May be inoperative provided appropriate

(ALT button) annunciation appears in PFD flight
director mode box.

-03 Approach C 1 0 May be inoperative provided appropriate

(APR button) annunciation appears in PFD flight
director mode box.

-04 Autopilot C 1 0 May be inoperative provided AP

(AP button) annunciation appears in PFD flight
director mode box.

-05 Back Course C 1 0 May be inoperative provided appropriate

(BC button) annunciation appears in PFD flight
director mode box.

-07 Coupled Side C 2 0 May be inoperative provided associated

(XFR Button - left or right green coupled arrow appears in PFD
arrow) flight director mode box.

-09 Flight Level Change C 1 0 May be inoperative provided appropriate

(FLC button) annunciation appears in PFD flight
director mode box.

-10 Half Bank C 1 0 May be inoperative provided green bank

(BANK button) limit arc appears on PFD attitude display.

(Continued)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 22-5
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

-13-03 Flight Guidance Controller

Annunciator
(Continued)

-11 Heading C 1 0 May be inoperative provided appropriate

(HDG button) annunciation appears in PFD flight
director mode box.

-12 Navigation C 1 0 May be inoperative provided appropriate

(NAV button) annunciation appears in PFD flight
director mode box.

-13 Vertical Navigation C 1 0 May be inoperative provided appropriate

(VNV button) annunciation appears in PFD flight
director mode box.

-14 Vertical Speed C 1 0 May be inoperative provided appropriate

(VS button) annunciation appears in PFD flight
director mode box.

-15 Yaw Damper C 1 0 May be inoperative provided YD

(YD button) annunciation appears in PFD flight
director mode box.

-13-04 Flight Guidance Controller

Function Control
(GMC 710)
(Units -0001 thru -0359
G1000-equipped aircraft
and Units -0800 and on)

-02 Approach B 1 0 May be inoperative provided procedures

(APR button) do not require its use.

-03 Autopilot B 1 0 May be inoperative provided autopilot

(AP button) system is considered inoperative (Refer
to item 22-10-03).

(Continued)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 22-6
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

-13-04 Flight Guidance Controller

Function Control
(Continued)

-04 Back Course C 1 0 May be inoperative provided procedures

(BC button) do not require its use.

-05 IAS/Mach Change-over D 1 0

(SPD Button)

-06 Coupled Side C 1 0 May be inoperative provided arrow points

(XFR button) to pilot-flying side.

-07 Course B 2 1 One may be inoperative provided

(CRS1 or CRS2 knob) procedures do not require its use.

-08 Course Direct C 2 0

(CRS1 or CRS2 PUSH DIR)

-10 Flight Level Change C 1 0 May be inoperative provided procedures

(FLC button) do not require its use.

-11 Half Bank C 1 0

(BANK Button)

-13 Heading Sync C 1 0

(HDG PUSH SYNC)

-14 Navigation B 1 0 May be inoperative provided procedures

(NAV Button) do not require its use.

-16 Vertical Navigation C 1 0 May be inoperative provided procedures

(VNV button) do not require its use.

-17 Vertical Speed C 1 0 May be inoperative provided procedures

(VS button) do not require its use.

(Continued)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 22-7
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT

-13-04 Flight Guidance Controller

Function Control
(Continued)

-18 Yaw Damper C 1 0 NOTE 1: Yaw damper may be engaged

(YD Button) by engaging autopilot.

NOTE 2: Yaw damper may be

disengaged by pressing autopilot
disconnect button.

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 23-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

-00-01 Flight Phone / SATCOM D - 0 May be inoperative provided procedures

*** System do not require its use.

-01 Cockpit Handset D - 0 May be inoperative provided procedures

do not require its use.

-02 Cabin Handset D - 0

-10-01 High Frequency (HF)

*** Communication System

-00A (Dual LRCS not required) D - - Any in excess of those required by

operating rule may be inoperative.

-00B (Dual LRCS required) C - 1 (O) Any in excess of one may be

inoperative while conducting operations
which require two Long-Range
Communication Systems (LRCS)
provided:
a) SATCOM voice or data link
operates normally,
b) Alternate procedures are
established and used,
c) SATCOM coverage is available
over intended route of flight, and
d) If SATCOM voice is to be used
over intended route of flight,
SATCOM voice short codes
(INMARSAT) or direct dial
commercial numbers (IRIDIUM)
must be available, prior
coordination with appropriate ATS
(FIR) facility is required.

NOTE: SATCOM voice is to be used only

as a backup to normal HF
communications.

(Continued)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 23-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

-10-01 High Frequency (HF)

Communication System
(Continued)

-00C A - 1 (O) Any in excess of one may be

inoperative provided:
a) Alternate communication
procedures are established and
used, and
b) Repairs are made within three
calendar days.

-01 Wire Antenna C 1 0 (M) May be inoperative, missing, or

damaged provided:
a) Horizontal and vertical stabilizers
are inspected for damage,
b) Any remaining portion of wire
antenna is removed, and
c) HF communication system is
considered inoperative (Refer to
item 23-10-01).

-12-01 Very High Frequency (VHF)

Communication System

-00A (Operator other than a D - - Any in excess of those required by

holder of an air carrier, or operating rule may be inoperative
commercial operator provided:
certificate) a) Affected system is not on an
emergency bus, and
b) Procedures do not require its use.

(Continued)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 23-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

-12-01 Very High Frequency (VHF)

Communication System
(Continued)

-00B (Holder of an air carrier, or C - 1 (O) May be inoperative provided:

commercial operator a) Affected system is not on an
certificate) emergency bus,
b) Operations are conducted under
VFR over routes navigated by
reference to visual landmarks,
c) Applicable airspace requirements
for the intended flight route are
complied with, and
d) Alternate procedures are
established and used, if
applicable.

-01 VHF Datalink (VDL) D - 0 May be inoperative provided procedures

*** (Units -0800 and on) do not require its use.

-20-01 Satellite Datalink Service

***

-01 Radio D - 0

-02A Weather D - 0 May be inoperative provided procedures

do not require its use.

NOTE: Any function(s) that operate

normally may be used.

-02B Weather C - 0 (O) May be inoperative provided alternate

procedures are established and used.

-03 Internet D - 0

-20-02 Ground D 1 0
Avionics/Diagnostics Wi-Fi
System
(Units -0800 and on)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 23-4
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

-20-03 Selective Call (SELCAL)

*** (System or individual
channel)

-00A (SELCAL not required) D - 0 May be inoperative provided procedures

do not require its use.

-00B (SELCAL required) C - 0 (O) May be inoperative provided alternate

procedures are established and used.

-20-04 SMS Text Message System D 1 0

*** (Units -0800 and on)

-40-01 Automatic Cabin Briefer D 1 0

***

-40-03 Passenger Address (PA) D 1 0 May be inoperative provided procedures

System do not require its use.

-40-04 Passenger Seat Belt / C 1 0 (O) May be inoperative provided cabin

Safety Chime occupants are briefed by alternate
means.

-50-01 Audio Panel C 2 1 Right side panel may be inoperative

(Units -0001 thru -0701) provided aircraft is operated single-pilot.

-02 Audio Selector / Volume C - - Individual selectors may be inoperative

Control provided associated system is not
(COM 1, COM 2, COM3, required by procedures or operating rule.
NAV 1, NAV 2, ADF 1, ADF
2, DME, MKR Button)
(Per side)
(Units -0001 thru -0359
G1000-equipped aircraft)

(Continued)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 23-5
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

-50-01 Audio Panel

(Continued)

-03 Marker Beacon Mute C 1 0

(MKR/MUTE Button)
(Per side)
(Units -0001 thru -0359
G1000-equipped aircraft)

-04 Intercom D 1 0 May be inoperative provided aircraft is

(INTR COM Button) operated single-pilot.
(Per side)
(Units -0001 thru -0359
G1000-equipped aircraft)

-05 Cabin Communication D 1 0

(CABIN Button)
(Per side)
(Units -0001 thru -0359
G1000-equipped aircraft)

-06 Clearance Playback D 1 0

(PLAY Button)
(Per side)
(Units -0001 thru -0359
G1000-equipped aircraft)

-07 Marker Beacon High D 1 0 May be inoperative provided approach

Sensitivity procedures do not require its use.
(HI SENS Button)
(Per side)
(Units -0001 thru -0359
G1000-equipped aircraft)

(Continued)

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 23-6
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

-50-01 Audio Panel

(Continued)

-08 Microphone Selector C 2 0 May be inoperative provided crew refers

Annunciator to PFD frequency box for active transmit
(COM1 MIC, COM2 MIC frequency (shown in green).
Annunciator)
(Per side)
(Units -0001 thru -0359
G1000-equipped aircraft)

-50-05 Cockpit Headset and Boom D - - Any in excess of one headset (including
Microphone boom microphone) for each required crew
member on flight crew compartment duty
may be inoperative or missing.

-03 Active Noise Reduction D - 0 May be inoperative provided normal

*** (ANR) Function audio function of headset is operative.

-04 Powered Headset System D - 0 May be inoperative provided non-

(Units -0800 and on) powered headset jack is operative or
headset is not used.

-50-06 Cockpit Headset Audio

System

-00A C 2 0 May be inoperative provided:

a) Both cockpit overhead
communication speakers are
operative and used,
b) Headset audio system is not
required by operating rule or
procedures, and
c) Aircraft is not operated single-
pilot.

-00B C 2 1 One may be inoperative provided left side

is operative for single-pilot operations.

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 23-7
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

-50-07 Push-to-talk (PTT) Switch

(Failed deselected)

-01 Yoke Switch B 2 1 (O) One may be inoperative provided

alternate procedures are established and
used for transmitting.

-01A Right Yoke Switch B 1 0 May be inoperative provided aircraft is

operated single-pilot.

-60-01 Static Wick NOTE: May include mounting base

provided no damage exists to attaching
structure.

-01 Aileron C 2 1 One may be damaged or missing

(Each side) provided outermost wick is installed and
not damaged.

-02 Wing Tip Assembly - 1 1 NOTE: Wing tip assembly is entire

(Each side) removable section outboard of fuel
(Units -0001 thru -0701) closure rib.

-05 Elevator C 3 1 Two may be damaged or missing

(Each side) provided outermost wick is installed and
not damaged.

-08 Rudder C 2 1 One may be damaged or missing

provided uppermost wick is installed and
not damaged.

-09 Stinger - 1 1

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MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 23-8
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS

-70-01 Cockpit Voice Recorder

(CVR)

-00A A 1 0 May be inoperative provided:

a) Any Flight Data Recorder (FDR)
required to be installed is
operative, and
b) Repairs are made within 72 hours
since CVR was found to be
inoperative or eight flights,
whichever occurs first.

-00C C 1 0 May be inoperative provided recorder is

*** not required by operating rule.

-01 Recorder Independent C 1 0

*** Power Supply (RIPS)

-03A Datalink Recording C 1 0 May be inoperative provided datalink

recording is not required by operating
rule.

-03B Datalink Recording A 1 0 May be inoperative provided repairs are

made within three flight days.

525MMELEU-01
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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 24-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER

-22-01 AC Inverter B 2 1 One may be inoperative provided:

(Units -0001 thru -0099 a) AC INV is selected to operative
excluding G1000-equipped inverter,
aircraft) b) Aircraft is not operated at night,
and
c) Aircraft is not operated IFR.

-22-01 AC Inverter B 2 1 One may be inoperative provided:

(Units -0100 thru -0359 a) INV is selected to operative
excluding G1000-equipped inverter,
aircraft) b) Aircraft is not operated at night,
and
c) Aircraft is not operated IFR.

-31-02 Battery Temperature C 1 0

*** Indicator

-40-01 External Power System D 1 0

-50-01 AC Cockpit Outlet

***

-00A (Outlet not required) D - 0 May be inoperative provided procedures

do not require its use.

-00B (Outlet required) C - 0 (O) May be inoperative provided alternate

procedures are established and used.

-60-01 DC Cockpit Outlet

***

-00A (Outlet not required) D - 0 May be inoperative provided procedures

do not require its use.

-00B (Outlet required) C - 0 (O) May be inoperative provided alternate

procedures are established and used.

-60-02 Ground Dispatch Power C 1 0

*** System

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-00-01 Required Documents Holder D 1 0 (O) May be inoperative or missing
(Airworthiness Certificate, provided an alternate means of securing
Registration, etc) and displaying documents is used.

-10-01 Cockpit Assist Handle D 1 0

-10-03 Cockpit Sunvisor System D - 0 May be inoperative or missing provided:

(Including attach a) Crewmember’s field of vision is
mechanism) not obstructed, and
b) Oxygen mask quick donning
ability is not affected.

-10-05 Flight Crew Seat

(Per seat)

-01A Armrest C 2 0 May be inoperative provided affected

armrest is stowed in retracted position.

-01B Armrest C 2 0 (M) May be inoperative provided affected

armrest is removed.

-02 Lumbar Support D 1 0

***

-03 Recline/Tilt Function B 1 0 (M) (O) May be inoperative provided:

a) Affected seat is secured in a
position that permits normal
visibility,
b) Full flight control movement is
available, and
c) Crewmember can reach all
necessary controls and equipment
while restrained.

-04 Restraint Buckle Protective D 1 0 May be damaged or missing.

*** Padding

(Continued)

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-10-05 Flight Crew Seat
(Per seat)
(Continued)

-06 Vertical Adjustment B 1 0 (M) (O) May be inoperative provided:

a) Affected seat is secured in a
position that permits pilot normal
visibility,
b) Full flight control movement is
available, and
c) Crewmember can reach all
necessary controls and equipment
while restrained.

-07 Copilot Seat Belt / Shoulder C 1 0 May be inoperative provided seat remains
Harness unoccupied.

-08 Copilot Floor Tracking C 1 0 May be inoperative provided seat remains

unoccupied.

-10-08 Eye Reference Ball C 3 0 (O) May be inoperative or missing

provided alternate procedures are
established and used for eye position
reference.

-10-09 Yoke-mounted Chart Holder D - 0

***

-01 Light D - 0
***

-20-01 Cabin Ashtray A - 1 May be inoperative or missing provided

*** (Excluding lavatory door) ashtray is replaced within three calendar
days.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-20-02 Belted Lavatory Seat
*** (Excludes lavatory waste
system)

-01 Seat Belt / Shoulder D 1 0 May be inoperative provided lavatory seat

Harness is placarded "DO NOT OCCUPY FOR
TAXI, TAKEOFF, LANDING OR WHEN
FASTEN SEAT BELT SIGN IS
ILLUMINATED”.

-02 Seat Belt / Shoulder D 1 0

*** Harness Keeper

-20-05 Passenger Convenience D - 0 Passenger convenience itesm, as

Items expressed in this MMEL, are those
related to passenger convenience,
comfort or entertainment such as, but not
limited to, galley equipment, movie
equipment, ashtrays, 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 operator’s appropriate document.

NOTE: Lavatory door ashtray is not

considered a passenger convenience
item.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-4
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-20-06 Passenger Seat D - 0 May be inoperative provided:
(Including side-facing seats, a) Seat does not block an
folding seats and couches) emergency exit,
(Per seat) b) Seat does not restrict any cabin
occupant access to aisle, and
c) Affected seat(s) are blocked and
placarded “DO NOT OCCUPY”.

NOTE: Affected seat(s) may include

seats near the inoperative seat(s).

-01A Armrest D - 0 May be missing, damaged or inoperative

(With seat controls) with seat occupied provided:
a) Armrest does not block an
emergency exit,
b) Armrest does not restrict any
cabin occupant from access to
aisle, and
c) If armrest is missing, affected seat
controls are considered
inoperative (Refer to item 25-20-
06-02).

-01B Armrest D - 0 (M) May be missing, damaged or

(Without seat controls) inoperative with seat occupied provided:
a) Armrest does not block an
emergency exit, and
b) Armrest does not restrict any
cabin occupant from access to
aisle.

(Continued)

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-5
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-20-06 Passenger Seat
(Including side-facing,
folding seats and couches)
(Per seat)
(Continued)

-02A Seat Controls D - 0 (M) May be inoperative with seat

(Includes recline, headrest, occupied provided seat is secured in taxi,
footrest, floor tracking, takeoff and landing position.
pedestal tracking, swivel,
and other positioning
controls)

-02B Seat Controls C - 0 May be inoperative with seat occupied

(Includes recline, headrest, provided control is failed in taxi, takeoff
footrest, floor tracking, and landing position.
pedestal tracking, swivel,
and other positioning
controls)

-02C Seat Controls D - 0 May be missing or inoperative in other

(Includes recline, headrest, than taxi, takeoff, and landing position
footrest, floor tracking, provided affected seat is considered
pedestal tracking, swivel, inoperative (Refer to item 25-20-06).
and other positioning
controls)

-03 Seat Belt / Shoulder D - 0 May be inoperative provided affected seat

Harness is placarded "DO NOT OCCUPY FOR
TAXI, TAKEOFF, LANDING OR WHEN
FASTEN SEAT BELT SIGN IS
ILLUMINATED".

-04 Seat Belt / Shoulder D 1 0

*** Harness Keeper

-05 Lumbar Support D 1 0

***

525MMELEU-01
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MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-6
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-30-01 Refreshment Center Hot C - 0 (M) May be inoperative provided system
*** Liquid Storage System is deactivated.
Heater

-50-01 Baggage Restraint System D - 0 Individual components may be

inoperative or missing provided baggage
is secured by other means or not carried.

-01A Anchor Plate C - 0 Individual anchor plates may be

inoperative provided:
a) No visible damage exists, and
b) Baggage is secured using
remaining anchor plates or not
carried.

-01B Anchor Plate C - 0 (M) Individual anchor plates may be

damaged provided:
a) Attaching structure is inspected
for damage, and
b) Baggage is secured using
remaining anchor plates or not
carried.

525MMELEU-01
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MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-7
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-50-02 Cabin Storage
Compartment

-00A C - 0 (M) May be inoperative provided:

a) Compartment does not contain
any aircraft system protection
devices,
b) Any emergency equipment
located in affected compartment is
considered inoperative,
c) Affected compartment is not used
for storage of any item except for
those permanently affixed,
d) Procedures are established and
used to secure compartment
closed, and
e) Affected compartment is
prominently placarded "DO NOT
USE".

-00B C - 0 (M) (O) May be inoperative provided:

a) Affected door is removed,
b) Affected compartment is not used
for storage of any item, except
those permanently affixed,
c) Cabin occupants are briefed that
affected compartment may not be
used, and
d) Affected compartment is
prominently placarded “DO NOT
USE”.

NOTE: Any permanently affixed

emergency equipment located in affected
compartment is available for use.

(Continued)

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-8
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-50-02 Cabin Storage
Compartment
(Continued)

-01 Shelving D - 0 (O) May be inoperative provided:

a) Any permanently affixed
emergency equipment located on
affected shelf is relocated and
available for use, and
b) Cabin occupants are briefed on
location of relocated equipment.

-02 Key Lock D - 0 May be inoperative in unlocked position.

***

-60-03 Emergency Medical

Equipment

-01 Automatic External D - 0

*** Defibrillator (AED)
(Includes associated
equipment)

-02 Emergency Medical Kit D - 0

*** (EMK)
(Includes associated
equipment)

-03 First Aid Kit (FAK) D - - Any in excess of those required by

*** (Includes associated operating rule may be incomplete,
equipment) missing, or inoperative.

525MMELEU-01
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MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-9
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-61-01 Life Preserver D - - Any in excess of those required by
*** (Crew and passenger) operating rule may be missing, or
inoperative provided:
a) Inoperative preserver is placarded
“INOPERATIVE”, removed from
installed location, and placed out
of sight so it cannot be mistaken
for a functional unit, and
b) Location placarding is removed or
obscured.

-62-01 Emergency Locator

Transmitter (ELT)

-01 Survival Type D - - Any in excess of those required by

*** operating rule may be missing, or
inoperative provided:
a) Inoperative ELT is placarded
“INOPERATIVE”, removed from
installed location, and placed out
of sight so it cannot be mistaken
for a functional unit, and
b) Location placarding is removed or
obscured.

-02A Fixed, Automatic A - 0 (M) May be inoperative provided:

a) System is deactivated or
removed, and
b) Repairs are made within six flights
or 25 flight hours, whichever
occurs first..

-02B Fixed, Automatic D - - (M) Any in excess of those required by

operating rule may be inoperative
provided system is deactivated or
removed.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 25-10
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
EQUIPMENT /
25
FURNISHINGS
-64-01 Life Raft D - - Any in excess of those required by
*** operating rule may be missing, or
inoperative provided affected raft is
placarded “INOPERATIVE” or removed.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 26-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION

-22-01 Portable Fire Extinguisher D - - Any in excess of those required by

operating rule may be inoperative or
missing provided:
a) Inoperative fire extinguisher is
placarded "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.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 27-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS

-20-01 Rudder Pedal Adjustment B 4 2 (M) (O) Two may be inoperative provided:
System a) Two pedal adjustments are not
inoperative at same pilot station,
b) Affected pedal is positioned in a
detent and adjustment mechanism
is secured from movement,
c) Unaffected pedal is adjusted to
match affected pedal, and
d) Crewmember seated at affected
station verifies full control
movement and brake application
is available while restrained, prior
to each flight.

-31-01 Electric Elevator Trim B 1 0 (M) May be inoperative provided:

a) Electric elevator trim system is
deactivated,
b) Manual trim is verified to operate
normally, and
c) Autopilot system is considered
inoperative (Refer to item 22-10-
03).

-70-02 Control / Gust Lock System C 1 0 (O) May be inoperative provided pilot
(Failed unlocked) verifies full flight control and throttle
movement.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 28-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

-10-01 Over-wing Refueling Cap D - 0

Lock
(Failed unlocked)

-41-01 Fuel Low Level Indicating A 2 1 (O) One may be inoperative provided:
System a) Procedures for monitoring fuel
quantity are established and used,
b) Both fuel quantity indicating
systems are operative, and
c) Repairs are made within three
flight days.

-41-02 Fuel Quantity Indicating A 2 1 (O) One indication may be inoperative

System provided:
(Wing tank) a) Both fuel low level indicating
(Units -0001 thru -0359) systems and both fuel flow
indicating systems are operative,
b) Fuel required for route to be flown
is increased by 10%,
c) Flight is restricted to a maximum
of three hours, remaining within
one hour of a suitable airport at all
points along route,
d) Both fuel tanks are fueled over-
wing to a known, balanced
quantity,
e) Fuel use is tracked,
f) If autopilot is used, it is
disconnected every twenty
minutes to detect possible lateral
fuel imbalance, monitor trim
required, and
g) Repairs are made within three
flight cycles.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 28-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

-41-02 Fuel Quantity Indicating A 2 1 (O) One indication may be inoperative

System provided:
(Wing tank) a) Both fuel low level indicating
(Units -0360 thru -0701) systems and both fuel flow
indicating systems are operative,
b) Fuel required for route to be flown
is increased by 10%,
c) Flight is restricted to a maximum
of three hours, remaining within
one hour of a suitable airport at all
points along route,
d) Both fuel tanks are fueled over-
wing to a known, balanced
quantity,
e) Fuel use is tracked,
f) If autopilot is used, it is
disconnected every twenty
minutes to detect possible lateral
fuel imbalance, monitor trim
required and aileron mistrim PFD
indication, and
g) Repairs are made within three
flight cycles.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 28-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL

-41-02 Fuel Quantity Indicating A 2 1 (O) One indication may be inoperative

System provided:
(Wing tank) a) Both fuel low level indicating
(Units -0800 and on) systems and both fuel flow
indicating systems are operative,
b) Fuel required for route to be flown
is increased by 10%,
c) Flight is restricted to a maximum
of three hours, remaining within
one hour of a suitable airport at all
points along route,
d) Both fuel tanks are fueled over-
wing to a known, balanced
quantity,
e) Fuel use is tracked,
f) If autopilot is used, it is
disconnected every twenty
minutes to detect possible lateral
fuel imbalance, monitor trim
required and RETRIM L-R WING
DOWN amber message, and
g) Repairs are made within three
flight cycles.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 30-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ICE AND RAIN
30
PROTECTION
-10-02 Stabilizer Pneumatic Boot B 1 0 (O) May be inoperative provided:
De-Ice System a) All de-ice boots are verified to be
(Failure to inflate) deflated and held down when
(Horizontal) service air system is active,
(Automatic or manual mode b) TAIL switch is selected OFF, and
failed) c) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions.

-10-04 Wing Bleed Air Anti-Ice B 2 0 (M) May be inoperative provided:

System a) Both wing valves are secured for
(Units -0001 thru -0701) no flow,
b) Both WING/ENG ANTI-ICE
switches are selected OFF or
ENG ON, and
c) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions.

-10-04 Wing Bleed Air Anti-Ice C 2 0 (M) May be inoperative provided:

System a) Both wing valves are secured for
(Units -0800 and on) no flow,
b) Both WING/ENG ICE
PROTECTION switches are
selected OFF or ENG ONLY, and
c) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions.

-20-01 Engine Anti-Ice System A 2 1 (M) May be inoperative provided:

(Without flow) a) Affected valve is secured for no
flow,
b) Both WING/ENG switches are
selected OFF,
c) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions, and
d) Repairs are made within three
flight days.

525MMELEU-01
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST

AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 30-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ICE AND RAIN
30
PROTECTION
-30-03 Pitot Tube Heater B 1 0 May be inoperative provided:
(Copilot) a) Pitot heater is not required by
(Units -0001 thru -0359) operating rule,
b) Aircraft is not operated at night,
c) Aircraft is not operated in
Instrument Meteorological
Conditions (IMC), and
d) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions.

-30-03 Pitot Tube Heater B 1 0 May be inoperative provided:

(Pilot) a) Pitot heater is not required by
(Units -0360 and on) operating rule,
b) Aircraft is not operated at night,
c) Aircraft is not operated in
Instrument Meteorological
Conditions (IMC), and
d) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions.

-30-04 Static Port Heater B 2 1 One may be inoperative provided:

(Copilot) a) Aircraft is not operated in
(Units -0001 thru -0359) Instrument Meteorological
Conditions (IMC),
b) Aircraft is not operated at night,
c) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions, and
d) Aircraft is not operated RVSM.

-30-04 Static Port Heater B 2 1 One may be inoperative provided:

(Pilot) a) Aircraft is not operated in
(Units -0360 and on) Instrument Meteorological
Conditions (IMC),
b) Aircraft is not operated at night,
c) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions, and
d) Aircraft is not operated RVSM.

525MMELEU-01
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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 30-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ICE AND RAIN
30
PROTECTION
-40-01 Rain Removal System C 1 0 May be inoperative provided aircraft is not
(Doors) operated in precipitation within five
nautical miles of airport used for takeoff,
intended landing or any alternates
required by operating rule.

-40-02 Windshield Bleed Air Anti- C 1 0 (M) May be inoperative provided:

Ice System a) Windshield anti-ice system is
secured for no flow,
b) Emergency pressurization system
is considered inoperative (Refer to
item 21-30-03), and
c) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions.

-40-03 Windshield Alcohol De-Ice C 1 0 (M) May be inoperative provided:

System a) Windshield de-ice system is
deactivated, and
b) Aircraft is not operated in known,
forecast, or AFM-defined icing
conditions.

-70-01 Drain Heater C - 0 (M) May be inoperative provided: |

(Evaporator fans, a) Drain heaters are deactivated, |
refreshment center, and / or b) Lavatory waste system is |
toilet relief tube) considered inoperative (Refer to |
item 38-30-03), and |
c) Evaporator fans, refreshment |
center, and toilet relief tube |
overboard drains are considered |
inoperative (Refer to item 38-30- |
04).

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CESSNA 525 DATE: 08/19/2014 31-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
INDICATING / RECORDING
31
SYSTEMS
-20-02 Clock D - - Any in excess of those required by
operating rule may be inoperative.

-20-04 Flight Hour Meter C 1 0 (O) May be inoperative provided flight

time is tracked by alternate means.

-30-03 Flight Data Recorder

***

-00A D 1 0 May be inoperative provided recorder is

not required by operating rule.

-00C A 1 0 May be inoperative provided:

a) Any Cockpit Voice Recorder
(CVR) required to be installed is
operative, and
b) Repairs are made within eight
flights or 72 hours, whichever
occurs first.

-01A Flight Data Recorder (FDR) A - - Up to five (5) percent of required

Parameters required by parameters may be inoperative provided
operating rule repairs are made within 90 calendar days
or prior to completion of next scheduled
inspection / check, whichever occurs first.

-01B Flight Data Recorder (FDR) A - - May be inoperative provided repairs are
Parameters not required by made prior to completion of next
operating rule scheduled inspection / check of FDR.

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CESSNA 525 DATE: 08/19/2014 31-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
INDICATING / RECORDING
31
SYSTEMS
-30-04 Quick Access Recorder
*** (QAR)

-00A D 1 0 May be inoperative provided recorder is

not required by operating rule.

-00B C 1 0 (O) May be inoperative when used for

Flight Data Monitoring (FDM) purposes,
provided approved alternate procedures,
if appropriate to other programmes using
associated data, are established and
used.

-40-02 Electronic Checklist D - 0 May be inoperative, missing, or out of

*** currency provided an approved checklist
is available and used.

-50-01 Annunciator
(Failed to illuminate)
(Units -0001 thru -0701)

-01 AC Power Fail D 1 0

(AC FAIL)
(Units -0100 thru -0359
G1000-equipped aircraft)

-03 Aft Baggage Door C 1 0 May be inoperative provided aft baggage

(BAGGAGE DOOR - AFT) door warning system is considered
(Units -0600 and on) inoperative (Refer to item 52-70-01-01).

-07 Cabin Door B 1 0 May be inoperative provided main cabin

(DOOR NOT LOCKED) and aft baggage door warning systems
(Units -0001 thru -0558) are considered inoperative (Refer to
items 52-70-01-01 and 52-70-01-07).

-07 Cabin Door B 1 0 May be inoperative provided main cabin

(CABIN DOOR) door warning system is considered
(Units -0600 thru -0701) inoperative (Refer to item 52-70-01-07).

(Continued)

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CESSNA 525 DATE: 08/19/2014 31-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
INDICATING / RECORDING
31
SYSTEMS
-50-01 Annunciator
(Failed to illuminate)
(Continued)

-09 Display Fan Fail D 1 0

(DISPLAY FAN FAIL)
(Units -0032 thru -0359
G1000-equipped aircraft)

-14 Forward Baggage Door B 1 0 May be inoperative provided forward

(BAGGAGE DOOR - FWD) baggage door warning system is
(Units -0600 thru -0701) considered inoperative (Refer to item 52-
70-01-06).

-20A Inverter Fail Caution D 3 0

(Amber INVERTER FAIL - 1
/ 2)
(Units -0100 thru -0359
G1000-equipped aircraft)

-20B Inverter Fail Warning D 1 0

(Red INVERTER FAIL)
(Units -0001 thru -0099
G1000-equipped aircraft)

-23 Nose Avionics Fan Fail D 1 0

(NOSE AVN FAN FAIL)
(Units -0032 thru -0359
G1000-equipped aircraft)

-24 Nose Compartment D 1 0

Overtemp
(NOSE COMP O'TEMP)
(Units -0001 thru -0031
G1000-equipped aircraft)

-50-02 Cabin Altitude Warning C 1 0 May be inoperative provided cabin

System pressurization system is considered
(Aural and / or visual inoperative (Refer to item 21-30-02).
warning failed)

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CESSNA 525 DATE: 08/19/2014 31-4
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
INDICATING / RECORDING
31
SYSTEMS
-50-03 Central Warning

-01 Master Warning Light C 2 1 Right side may be inoperative for single-
(Failed to illuminate) pilot operations.

-02 Master Warning Cancel / C 2 1 Right side may be inoperative for single-
Reset Function pilot operations.

-03 Master Caution Light C 2 1 Right side may be inoperative for single-
(Failed to illuminate) pilot operations.

-04 Master Caution Cancel / C 2 1 Right side may be inoperative for single-
Reset Function pilot operations.

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CESSNA 525 DATE: 08/19/2014 32-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR

-41-01 Anti-Skid System C 1 0 May be inoperative provided:

(Units -0001 thru -0558) a) Aircraft is operated in accordance
with AFM DISPATCH WITH
ANTISKID SYSTEM
INOPERATIVE abnormal
procedure, and
b) Steep approaches are not
conducted.

NOTE: If thrust attenuators are also

failed, takeoff and landing factors must be
multiplied together.

-41-01 Anti-Skid System C 1 0 May be inoperative provided:

(Units -0600 and on) a) Aircraft is operated in accordance
with AFM ANTISKID SYSTEM
INOPERATIVE DISPATCH
abnormal procedure, and
b) Steep approaches are not
conducted.

-44-01 Tire Pressure Monitoring D 1 0 NOTE: Any individual wheel sensors

*** System which are operative may be used.
(STC ST02272SE)

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CESSNA 525 DATE: 08/19/2014 33-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

-10-01 Cockpit and Instrument

Lighting
(Excluding button lights,
standby flight instrument
lighting, internally lighted
annunciators, and required
placard lighting)

-00A (Day) C - 0 May be inoperative provided aircraft is not

operated at night.

-00B (Night) C - - Individual lights may be inoperative

provided:
a) Cockpit emergency lighting is
operative,
b) Remaining lights are sufficient to
clearly illuminate all required
instruments, controls, and other
devices for which it is provided,
c) Remaining lights are positioned so
that direct rays are shielded from
crewmembers' eyes, and
d) Lighting configuration and
intensity is acceptable to flight
crew.

-10-04 Standby ALT/AS Placard C 1 0 May be inoperative provided aircraft is not

Lighting operated at night.
(Units -0001 thru -0359
G1000-equipped aircraft)

-10-05 Windshield Ice Detection

Light

-00A (Single light failed) C 2 1 (O) One may be inoperative provided

alternate procedures are established and
used to monitor ice accretion.

(Continued)

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CESSNA 525 DATE: 08/19/2014 33-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

-10-05 Windshield Ice Detection

Light
(Continued)

-00B (Both lights failed) C 2 0 May be inoperative provided aircraft is not

operated at night.

-00C (Right side failed) C 1 0 May be inoperative for single-pilot

operations.

-20-02 Cabin Interior Lighting

(Excluding cabin emergency
lighting)

-00A C - - (O) Individual lights may be inoperative

provided:
a) Sufficient lighting is operative for
crew to perform required duties,
b) Cabin emergency lighting is
verified operative, and
c) Sufficient lighting is operative for
carrying cabin occupants at night.

-00B D - 0 (O) May be inoperative provided:

a) Cabin emergency lighting is
verified operative, and
b) Aircraft is not operated at night or
cabin occupants are not carried.

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CESSNA 525 DATE: 08/19/2014 33-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

-20-04 Lighted Passenger C - 0 May be inoperative provided no cabin

Information Sign occupants are carried.
(Excluding cabin exit signs)
(Without cabin occupants)

-30-01 Aft Baggage Compartment C 1 0

Light

-30-02 Nose Baggage C 1 0

Compartment Light

-40-01 Anti-Collision Light System C 1 0 May be inoperative provided system is

(Wing strobe) not required by operating rule.

-40-02 Ground Recognition Light C 1 0 NOTE: Position / navigation or anti-

(Beacon) collision lights may be used on ground to
alert nearby aircraft or personnel when
engines are running or prior to start.

-40-03 Landing Light

-00A (Single light failed) B 2 1 One may be inoperative.

-00B (Both lights failed) C 2 0 May be inoperative provided aircraft is not

operated at night.

-01 Recognition / Taxi Mode C 1 0 (O) May be inoperative provided at least

one landing light is verified operative for
night operations.

-02 Pulse Light Mode D 1 0 (O) May be inoperative provided at least

*** one landing light is verified operative for
night operations.

-40-05 Position / Navigation Light C 1 0 May be inoperative provided system is

System not operated at night.

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CESSNA 525 DATE: 08/19/2014 33-4
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS

-40-10 Wing Inspection Light C 1 0 May be inoperative provided:

a) Aircraft is not operated at night in
known, forecast, or AFM-defined
icing conditions, and
b) Ground deicing procedures do not
require its use.

-50-01 Cockpit Flashlight C - - Any in excess of those required by

operating rule may be inoperative or
missing.

-01 Holder C - 0 May be inoperative provided associated

*** flashlight is stowed by alternate means.

-50-04 Exterior Emergency Light B 2 0 May be inoperative provided aircraft is not

operated at night.

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CESSNA 525 DATE: 08/19/2014 34-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-16-01 Altitude Alerting System B - 0 (O) May be inoperative provided:

a) Autopilot with altitude hold and
capture operates normally, and
b) Aircraft is not operated RVSM.

-02 Visual Alert C - 0 May be inoperative provided:

a) Aural alert operates normally, and
b) Autopilot with altitude hold and
capture operates normally.

-18-01 Angle of Attack (AOA) C 1 0 May be inoperative provided stick shaker

System Indicator is verified operative.
(Units -0001 thru -0701)

-18-02 Angle of Attack (AOA) C 1 0 May be inoperative provided aircraft is not

Heater operated in known, forecast, or AFM-
defined icing conditions.

-23-01 Non-stabilized Magnetic

Compass
(Units -0360 and on)

-00A (Day, VMC) B 1 0 May be inoperative provided:

a) Any combination of two gyro or
AHRS-stabilized compass
systems are operative, and
b) Aircraft is not operated at night or
in Instrument Meteorological
Conditions (IMC).

(Continued)

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CESSNA 525 DATE: 08/19/2014 34-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-23-01 Non-stabilized Magnetic

Compass
(Units -0360 and on)
(Continued)

-00B B 1 0 May be inoperative provided:

a) Any combination of two gyro or
AHRS-stabilized compass
systems are operative,
b) Aircraft is operated with dual
independent navigation capability,
and
c) Aircraft is operated under positive
radar control by ATC on enroute
portion of flight.

-01 Internal Lighting C 1 0 May be inoperative provided flight crew

determines adequate natural or artificial
lighting exists to read compass.

-24-01 Mechanical Slip/Skid B 2 1 Pilot side must be operative for single-

Indicator pilot operations.
(Units -0001 thru -0359
excluding G1000-equipped
aircraft)

-24-01 Mechanical Slip/Skid B 1 0

Indicator
(Copilot's)
(Units -0360 thru -0558
single PFD-equipped
aircraft)

-01 Internal Lighting C 1 0 May be inoperative provided flight crew

determines adequate natural or artificial
lighting exists to read indicator.

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CESSNA 525 DATE: 08/19/2014 34-3
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-25-01 Cursor Control Panel C 1 0 May be inoperate provided Class 3 EFB

*** (Units -0360 thru -0701) is considered inoperative (Refer to item
46-00-01).

-03 Memory Buttons D 3 0

(MEM1, MEM2, MEM3)

-04 CHART Button C 1 0 NOTE: Electronic charts will not be

available, alternate charts must be
carried.

-05 Rotate Button C 1 0 NOTE: Some electronic charts may not

be legible, alternate charts must be
carried.

-06 ZOOM Button C 1 0 NOTE 1: Some electronic charts may not

be legible, alternate charts must be
carried.

NOTE 2: Graphic weather zoom function

is considered inoperative.

-07 Joystick C 1 0 NOTE 1: Some electronic charts may not

be legible, alternate charts must be
carried.

NOTE 2: Graphic weather pan function is

considered inoperative.

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CESSNA 525 DATE: 08/19/2014 34-4
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-25-05 Display Controller B 1 0 (M) Copilot’s side may be failed provided:

(GCU 275) a) Controller is deactivated,
(Units -0800 and on) b) Both touchscreen controllers are
operative, and
c) Barometer synchronization is
verified engaged.

-09 Barometer Standard C 1 0

(PUSH STD)

-11 Range / Pan Control C 1 0 May be inoperative provided touchscreen

(Knob) controller for associated display is
operative.

-12 Clear C 1 0
(CLR)

-13 Enter C 1 0
(ENT)

-14 Cursor / Select C 3 0

(PFD / PUSH CRSR)

-15 Direct To C 1 0 NOTE: Function may be selected on

(D>) touchscreen controller.

-16 Flight Plan C 1 0 NOTE: Function may be selected on

(FPL) touchscreen controller.

-17 Radio Control C 1 0 NOTE: Function may be selected on

(COM/NAV) touchscreen controller.

-18 Procedure C 1 0 NOTE: Function may be selected on

(PROC) touchscreen controller.

-19 Barometer Setting B 1 0 May be inoperative provided barometer

(BARO) synchronization is enabled.

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CESSNA 525 DATE: 08/19/2014 34-5
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-25-07 Touchscreen Controller B 1 0 (M) May be inoperative provided

(Right GTC) controller is deactivated.
(Units -0800 and on)
NOTE: Any functions or controls that
operate normally may be used.

-25-08 MFD Control Unit B 1 0 (O) May be inoperative provided:

(GCU 475) a) Weather radar is considered
(Units -0001 thru -0359 inoperative (Refer to item 34-42-
G1000-equipped aircraft) 01),
b) Datalink is considered inoperative
(Refer to item 23-20-01),
c) Electronic chart is considered
inoperative,
d) Procedures do not require use of
MFD,
e) Aircraft is operated in Visual
Meteorological Conditions (VMC),
f) Aircraft is not operated at night,
g) PFD inset maps are used, and
h) Alternate procedures are
established and used.

-25-10 Synthetic Vision C 1 0 May be inoperative provided procedures

*** (Units -0001 thru -0359 do not require its use.
G1000-equipped aircraft
and Units -0800 and on)

-31-01 Localizer System D - - May be inoperative provided:

a) Associated glideslope is
considered inoperative (Refer to
item 34-32-01), and
b) Aircraft is not operated under
Instrument Flight Rules (IFR).

-32-01 Glideslope System D - - May be inoperative provided aircraft is not

operated under Instrument Flight Rules
(IFR).

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CESSNA 525 DATE: 08/19/2014 34-6
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-34-01 Marker Beacon Receiver C - 0 May be inoperative provided:

System a) Procedures do not require its use,
and
b) System is not required by
operating rule.

-36-01 Reactive Windshear System C 1 0 (O) May be inoperative provided alternate

*** (Includes TAWS windshear procedures are established and used.
mode)

-42-01 Weather Radar System C 1 0 May be inoperative provided:

a) Aircraft is not operated at night,
and
b) Aircraft is not operated in
Instrument Meteorological
Conditions (IMC).

-44-01 Radio Altimeter System

*** (Units -0001 thru -0359)

-44-01 Radio Altimeter System

(Units -0360 and on)

-00A (TAWS and TCAS II not C 1 0 (M) May be inoperative provided:

required) a) Radio altimeter system is
(Units -0001 -0701) deactivated,
b) Approach minimums or operating
procedures do not require its use,
c) Basic TAWS modes are
considered inoperative (Refer to
item 34-44-03), and
d) TCAS II is considered inoperative
(Refer to item 34-45-01).

(Continued)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-44-01 Radio Altimeter System

(Continued)

-00A (TAWS and TCAS II not C 1 0 (M) May be inoperative provided:

required) a) Radio altimeter system is
(Units -0800 and on) deactivated,
b) Approach minimums or operating
procedures do not require its use,
c) Basic TAWS modes are
considered inoperative (Refer to
item 34-44-03), and
d) TCAS II is considered inoperative
(Refer to item 34-45-01).

NOTE: Landing Operations Phase Inhibit

(LOPI) operation will be affected. LOPI
may not activate during approach or go-
around.

-00B (TAWS or TCAS II required) A 1 0 (M) May be inoperative provided:

(Units -0001 -0701) a) Radio altimeter system is
deactivated,
b) Approach minimums or operating
procedures do not require its use,
c) Basic TAWS modes are
considered inoperative (Refer to
item 34-44-03),
d) TCAS II is considered inoperative
(Refer to item 34-45-01), and
e) Repairs are made within six flights
or two calendar days, whichever
occurs first.

(Continued)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-44-01 Radio Altimeter System

(Continued)

-00B (TAWS or TCAS II required) A 1 0 (M) May be inoperative provided:

(Units -0800 and on) a) Radio altimeter system is
deactivated,
b) Approach minimums or operating
procedures do not require its use,
c) Basic TAWS modes are
considered inoperative (Refer to
item 34-44-03),
d) TCAS II is considered inoperative
(Refer to item 34-45-01), and
e) Repairs are made within six flights
or two calendar days, whichever
occurs first.

NOTE: Landing Operations Phase Inhibit

(LOPI) operation will be affected. LOPI
may not activate during approach or go-
around.

-44-02 Surface Awareness System C 1 0

*** (Runway Awareness and
Advisory System RAAS)
(Units -0001 thru -0701)

-44-02 Surface Awareness System C 1 0

*** (SurfaceWatch)
(Units -0800 and on)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-44-03 Terrain Awareness and C 1 0 (O) May be inoperative provided alternate

*** Warning System (TAWS) procedures are established and used.
(Class A or B TAWS not
required) NOTE: Any mode that operates normally
may be used.

-44-03 Terrain Awareness and A 1 0 May be inoperative provided repairs are

Warning System (TAWS) made within six flights or two calendar
(Including test mode) days, whichever occurs first.
(Class A or B TAWS
required)

-01 Forward Looking Terrain B 2 0 (O) May be inoperative provided alternate

Avoidance Function and procedures are established and used.
Premature Descent Alert
Function

-02 Excessive Rate of Descent B 2 0 May be inoperative provided Forward

(Mode 1) and Altitude Loss Looking Terrain Avoidance and
After Takeoff or Missed Premature Descent Alert Functions are
Approach (Mode 3) operative (Refer to item 33-44-03-01).

-03A Voice Callouts (Mode 6) B 1 0 (O) May be inoperative provided alternate

("Five-Hundred") procedures are established and used.

-03B Voice Callouts (Mode 6) C - 0 (O) May be inoperative provided alternate

(Other) procedures are established and used.

-04B Excessive Closure Rate to B 2 0 May be inoperative provided Forward

Terrain (Mode 2) and Flight Looking Terrain Avoidance and
Into Terrain Not in Landing Premature Descent Alert Functions are
Configuration (Mode 4) operative (Refer to item 33-44-03-01).
(Class B TAWS required)

-05 Excessive Downward B - 0

Glideslope/Glidepath
Deviation (Mode 5)
(Class B TAWS required)

(Continued)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-44-03 Terrain Awareness and

Warning System (TAWS)
(Continued)

-06 Terrain Display C - 0

*** (Class B TAWS required)

-07 Switch C - 0
(Any excluding TAWS Test)
(Class B TAWS required)

-08 Annunciator / Indication C - 0

(Class B TAWS required)

-45-01 Traffic Alert and Collision

*** Avoidance System
(TCAS I or TCAS II)

-00A (TCAS not required) C 1 0 (M) May be inoperative provided:

a) System is deactivated,
b) System is not required by
operating rule, and
c) Enroute or approach procedures
do not require its use.

-00B (TCAS required) A 1 0 (M) May be inoperative provided:

a) System is deactivated,
b) Enroute or approach procedures
do not require its use, and
c) Repairs are made within ten
calendar days.

-01 Traffic Alert (TA) Display C - 0 (O) May be inoperative provided:

System a) Resolution Advisory (RA) visual
(TCAS II only) display and audio function are
operative, and
b) Enroute or approach procedures
do not require its use.

(Continued)

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CESSNA 525 DATE: 08/19/2014 34-11
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-45-01 Traffic Alert and Collision

Avoidance System
(Continued)

-02A Resolution Advisory (RA) C 2 1 One may be inoperative on pilot not flying
Display System side.
(TCAS II only)

-02B Resolution Advisory (RA) C 2 0 (O) May be inoperative provided:

Display System a) Traffic Alert (TA) visual display
(TCAS II only) and audio function are operative,
b) TA-only mode is selected by flight
crew, and
c) Enroute or approach procedures
do not require its use.

-03 Combined Traffic Alert (TA) C 2 1 One may be inoperative provided:

and Resolution Advisory a) Affected system is on pilot not
(RA) Display System flying side,
(TCAS II only) b) TA and RA visual display is
operative on pilot flying side, and
c) TA and RA audio function is
operative on pilot flying side.

-04 Audio Function B 1 0 May be inoperative provided enroute or

approach procedures do not require use
of TCAS.

-05 Airspace Selection Function C - 0

-45-02 Traffic Collision Avoidance D 1 0

*** Device (TCAD)

-46-01 Lightning Detection System D 1 0 May be inoperative provided system is

*** not required by operating rule.

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-50-01 Radio Magnetic Indicator C - 0 May be inoperative provided procedures

(RMI) do not require its use.
(Units -0001 thru -0359
excluding G1000-equipped
aircraft)

-51-01 Distance Measuring D - - Any in excess of those required by

Equipment (DME) operating rule may be inoperative.

-52-01 ATC Transponder and

Automatic Altitude Reporting
System

-00A (Individual transponder D - 1 May be inoperative provided system is

failed) not required by operating rule.

-00B (All transponders failed) A - 0 May be inoperative provided:

a) Operations do not require its use,
b) Prior to flight, approval is obtained
from ATC facilities having
jurisdiction over planned route of
flight,
c) TCAS, if installed, is considered
inoperative (Refer to item 34-45-
01),
d) Aircraft is not operated RVSM,
and
e) Repairs are made within five
flights.

-01 Elementary and Enhanced D - 0 May be inoperative provided operations

*** Downlink Aircraft Reportable do not require their use.
Parameters
(Not required by operating
rule)

(Continued)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-52-01 ATC Transponder and

Automatic Altitude Reporting
System
(Continued)

-02 ADS-B Squitter D - 0 May be inoperative provided operations

Transmission do not require its use.
(Units -0001 thru -0359
G1000-equipped aircraft
and Units -0800 and on)

-54-01 Very High Frequency Omni C - 0 May be inoperative provided:

Range (VOR) System a) Affected system is not on an
emergency bus,
b) Procedures do not require its use,
and
c) System is not required by
operating rule.

-55-01 Automatic Direction Finder D - 0 May be inoperative provided operations

*** (ADF) do not require its use.

-57-01 Global Navigation Satellite C - 0 May be inoperative provided:

System (GNSS) a) System is not required by
(Including SBAS) operating rule, and
b) Operations do not require its use.

NOTE 1: Enhanced function of TAWS

may not be available.

NOTE 2: ADS-B output may not be

available.

-60-01 Data Loader C - - NOTE: Certain card slots are used for
(SD card slot) real-time data access. If inoperative,
(Units -0001 thru -0359 associated features are considered
G1000-equipped aircraft inoperative.
and Units -0800 and on)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-60-01 Data Loader C - 0

(Units -0001 thru -0359
excluding G1000-equipped
aircraft and Units -0360 thru
-0701)

-60-02 Flight Management System C - 0 May be inoperative provided:

(FMS) a) System is not required by
operating rule, and
b) Operations do not require its use.

NOTE: Enhanced function of TAWS may

not be available.

-60-03 Information Management D 1 0 May be inoperative provided navigation

*** Server database, electronic charts, and
(IMS-3500) performance database are loaded by
(Units -0600 thru -0701) alternate means.

-61-01 Navigation Database

-00A C - 0 (O) May be inoperative provided:

a) Conventional (non-RNAV/RNP)
navigation is sufficient for route to
be flown,
b) Current aeronautical information
(e.g. Charts) is available for route
to be flown and airports to be
used,
c) Navigation database information
is disregarded, and
d) Radio navigation aids, which are
required to for departure, arrival,
and approach procedures, are
manually tuned and identified.

(Continued)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION

-61-01 Navigation Database

(Continued)

-00B A - 0 (O) May be out of currency provided:

a) Area navigation (RNAV/RNP)
departure, arrrival and approach
procedures are checked not to
depend on data amended in
current database cycle, or
Conventional (non-RNAV/RNP) or
ANSP assistance are used as an
alterative to RNAV/RNP
procedures which have been
amended in current database
cycle,
b) Current aeronautical information is
used to verify database navigation
fixes, coordinates, frequencies,
status (as applicable), and
suitability of navigation facilities
required for route to be flown,
prior to each flight, and
c) Radio navigation aids, which are
required for departure, arrival, and
approach procedures, which have
been amended in current
database cycle, are manually
tuned and identified.

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
35 OXYGEN

-00-03 Oxygen System

-01 Fill Port C 1 0 (M) May be inoperative provided bottle is

filled using alternate means, if service is
required.

-03 Blowout Disk / Green Label C 1 0 (O) May be missing or damaged provided
oxygen pressure is verified prior to each
flight.

-10-01 Flight Crew Oxygen System

-01 Copilot Oxygen Mask C 1 0 May be inoperative provided copilot seat

is not occupied.

-20-01 Passenger Oxygen System

-00A (With cabin occupants) B 1 0 May be inoperative provided:

a) Cabin pressurization system is
operative,
b) Portable oxygen system is
available,
c) Aircraft is able to decend within
four minutes to a cabin pressure
altitude of 13,000 feet at all points
along route to be flown, and
d) Aircraft is operated at FL250 or
below.

-00B (Without cabin occupants) C 1 0 May be inoperative provided:

a) OXYGEN CONTROL is selected
to CREW ONLY, and
b) No cabin occupants are carried.

-00C (Cabin unpressurized) C 1 0 May be inoperative provided cabin

pressurization system is considered
inoperative (Refer to item 21-30-02).

(Continued)

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CESSNA 525 DATE: 08/19/2014 35-2
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
35 OXYGEN

-20-01 Passenger Oxygen System

(Continued)

-01 Mask B - 0 (M) Individual oxygen masks or

dispensers may be inoperative or missing
provided:
a) Affected mask pintle pin is
installed, and
b) Associated seat or lavatory is
placarded "DO NOT OCCUPY".

-02 Drop-out Panel C - 0 (M) Individual panels may be out of

normal position provided:
a) Affected oxygen mask and drop
out panel are removed,
b) Affected mask pintle pin is
installed, and
c) Associated seat or lavatory is
placarded "DO NOT OCCUPY".

-30-02 Protective Breathing D - - Any in excess of those required by

*** Equipment (PBE) operating rule may be missing, or
inoperative provided:
a) Inoperative PBE is placarded
“INOPERATIVE”, removed from
installed location, and placed out
of sight so it cannot be mistaken
for a functional unit, and
b) Location placarding is removed or
obscured.

NOTE: Inoperative PBE may be subject

to dangerous goods requirements.

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AIRCRAFT: REVISION NO. 01 PAGE NO.

CESSNA 525 DATE: 08/19/2014 38-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
38 WATER / WASTE

-30-01 Relief Tube C 1 0 (M) May be inoperative provided:

(Toilet) a) All liquid is removed from relief
tube, and
b) Relief tube is placarded “DO NOT
USE”.

-30-03 Lavatory Waste System C 1 0 Individual components may be

inoperative provided:
a) Cabin occupants are briefed prior
to each flight that lavatory is
inoperative and unusable, and
b) Lavatory is placarded "DO NOT
USE".

-30-04 Overboard Drain

(Excluding drain heater)

-02 Evaporator Fan C 2 0 May be damaged or obstructed provided

(Forward or aft) affected evaporator fan is considered
inoperative (Refer to item 21-50-03).

-03 Refreshment Center C 1 0 (O) May be damaged or obstructed

provided:
a) All liquid is removed from
refreshment center hot liquid
storage and drip pan,
b) Refreshment center hot liquid
storage and drip pan are
placarded "DO NOT USE", and
c) Ice drawer drain valve remains
closed.

-04 Relief Tube C 1 0 May be damaged or obstructed provided

(Toilet) toilet relief tube is considered inoperative
(Refer to item 38-30-01).

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CESSNA 525 DATE: 08/19/2014 45-1
1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
CENTRAL MAINTENANCE
45
SYSTEM
-00-01 Aircraft Recording System D 1 0
*** (AReS)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
46 INFORMATION SYSTEMS

-00-01 Electronic Flight Bag (EFB) C - 0 (O) May be inoperative provided alternate
*** System procedures are established and used.
(Includes IFIS)
NOTE: Any function, program, or
document which operates normally may
be used.

-01 Data Connectivity C - 0 (O) May be inoperative provided alternate

(Class 2) procedures are established and used.

-02 Power Connection C - 0 (O) May be inoperative provided alternate

(Class 1 & 2) procedures are established and used.

-03 Mounting Device C - 0 (M) (O) May be inoperative provided:

(Class 2) a) Associated EFB and hardware is
secured by alternate means or
removed from aircraft, and
b) Alternate procedures are
established and used.

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
52 DOORS

-10-01 Main Cabin Door

-01 Key Lock D 1 0

(Failed unlocked)

-04 Primary Seal C 1 0 May be inoperative provided:

(Cabin unpressurized) a) Primary seal does not interfere
with door operation, and
b) Cabin pressurization system is
considered inoperative (Refer to
item 21-30-02).

-05A Secondary Seal C 1 0 May be damaged provided:

(Cabin pressurized) a) Primary door seal is operative,
b) Secondary seal does not interfere
with door operation, and
c) Aircraft is operated at FL250 or
below.

-05B Secondary Seal C 1 0 May be damaged provided:

(Cabin unpressurized) a) Secondary seal does not interfere
with door operation, and
b) Cabin pressurization system is
considered inoperative (Refer to
item 21-30-02).

-08 Gust Lock B 1 0 (O) May be inoperative provided a

procedure is established and used to
prevent unrestricted movement of cabin
door.

-20-01 Escape Hatch Lock Pin Deleted, revision 3A

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
52 DOORS

-30-01 Aft Baggage Door

-01 Key Lock D 1 0 May be inoperative provided door is

(Failed unlocked) verified closed and latched prior to each
flight.

NOTE: Aft baggage door warning system

may activate.

-40-01 Nose Baggage Door

-01A Key Lock C 2 0 May be inoperative provided door is

(Failed unlocked) verified closed and latched prior to each
flight.

NOTE: Nose baggage door warning

system may activate.

-01B Key Lock C 2 1 (O) One may be inoperative provided

(Failed locked) alternate procedures are established and
used to perform required preflight actions
through operative door.

-70-01 Door Warning System

-01 Aft Baggage C 1 0 May be inoperative provided:

a) Door is verified closed, latched,
and locked prior to each flight, and
b) Aircraft is operated at 200 KIAS or
less.

-06 Nose Baggage B 2 0 May be inoperative provided:

a) Door is verified closed, latched,
and locked prior to each flight, and
b) Aircraft is operated at 200 KIAS or
less.

(Continued)

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
52 DOORS

-70-01 Door Warning System

(Continued)

-07 Main Cabin B 1 0 (O) May be inoperative provided:

a) Door is verified closed and handle
latched,
b) All lock flags are visible in sight
glass locations,
c) Internal door handle is verified
correctly stowed,
d) Aircraft is operated at 200 KIAS or
less, and
e) Aircraft is operated at FL250 or
below.

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SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
ENGINE FUEL AND
73
CONTROL
-33-01 Fuel Flow Indicating System A 2 1 One may be inoperative provided:
a) Both fuel quantity indicating
systems are operative, and
b) Repairs are made within three
flight days.

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1. REPAIR CATEGORY
SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
76 ENGINE CONTROLS

-01-01 Engine Synchronizer C 1 0

System
(Failed off)

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SYSTEM, 2. NUMBER INSTALLED
SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
78 ENGINE EXHAUST

-30-02 Thrust Attenuator C 2 0 (M) May be inoperative provided:

(Units -0001 thru -0558) a) Both attenuators are deactivated
in stowed position,
b) Aircraft is operated in accordance
with AFM DISPATCH WITH
ATTENUATOR STOWED
abnormal procedure, and
c) Steep approaches are not
conducted.

NOTE: If anti-skid system is also failed,

takeoff and landing factors must be
multiplied together.

525MMELEU-01