EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST
CESSNA CE-560XL
Citation Excel
REVISION: 1
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EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST
CESSNA CITATION 560XL Revision 1
23 October 2012
This Master Minimum Equipment List (MMEL) is issued by the European Aviation Safety Agency
(EASA) at the above revision and is recommended for approval as the basis of the preparation and
approval of individual operators' Minimum Equipment Lists (MELs) for aircraft of this type as
certified by EASA and operated under the jurisdiction of EASA member states National Authorities.
MMEL Section Manager
For and on behalf of the EASA
Correspondence concerning this document should be addressed to the office listed below:
European Aviation Safety Agency
Postfach 10 12 53
50452 Koln
Germany
Attention:
MMEL Section Manager, Experts Department
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REVISION RECORD
REVISION No.
ISSUE DATE
ORIGINAL
10-JAN-2009
1
23 October 2012
INCORPORATED BY
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TABLE OF CONTENTS
I.
III.
V.
VII - VIII.
XI. – XII.
XIII. – XVII.
XVIII - XX.
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APPROVAL SHEET
REVISION RECORD
TABLE OF CONTENTS
LIST OF EFFECTIVE PAGES
PREAMBLE
DEFINITIONS AND EXPLANATORY NOTES
HILIGHTS OF REVISION
AIR CONDITIONING
AUTO FLIGHT
COMMUNICATIONS
ELECTRICAL POWER
EQUIPMENT/FURNISHINGS
FIRE PROTECTION
FLIGHT CONTROLS
FUEL
ICE AND RAIN PROTECTION
INDICATING & RECORD
LIGHTS
NAVIGATION
OXYGEN
WATER/WASTE
CENTRAL MAINTENANCE
INFORMATION SYSTEMS
AIRBORNE AUXILIARY POWER
DOORS
ENGINE FUEL CONTROL
ENGINE CONTROLS
ENGINE INDICATING
EXHAUST
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List of Effective Pages (Continued)
Preamble
Preamble (Continued)
Definitions and Explanatory Notes
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Definitions and Explanatory Notes (Continued)
Definitions and Explanatory Notes (Continued)
Definitions and Explanatory Notes (Continued)
Highlights of Revision Original
Highlights of Revision Original (Continued)
Highlights of Revision Original (Continued)
Air Conditioning
Air Conditioning (Continued)
Air Conditioning (Continued)
Air Conditioning (Continued)
Air Conditioning (Continued)
Air Conditioning (Continued)
Auto Flight
Auto Flight (Continued)
Communications
Communications (Continued)
Communications (Continued)
Communications (Continued)
Communications (Continued)
Communications (Continued)
Electrical Power
Electrical Power (Continued)
Equipment/Furnishings
Equipment/Furnishings (Continued)
Equipment/Furnishings (Continued)
Equipment/Furnishings (Continued)
Equipment/Furnishings (Continued)
Equipment/Furnishings (Continued)
Fire Protection
Fire Protection (Continued)
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Flight Controls
Flight Controls (Continued)
Fuel
Fuel (Continued)
Ice and Rain Protection
Ice and Rain Protection (Continued)
Ice and Rain Protection (Continued)
Ice and Rain Protection (Continued)
Indicating & Record
Indicating & Record (Continued)
Indicating & Record (Continued)
Indicating & Record (Continued)
Indicating & Record (Continued)
Indicating & Record (Continued)
Indicating & Record (Continued)
Indicating & Record (Continued)
Indicating & Record (Continued)
Indicating & Record (Continued)
Lights
Lights (Continued)
Lights (Continued)
Lights (Continued)
Navigation (Continued)
Navigation (Continued)
Navigation (Continued)
Navigation (Continued)
Navigation (Continued)
Navigation (Continued)
Navigation (Continued)
Navigation (Continued)
Navigation (Continued)
Navigation (Continued)
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Oxygen
Oxygen (Continued)
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Water/Waste
Water/Waste (Continued)
Central Maintenance
Central Maintenance (Continued)
Information Systems
Information Systems (Continued)
Airborne Auxiliary Power
Airborne Auxiliary Power (Continued)
Doors
Doors (Continued)
Engine Fuel Control
Engine Fuel Control (Continued)
Engine Controls
Engine Controls (Continued)
Engine Indicating
Engine Indicating (Continued)
Exhaust
Exhaust (Continued)
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PREAMBLE
The following is applicable for operators under EASA or European operating regulations (EUOPS). The regulations require that all equipment installed on an aircraft in compliance with the
Airworthiness code and the operating requirements must be operative. However, the Regulations
also permit 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 component may not be necessary when the remaining operative equipment can
provide an acceptable level of safety.
EASA Master Minimum Equipment List (MMEL) is developed by the Type Certificate Holder to
improve aircraft utilisation and thereby provide more convenient and economic air transportation
for the public. EASA MMEL includes those items of equipment related to airworthiness and
operating requirements and other items of equipment which EASA finds may be inoperative and
yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not
contain obviously required items such as wings, flaps, and rudders.
The MMEL is the basis for development of individual operator's MELs, 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 cannot be less restrictive than the
MMEL. The individual operator's MEL, when approved permits operation of the aircraft with
inoperative equipment.
Equipment not required by the operation being conducted and equipment in excess of the
requirements are included in the MEL with appropriate conditions and limitations. The MEL must
not deviate from Airworthiness Directives or any other Mandatory Requirement It is important to
remember that all equipment related to the airworthiness and the operating requirements of the
aircraft not listed on the MMEL must be operative.
Suitable conditions and limitations in the form of placards, maintenance procedures, crew
operating procedures and other restrictions as necessary are specified in the MEL to ensure that
an acceptable level of safety is maintained.
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(Continued)
The MEL is intended to permit operation with inoperative items of equipment for a period of time
until rectifications can be accomplished. It is important that rectifications be accomplished at the
earliest opportunity. In order to maintain an acceptable level of safety and reliability, the MMEL
establishes limitations on the duration of, and conditions for operation with, inoperative equipment.
The operator may be permitted, by their competent authority, a one-time extension of the
applicable rectification intervals B, C or D for the same duration as that specified in their MEL. This
extension policy has been taken into account during the development of this document.
When an item of equipment is discovered to be inoperative, it is reported by making an entry in the
Aircraft Maintenance Record/Logbook as prescribed by the applicable regulations. The item is then
either rectified or may be deferred per the MEL or other approval means acceptable to the
competent Authority 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 of
equipment inoperative.
When these requirements are met, an Airworthiness Release, Aircraft Maintenance
Record/Logbook entry, or other approved documentation is issued as prescribed by the applicable
regulations. Such documentation is required prior to operation with any item of equipment
inoperative.
Operators are responsible for exercising the necessary operational control to ensure that an
acceptable level of safety is maintained. The exposure to additional failures during continued
operation with inoperative systems or components must 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 must be considered.
Operators are to establish a controlled and sound rectification program including the parts,
personnel, facilities, procedures and schedules to ensure timely rectification. This program should
identify the actions required for Maintenance discrepancy messages.
WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE,
DEFINITIONS AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS
REQUIRED.
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DEFINITIONS AND EXPLANATORY NOTES
1.
In this list, the items of equipment are classified in systems according to the ATA 100
specification. Individual items within a given ATA classification are numbered sequentially.
2.
“Item” (Column 1): The equipment, system, components or function as listed in Column 1.
“(If installed)”: Indicates the listed item of equipment is not applicable to all models or
configurations. It does not imply that the aeroplane may be operated in accordance with this
MMEL with the item removed.
NOTE 1: Items annotated in UPPER CASE letters indicate the precise flight deck legend
used.
3.
“Rectification Intervals” (Column 2): 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 given in the “Rectification Interval” column (2)
of the MMEL.
Category A
No standard interval is specified. However, items in this category shall be rectified in
accordance with the conditions stated in the Remarks column (5) of the MMEL.
Where a time period is specified it shall start at 00:01 on the calendar day following the day
of discovery.
Category B
Items in this category shall be rectified within three (3) consecutive calendar days,
excluding the day of discovery. For example, if it was recorded at 10 am on January 26th,
the three day interval would begin at midnight on the 26th and end at midnight on the 29th.
Category C
Items in this category shall be rectified within ten (10) consecutive calendar days, excluding
the day of discovery. For example, if it was recorded at 10 am on January 26th, the 10 day
interval would begin at midnight on the 26th and end at midnight on February 5th.
Category D
Items in this category shall be rectified within one hundred and twenty (120) consecutive
calendar days, excluding the day of discovery.
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DEFINITIONS AND EXPLANATORY NOTES
4.
“Number Installed” (Column 3): The number of the specified items normally installed in the
aeroplane. This number identifies the aeroplane configuration considered in developing the
MMEL.
5.
“Number Required for Dispatch (Column 4): The minimum number of the specified items
required for operation provided the conditions defined in Column 5 are met.
6.
“Remarks or Exceptions” (Column 5): This column includes a statement prohibiting
operation or permitting operation with a specific number of items inoperative, provisos
(conditions and limitations) for such operation and appropriate notes.
A note in column 5 indicates additional information and references for crew and/or
maintenance personnel consideration; they are not part of the provisos.
Where references are stated in column 5 these are to identify certain inter-relationships
between the subject item and other MMEL items, AFM material etc. These references are
intended to assist, but not relieve, an operator of the responsibility for determining such
inter-relationships as stated in the Preamble.
7.
Dash (-): This symbol indicates a variable quantity when used in Columns 3 or 4.
8.
Each inoperative item must be placarded to inform and remind the crew members and
maintenance personnel of the equipment condition. To the extent practicable, placards
should be located adjacent to the control or indicator for the item affected such that it is
clear to the operating crew that it or its associated system is inoperative.
9.
“Inoperative”: A system or item of equipment is deemed inoperative if it malfunctions such
that it does not accomplish its intended purpose and/or is not consistently functioning within
its designed operating limit(s) or tolerance(s).
10.
“(O)”: The use of this symbol in Column 5 indicates that an appropriate operating procedure
(or change to an existing procedure) must be established, published and utilized to maintain
the required level of safety while operating under the terms of the (M) MEL.
Normally, these procedures are accomplished by the flight crew. However, other personnel
may be qualified and authorized to perform certain functions.
11.
“(M)”: The use of this symbol in Column 5 indicates that an appropriate maintenance
procedure must be established, published and utilized prior to the first flight undertaken
following discovery of the defect and, if necessary, repeated at specified intervals during
operation under the terms of the (M)MEL to maintain the required level of safety.
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DEFINITIONS AND EXPLANATORY NOTES
Normally, these procedures are accomplished by maintenance personnel. However, other
personnel may be qualified and authorised to perform certain functions.
Note:
When an item is annotated (O)/(M), the “/” is defined as “and/or”, which shows that
there may be different options available in respect of the MEL procedures.
12.
“Visual Flight Rules (VFR)”: is as defined by National Authority Operating Requirements.
This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.
13.
“Icing Conditions”: An atmospheric condition that may cause ice to form on the aeroplane or
in the engines.
14.
“Visible Moisture”: An atmospheric environment containing water in any form that can be
seen in natural or artificial light, i.e. clouds, fog, rain, sleet, hail, snow.
15.
“Flight Hour”: The time from the moment an aeroplane leaves the surface of the earth until it
touches it at the next point of landing.
16.
“Flight”: For the purpose of a MEL, a flight is the period of time between the moment when
an aeroplane begins to move by its own means, for the purpose of preparing for take-off,
until the moment the aeroplane comes to a complete stop on its parking area, after the
subsequent landing (and no subsequent take-off).
17.
“Flight day”: A 24 hour period (from midnight to midnight) either UTC or local time as
established by the operator, during which at least one flight is initiated for the affected
aeroplane.
18.
“Authority”: The competent regulatory authority according to the country of registry.
19.
“Deleted”: When applied to an item number, indicates that the item was previously listed but
is now required to be operative.
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DEFINITIONS AND EXPLANATORY NOTES
20.
“Combustible (Material)”: refers to 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.); and
Note:
If serviceable tires are included they should only be inflated to a minimum pressure
that preserves their serviceability.
3) Inflight service material (return catering – only closed catering trolley/boxes, no
newspapers, no alcohol or duty free goods).
21.
“System”: System means the group of directly related components which together perform
a specified function, for example “RPM Indication System” would include the RPM Indicator,
tachometer generator, circuit breaker and associated circuitry.
22.
“Dispatch”: The point at which an aeroplane first moves under its own power for the
purpose of commencing a flight.
Note:
The MMEL/MEL applies to all defects that occur up to the point of dispatch, and
comes into effect again when the aeroplane next comes to rest at the end of its
flight.
23.
“Deactivated” and “Secured”: means that the specified component must be put into an
acceptable condition for safe flight. An acceptable method of securing or deactivating will
be established by the operator.
24.
"Administrative control item": means an item listed by the operator in the MEL for tracking
and informational purposes. It may be added to an operator's MEL by approval of the
National Authority provided no relief is granted, or provided conditions and limitations are
contained in an approved document (i.e. Structural Repair Manual, airworthiness directive,
etc.). If relief other than that granted by an approved document is sought for an
administrative control item, a request must be submitted to the National Authority. If the
request results in review and approval by the OEB, the item becomes an MMEL item rather
than an administrative control item.
25.
"Excess Items": means those items that have been installed that are redundant to the
requirements of the Operating Requirements
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DEFINITIONS AND EXPLANATORY NOTES
1.
"Day of Discovery": is the calendar day an equipment/instrument malfunction was recorded
in the aeroplane maintenance log and or record. This day is excluded from the calendar
days or flight days specified in the MMEL for the repair of an inoperative item of equipment.
This provision is applicable to all MMEL items, i.e., categories "A, B, C, and D."
2.
“Considered Inoperative”: as used in the provisos means that item must be treated for
dispatch, taxi and flight purposes as though it were inoperative. The item shall not be used
or operated until the original deferred item is repaired. Additional actions include:
documenting the item on the dispatch release (if applicable), placarding, and complying
with all remarks, exceptions, and related MMEL provisions, including any (M) and (O)
procedures and observing the repair category.
3.
“Is not used”: in the provisos, remarks or exceptions for an MMEL item may specify that
another item relieved in the MMEL “is not used.” In such cases, crewmembers should not
activate, actuate, or otherwise utilize that component or system under normal operations. It
is not necessary for the operators to accomplish the (M) procedures associated with the
item. However, operational requirements must be complied with, and an additional placard
must be affixed, to the extent practical, adjacent to the control or indicator for the item that
is not used to inform crewmembers that a component or system is not to be used under
normal operations.
4.
“MCTOM”: means the Maximum Certificated Takeoff Mass.
5.
“MAPSC”: means the Maximum Approved Seating Configuration
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HIGHLIGHTS OF REVISION
Note:
Updated entire document’s number scheme to reflect those changes made in 560XL
FAA MMEL Revision 6.
Reformatted blank pages throughout the document.
21-10-05
Moved relief from chapter 33 and added relief for holder assembly.
21-21-04
Revised relief title. Relief was previously listed as Pilot Wemac.
21-21-05
Added new relief for cabin air outlet.
21-30-02
Revised relief.
21-30-02-03
Relief removed for manual control mode.
21-32-01
Clarified relief between pressurized and unpressurized relief.
21-32-02
Clarified relief between pressurized and unpressurized relief.
21-32-03
Revised Remarks and Exceptions, Deleted relief for Manual Mode.
21-33-02
Clarified relief between pressurized and unpressurized relief and added gravel
operation restriction.
21-50-01
Removed unnecessary proviso item.
21-60-01
Removed unnecessary proviso item.
21-62-01
Revised proviso to remove requirement for AFM procedures be followed.
22-10-01
Removed note and incorporated into proviso. Removed A/-/0 relief.
22-10-02
Removed note and incorporated into proviso.
22-10-03
Removed note and incorporated into proviso.
23-10-01
Deleted A/-/0 relief
23-10-01-04
Added relief for HF wire antenna.
23-20-03
Added note.
23-60-01
Added new relief for static wicks
24-21-01
Revised relief to add track engine operating time and maintenance schedule.
25-10-01
Revised title.
25-10-01-03
Combined recline and tilt function relief. Revised Remarks and Exceptions
25-10-01-06
Revised Remarks and Exceptions
25-10-02
Revised proviso and require alternate procedures be established.
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HIGHLIGHTS OF REVISION (Continued)
25-10-05-01
Revised proviso for better definition.
25-10-07
Added relief for cockpit assist handle.
25-20-01
Revised title to include side facing seats. Added lumbar support and incorporated
note 1 into proviso.
25-20-02
Added relief for refreshment center.
25-40-01
Revised relief combining separate relief items into one proviso.
25-60-01
Revised relief to reflect FAA MMEL
25-60-02
Revised relief to reflect FAA policy letter.
25-61-01
Revised title to include crew and passenger.
25-62-01
Revised relief to reflect FAA policy letter.
26-10-01
Revised proviso to remove unnecessary item.
27-20-01
Revised proviso to reflect FAA MMEL.
27-31-01
Removed note and incorporated into proviso.
27-31-02
Added new relief for elevator trim position indicator tip.
27-51-01
Added new relief for flap position indictor tip.
27-60-01
Revised relief to include maximum airspeed restriction.
28-00-01
Removed locking dust cap relief.
28-40-01
Revised proviso adding three day restriction.
28-41-01
Removed relief for wing tank fuel quantity indicating system.
30-00-01
30-30-01
30-30-02
30-30-03
30-30-04
30-40-03
31-10-01
31-10-02
31-50-02
31-50-04-02
31-50-11
31-50-12
31-50-16-01
31-50-20
Revised proviso.
Revised relief to reflect FAA MMEL.
Relief removed for Standby pitot tube heater.
Revised relief to reflect FAA MMEL.
Revised relief to reflect FAA MMEL.
Added relief for surface seal protection system.
Added relief for autopilot mode controller AP button light.
Added new relief for autopilot mode controller YD engage light.
Removed relief for AP engage switch.
Removed relief for battery overtemp.
Removed relief for fuel quantity fault monitoring system.
Revised proviso.
Title revised to add failure to illuminate.
Removed relief for YD engage switch.
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HIGHLIGHTS OF REVISION (Continued)
33-10-01
33-20-01
33-20-03
33-40-01
33-40-10
33-50-02
33-50-03
34-25-06-01
34-25-09
34-44-01
34-44-02
34-45-01
35-00-01
35-00-02
35-00-03
35-20-01
46-00-01
46-00-03
46-00-04
49-20-01
49-50-01
52-10-01
52-10-02
52-10-04
52-10-06
73-30-01
Revised title and proviso.
Revised repair category and provisos.
Revised title and proviso.
Revised proviso requiring other operative lights and repairs made in three flight
days.
Revised repair category, number installed, number required for dispatch, and
proviso.
Relief moved to chapter 25.
Revised titles and added relief.
Revised proviso.
Revised proviso.
Added relief for runway awareness and advisory system.
Revised proviso from 5 further flights to 6.
Added relief for audio functions and airspace selection function.
Revised proviso.
Revised proviso.
Added relief for blowout Disc/Green label.
Reformatted relief for oxygen system, mask, and drop out panel.
Removed (M) procedures.
Relief removed.
Added relief.
Revised proviso.
Revised proviso.
Revised title.
Revised title.
Revised proviso.
Removed cabin door precatch relief.
Revised proviso to removed requirement for both fuel quantity indicating systems be
operative.
XX
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST
INTENTIONALLY LEFT BLANK
CITATION 560XL
23 October 2012
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 21 AIR CONDITIONING
Item
Page: 21-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-21-01
Display Guidance Computer
(DGC) Fan (IC FAN 1 or 2)
(Units 5001 – 6000)
B
2
0 (O) May be inoperative provided operations
are conducted per Aeroplane Flight Manual
limitations and IC FAN 1 or 2 abnormal
procedures.
-21-02
Display Unit (DU) Fan
(DU 1, 2 or 3) Annunciator
(Units 5501 – 6000)
B
3
0 (O) May be inoperative provided operations
are conducted per Aeroplane Flight Manual
limitations and IC FAN 1 or 2 abnormal
procedures.
-21-03
Radome Fan
(Units 5001 – 6000)
C
1
0 (O) May be inoperative provided operations
are conducted per Aeroplane Flight Manual
limitations and RADOME FAN abnormal
procedures including a maximum ground
operation time of 30 minutes with avionics
on.
-21-04
Cockpit Air Outlet
C
-
0
-21-05
Cabin Air Outlet
C
-
0
-21-06
Overhead Cabin
Blower/Wemac Boost Fan
(Units 5001-5500)
C
1
0
-21-07
Cockpit Recirculation Fan
C
1
0
-30-01
Emergency Pressurization
System
C
1
0 (O) May be inoperative provided:
a) Air cycle machine is operative,
b) Both left and right bleed sources are
operative, and
c) Aeroplane is operated at FL 250 or
below.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 21 AIR CONDITIONING
Item
Page: 21-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-30-02
Cabin Pressurization System
C
1
0 (O)May be inoperative provided:
a) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
b) Cabin EMER DUMP is selected ON,
c) Cabin altitude is set to 14,000 feet,
and
d) Aeroplane is operated at 14,000 feet
MSL or below.
-01
Auto Schedule Control Mode
C
1
0 May be inoperative provided:
a) Cabin differential pressure gauge is
operative,
b) Cabin altimeter is operative,
c) Cabin rate indicator is operative, and
d) Aircraft is operated at FL 410 or
below.
-02
Isobaric Control Mode
C
1
0 May be inoperative provided:
a) Cabin differential pressure gauge is
operative,
b) Cabin altimeter is operative,
c) Cabin rate indicator is operative, and
d) Aeroplane is operated at FL 410 or
below.
-03
Manual Control Mode
Deleted revision 1.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 21 AIR CONDITIONING
Item
-32-01
Page: 21-3
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Cabin Differential Pressure
Gauge
-01
(Pressurized)
C
1
0 (O) May be inoperative provided:
a) Cabin altimeter is operative,
b) Either auto schedule or isobaric
control mode is operative, and
c) A chart is provided and used to
convert cabin and aeroplane altitude
to differential pressure.
-02
(Unpressurized)
C
1
0 (O) May be inoperative provided:
a) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
b) Cabin EMER DUMP is selected ON,
c) Cabin altitude is set to 14,000 feet,
and
d) Aeroplane is operated at 14,000 feet
MSL or below.
-32-02
Cabin Altimeter
-01
(Pressurized)
C
1
0 (O) May be inoperative provided:
a) Cabin differential pressure gauge is
operative, and
b) A chart is provided and used to
convert aeroplane altitude and
differential pressure to cabin altitude.
-02
(Unpressurized)
C
1
0 (O) May be inoperative provided:
a) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
b) Cabin EMER DUMP is selected ON,
c) Cabin altitude is set to 14,000 feet,
and
d) Aeroplane is operated at 14,000 feet
MSL or below.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 21 AIR CONDITIONING
Item
-32-03
Page: 21-4
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Cabin Rate Indicator
-01
(Pressurized)
C
1
0 May be inoperative provided:
a) Cabin altimeter is operative,
b) Cabin differential pressure gauge is
operative, and
c) Either autoschedule or isobaric
control mode is operative.
-02
(Unpressurized)
C
1
0 (O) May be inoperative provided:
a) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
b) Cabin EMER DUMP is selected ON,
c) Cabin altitude is set to 14,000 feet,
and
d) Aeroplane is operated at 14,000 feet
MSL or below.
-33-01
Outflow Valve
(Unpressurized)
C
2
0 (M) (O) May be inoperative provided:
a) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
b) At least one valve is removed,
c) PRESS SOURCE selector remains
OFF,
d) Cabin EMER DUMP is selected ON,
e) Cabin altitude is set to 14,000 feet,
and
f) Aeroplane is operated at 14,000 feet
MSL or below.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 21 AIR CONDITIONING
Item
-33-02
Page: 21-5
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Flow Control and Shutoff
Valve
-01
(Unpressurised)
C
2
0 (O) May be inoperative provided:
a) Gravel operations are prohibited,
b) Both flow control and shutoff valves
are verified CLOSED,
c) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
d) PRESS SOURCE selector remains
OFF,
e) Cabin EMER DUMP is selected ON,
f) Cabin altitude is set to 14,000 feet,
and
g) Aeroplane is operated at 14,000 feet
MSL or below.
-02
(Pressurized)
C
2
1 (O) One may be inoperative provided:
a) Right side must be operative for
gravel operations,
b) PRESS SOURCE selector remains
on the operative source,
c) Failed flow control and shutoff valve
is CLOSED, and
d) Aeroplane is operated at FL 250 or
below.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 21 AIR CONDITIONING
Item
Page: 21-6
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-50-01
Air Cycle Machine
(Unpressurized)
C
1
0 (O) May be inoperative provided:
a) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
b) PRESS SOURCE selector remains
OFF,
c) Cabin EMER DUMP is selected ON,
d) Cabin altitude is set to 14,000 feet,
and
e) Aeroplane is operated at 14,000 feet
MSL or below.
-50-02
Freon/R134a Air Conditioning C
System
(Units 5001 – 5500)
(If Installed)
1
0 (M) May be inoperative provided
Freon/R134a air conditioning system is
deactivated.
-60-01
Cockpit/Cabin Air
Temperature Control System
(Unpressurized)
C
1
0 (O) May be inoperative provided:
a) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
b) Cabin PRESS SOURCE selector
remains OFF,
c) Cabin EMER DUMP is selected ON,
d) Cabin altitude is set to 14,000 feet,
and
e) Aeroplane is operated at 14,000 feet
MSL or below.
-01
Automatic Mode
C
2
0 May be inoperative provided the associated
air temperature control system is operative
in manual mode.
-02
Manual Mode
C
2
0 May be inoperative provided the associated
air temperature control system is operative
in automatic mode.
Cabin Temperature Remote
Controller System
D
1
0
-61-01
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 21 AIR CONDITIONING
Item
-62-01
Page: 21-7
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Cabin Temperature Indicator
-01
Without Cabin Occupants
C
1
0
-02
With Cabin Occupants
C
1
0 (O) May be inoperative provided:
a) Alternate means are established and
used to determine cabin
temperature, and
b) Aeroplane is operated per Aeroplane
Flight Manual COLD WEATHER
OPERATIONS, Normal Procedures.
Cockpit Temperature
Indicator
C
1
0
-62-02
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 22 AUTOFLIGHT
Item
Page: 22-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-10-01
Autopilot
B
1
0 (M) (O) One or more functions may be
inoperative provided:
a) For the intended operations, any
increase in crew workload caused by
the inoperative functions has been
considered,
b) Inoperative functions are deactivated
as applicable,
c) Applicable operating minima do not
require its use,
d) The navigation specifications of the
route to be flown do not require their
use, and
e) Aircraft is not operated RVSM.
-10-02
Yaw Damper
B
1
0 (M) (O) May be inoperative provided:
a) Yaw damper is deactivated,
b) Autopilot is considered inoperative,
c) Aircraft is not operated RVSM.
-10-03
Autopilot Disconnect
Functions
(Red, Yoke Mounted Quick
Release Controls)
-01
C
2
1 One may be inoperative for pilot not flying
provided:
a) Autopilot is not used below 1500 feet
AGL, and
b) Approach minimums do not require
use of the autopilot.
-02
B
2
0
(M) (O) May be inoperative provided:
a) Autopilot is considered inoperative,
b) Electric trim is considered
inoperative,
c) Aircraft is not operated RVSM.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 22 AUTOFLIGHT
Item
-10-04
Go-Around Button
Page: 22-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
2
1
C
2
0 May be inoperative provided:
a) Flight director is not used for takeoff
or during go-around, and
b) Autopilot is disconnected for goaround.
NOTE: FMS missed approach procedure
must be activated via the FMS CDU.
-10-05
Autopilot/Flight Director
Touch Control Steering
(TCS or AP SYNC)
C
2
0
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 23 COMMUNICATIONS
Item
Page: 23-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exception
-00-01
VHF Communications
System
C
-
1 May be inoperative provided:
a) COMM 1 is operative, and
b) Aircraft is operated VFR over routes
navigated by reference to visual
landmarks.
-00-02
Flight Phone System
(If Installed)
D
-
0
-01
Cockpit Handset
D
-
0
-02
Cabin Handset
D
-
0
-00-03
Radio Tuning Control on
Cursor Control Panel (CCP)
(Units 6001 and on)
C
2
0 May be inoperative provided direct tuning is
operative on both cockpit display units
(CDUs).
-00-04
SATCOM
(If Installed)
D
-
0 May be inoperative provided procedures do
not require its use.
-00-05
Radio Management Unit
(RMU)
(Units 5001 – 6000)
C
2
1 (O) One may be inoperative provided:
a) Remaining RMU is operative, and
b) Auxiliary com/nav control display unit
is verified operative.
-00-06
Cockpit Voice Recorder
(CVR) (If installed)
A
1
0 One or more may be inoperative provided:
a) The Aeroplane does not exceed 8
further consecutive flights with the
cockpit voice recorder inoperative,
b) A maximum of 72 hours have
elapsed since the cockpit voice
recorder was found to be
inoperative, and
c) Any flight data recorder required to
be carried is operative.
NOTE: This alleviation is not applicable to
combined CVR/FDRs.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 23 COMMUNICATIONS
Item
-10-01
Page: 23-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exception
High Frequency (HF)
Communication System
(If Installed)
-01
D
-
-
Any in excess of those required for the
intended route, may be inoperative.
-02
C
-
1 (O) Any in excess of one may be inoperative
for flight on a route that requires two Long
Range Communication Systems provided:
a) SATCOM air-ground
communications with relevant Air
Navigation Service Provider(s) is
available over the route to be flown,
b) SATCOM voice function is operative,
c) Prior to each flight, coordination with
the appropriate Air Navigation
Service Provider(s) is established
where INMARSAT codes, or
equivalent, are not available whilst
using SATCOM voice function, and
d) Alternate communication procedures
are established and used.
NOTE1:
SATCOM is to be used only as a
backup to normal HF
Communications, unless
otherwise authorized by the
appropriate ATS facilities.
NOTE 2: For all routes, consider the need
for ACAS.
-03
A
-
1 (O) Any in excess of one may be inoperative
for a maximum of 3 calendar days, for flight
on a route that requires two Long Range
Communication Systems provided alternate
communication procedures are established
and used.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 23 COMMUNICATIONS
Item
-10-01
Page: 23-3
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exception
High Frequency (HF)
Communication System
(If Installed) (Continued)
NOTE 1: When the route enters airspace
for which an In Flight Blind
Broadcast Procedure exists,
select the appropriate I.F.B.F.
VHF frequency and apply the
procedure.
NOTE 2: For all routes, consider the need
for ACAS.
-04
High Frequency (HF)
Externally Mounted Wire
Antenna
(If installed)
C
-
0 (M) May be inoperative or missing provided:
a) Antenna and associated mounting
hardware are removed, and
b) High Frequency (HF) communication
system is considered inoperative.
-20-01
Selective Call (SELCAL)
Systems
(If Installed)
-01
D
-
0 May be inoperative provided procedures do
not require its use.
-02
C
-
0 (O) May be inoperative provided alternate
procedures are established and used.
-01
D
-
0 May be inoperative provided procedures do
not require its use.
-02
C
-
0 (O) May be inoperative provided alternate
procedures are established and used.
-20-02
Individual SELCAL
(VHF/UHF/HF) Channel
(If Installed)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 23 COMMUNICATIONS
Item
-20-03
Page: 23-4
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exception
Datalink
(AFIS/ACARS/UNILINK)
(If Installed)
-01
D
-
0 May be inoperative provided procedures do
not require its use.
NOTE: Subscription based service status
does not constitute inoperative
equipment.
-02
C
-
0 (O) May be inoperative provided alternate
procedures are established and used.
NOTE: Subscription based service status
does not constitute inoperative
equipment.
-40-01
Passenger Address (PA)
System
-01
Passenger Configuration
C
1
0 (O) May be inoperative provided alternate
normal, abnormal, and emergency
procedures, and/or operating restrictions are
established.
NOTE: Any function that operates normally
may be used.
-02
Cargo Configuration
D
1
0 May be inoperative provided procedures do
not require its use.
-40-02
Automatic Cabin Briefer
(If Installed)
D
1
0 (O) May be inoperative provided cabin
occupants are briefed by alternate means.
-50-01
Cockpit Overhead
Communication Speaker
C
2
1 One may be inoperative provided:
a) Affected speaker is not required for
procedures, and
b) A headset is installed and used for
associated inoperative speaker
including headset use during
emergency procedures.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 23 COMMUNICATIONS
Item
-50-02
Hand-Held Microphone
-50-03
Headset with Boom
Microphones
-60-01
Static Wick
Page: 23-5
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exception
C
D
2
-
0 May be inoperative provided associated
headset/boom microphone is operative.
-
Any in excess of one headset (including
boom microphone) for each required crew
member on flight deck duty may be missing
or inoperative.
-01
Left Wing
C
6
5 Wingtip static wick must be operative.
-02
Right Wing
C
6
5 Wingtip static wick must be operative.
-03
Empennage Stinger
C
1
0
-04
Airborne Flight Information
system (AFIS) (If installed)
installed)
C
1
0
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 23 COMMUNICATIONS
Item
Revision No: 1
Page: 23-6
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exception
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 24 ELECTRICAL POWER
Item
Page: 24-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-00-01
Ground Power Dispatch
Switch
(If Installed)
C
1
0
-21-01
AC Bearing
(AC BEARING, L or R
annunciator illuminated)
A
2
1 (O) May be inoperative provided:
a) Procedures for tracking engine
operating time on affected side are
established and used, and
b) AC Alternator Bearing maintenance
is accomplished within time limits
required by AC BEARING L or R
annunciator aeroplane flight manual
procedure.
-31-01
Battery Temperature
Indicator
(If Installed)
C
1
0
-35-01
Engine Driven Generator
A
2
1 (O) One may be inoperative provided:
a) Aeroplane is equipped with an APU,
b) APU is operative and used entire
flight,
c) APU generator is verified operative
and is used entire flight,
d) Aeroplane is operated at FL 300 or
below, and
e) Repairs are made within 3 flight
days.
-35-02
Auxiliary Power Unit (APU)
Generating System
(If Installed)
C
1
0 May be inoperative provided APU generator
switch remains off.
-40-01
External Power Receptacle
C
1
0
-50-01
AC Cockpit Outlet
(If Installed)
-01
C
-
0 (O) May be inoperative provided alternate
procedures are established and used.
-02
D
-
0 May be inoperative provided procedures do
not require its use.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 24 ELECTRICAL POWER
Item
Revision No: 1
Page: 24-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 25 EQUIPMENT/FURNISHINGS
Item
Page: 25-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-00-01
Required Documents Holder
(Airworthiness Certificate,
Registration, etc.)
D
1
0 (O) May be missing or inoperative provided
an alternate means of securing and
displaying the documents is used.
-00-02
Security System
(Securaplane) (If Installed)
D
1
0
-10-01
Flight Crew Seat (per seat)
-01 Remain in Aeroplane
C
-
0 May be inoperative provided
a) seat position is acceptable for crew,
and
b) Armrest is stowed in retracted
position.
-02 Removed from Aeroplane
C
-
0 (M) May be inoperative provided seat
position is acceptable to the flight crew
member.
-01
Armrest
NOTE: If an inoperative armrest will hinder
an emergency evacuation or any
other flight duties is should be
removed.
-02
Lumbar Support (If Installed)
C
1
0
-03
Recline/Tilt Function
B
1
0 (M) May be inoperative provided:
a) Affected seat is secured or locked in
a fixed position,
b) Affected seat is failed in a position
that permits normal visibility,
c) Full flight control movement is
available, and
d) Crewmember can reach all
necessary controls and equipment
while restrained.
-04
Restraint Buckle Protective
Padding
(If installed)
C
-
0 May be missing or inoperative.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 25 EQUIPMENT/FURNISHINGS
Item
-10-01
Page: 25-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Flight Crew Seat (per seat)
(Continued)
-05
Thigh Support
(If installed)
C
1
0 May be inoperative provided full flight
control movement is available.
-06
Vertical Adjustment
B
1
0 (M) May be inoperative provided:
e) Affected seat is secured or locked in
a fixed position,
f) Affected seat is failed in a position
that permits normal visibility,
g) Full flight control movement is
available, and
h) Crewmember can reach all
necessary controls and equipment
while restrained.
-10-02
Pilot or Copilot Eye Locator
Reference Ball
C
3
0 (O) May be inoperative or missing provided
alternate procedures are developed and
used for eye position reference.
-10-03
Yoke Mounted Chart Holder
(If Installed)
C
2
0
-10-04
Yoke Mounted Chart Holder
Light (If Installed)
C
2
0
-10-05
Cockpit Flashlight and Holder
Assembly (If Installed)
-01
Flashlight
C
2
0 May be inoperative or missing provided
each required member has an operative
independent portable light readily available
when seated at designated station.
-02
Holder Assembly
C
2
0 May be inoperative provided associated
flashlight is stowed by alternate means.
-10-06
Cockpit Sunvisor System
and/or Attach Mechanism
D
-
0 May be missing or inoperative provided
pilot’s field of vision is not obstructed.
-10-07
Cockpit Assist Handle
D
-
0
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 25 EQUIPMENT/FURNISHINGS
Item
-20-01
Passenger Seat
(Including Side Facing Seats)
Page: 25-3
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
D
-
-
May be inoperative provided:
a) Seat does not block an
emergency exit,
b) Seat does not restrict any cabin
occupant from access to the
aisle,
c) Affected seat(s) are blocked and
placarded "DO NOT OCCUPY",
and
d) A seat with an inoperative
seatbelt is considered
inoperative.
NOTE: Affected seat(s) may include seats
near the inoperative seat(s).
-01
Armrest
-10 With Recline Mechanism
D
-
-
(M) May be inoperative or missing and seat
occupied provided:
a) Armrest does not block an
emergency exit,
b) Armrest does not restrict any
passenger from access to the main
Aeroplane aisle, and
c) If armrest is missing, seat is secured
in the full upright position.
NOTE: Any damage to passenger seats
and components must not be
detrimental to passenger safety.
-20 Without Recline Mechanism
D
-
-
May be inoperative or missing and seat
occupied provided:
a) Armrest does not block an
emergency exit, and
b) Armrest does not restrict any
passenger from access to the main
Aeroplane aisle.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 25 EQUIPMENT/FURNISHINGS
Item
-20-01
-02
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Passenger Seat
(Including Side Facing Seats)
(Continued)
Headrest
C
-
-
May be inoperative and seat occupied
provided headrest is failed in placarded taxi,
takeoff and landing position.
C
-
-
May be missing or inoperative in other than
placarded taxi, takeoff, and landing position
provided affected seat is considered
inoperative.
NOTE:
-03
Page: 25-4
Recline Mechanism
Any damage to passenger seats
and components must not be
detrimental to passenger safety.
C
-
-
May be inoperative and seat occupied
provided seat back is immovable in the
upright position.
D
-
-
(M) May be inoperative and seat occupied
provided seat back is secured in full upright
position.
-04
Floor Tracking Mechanism
C
-
-
May be inoperative and seat occupied
provided
a) Seat base is failed immovable,
b) Seat does not restrict any cabin
occupant from access to the main
aircraft aisle,
c) Seat is positioned so it will not affect
emergency egress.
-05
Seat Tracking and Swivel
Mechanism
C
-
-
May be inoperative and seat occupied
provided seat is failed immovable in
placarded taxi, takeoff and landing position.
-06
Lumbar Support
(If installed)
D
-
-
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 25 EQUIPMENT/FURNISHINGS
Item
-20-02
-01
Page: 25-5
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Refreshment Center
Hot Liquid Storage System
Heater
C
1
0 (M) May be inoperative provided system is
deactivated.
-40-01
Ashtray
A
-
1 Any in excess of one may be inoperative for
three flight days.
-60-01
Emergency Vision Assurance
System (EVAS)
(If Installed)
D
-
0 May be inoperative, missing, or removed if
removal is directed by the EVAS Operator’s
Guide provided procedures do not require
its use.
-60-02
Emergency Medical
Equipment
-01
Automatic External
Defibrillator (AED) and/or
Associated Equipment
(If Installed)
D
-
0 (O) May be incomplete, missing or
inoperative provided AED is resealed in a
manner that will identify it as a unit that
cannot be mistaken for a fully serviceable
unit.
-02
Emergency Medical Kit
(EMK) and/or
Associated Equipment
(If Installed)
D
-
0 (O) May be incomplete, missing or
inoperative provided EMK is resealed in a
manner that will identify it as a unit that
cannot be mistaken for a fully serviceable
unit.
-03
First Aid Kit (FAK) and/or
Associated Equipment
D
-
1 Any in excess of those required may be
incomplete or missing.
Life Jackets
(Crew and Passenger)
(If installed)
D
-
-
-61-01
Any in excess of the minimum required may
be missing or inoperative provided:
a) Inoperative lifejacket is placarded
inoperative, removed from the
installed location and placed out of
sight so it cannot be mistaken for a
functional unit, and
b) Required distribution of serviceable
lifejackets is maintained.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 25 EQUIPMENT/FURNISHINGS
Item
-62-01
Page: 25-6
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Emergency Locator
Transmitter (ELT)
-01
Survival ELT(S)
(If installed)
D
-
-
(M) Any in excess of those required may be
missing or inoperative provided the
inoperative equipment is placarded
inoperative, removed from the installed
location, and placed out of sight so it cannot
be mistaken for a functional unit.
-02
Fixed ELTs
(If installed)
D
-
-
(M) Any in excess of those required by
operating requirements may be missing or
inoperative provided system is deactivated.
A
-
0 May be inoperative provided repairs are
made within 6 further flights or 25 flying
hours, whichever occurs first.
C
-
-
-64-01
Life Raft
(If Installed)
Any in excess of those required may be
missing or inoperative provided the
inoperative equipment is placarded
inoperative, removed from the installed
location, and placed out of sight so it cannot
be mistaken for a functional unit.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 26 FIRE PROTECTION
Item
Page: 26-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-10-01
APU Fire Detection System
(If installed)
C
1
0 May be inoperative provided APU is
considered inoperative
-11-01
Baggage Smoke Detector
(If installed)
C
-
-
Any in excess of those required by
regulations may be inoperative.
-12-01
Lavatory Smoke Detector
(If Installed)
C
-
-
Any in excess of those required by
regulations may be inoperative.
-22-01
Portable Fire Extinguisher
D
-
-
Any in excess of those required by
regulations may be inoperative or missing
provided:
a) Inoperative fire extinguisher is
tagged inoperative, removed from
the installed location and stored out
of sight so it cannot be mistaken for
a functional unit, and
b) Required distribution is maintained.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 26 FIRE PROTECTION
Item
Revision No: 1
Page: 26-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 27 FLIGHT CONTROLS
Item
Page: 27-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-20-01
Rudder Pedal Adjustment
System
B
4
2 (M) (O) May be inoperative provided:
a) Two pedal adjustments are not
inoperative at the 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) Pilot with affected pedal verifies full
control movement and brake
application is available while
restrained, prior to each flight.
-31-01
Electric Trim
B
1
0 (M) (O) May be inoperative provided:
a) Electric trim system is deactivated,
b) Autopilot is considered inoperative,
and
c) Aeroplane is not operated RVSM.
-31-02
Elevator Trim Position
Indicator Tip
C
1
0 (M) May be missing provided an alternate
means of marking Indicator Tip is
established and used.
-42-01
Horizontal Stabilizer Actuator
A
1
0 (M) (O) May be inoperative provided:
a) Horizontal stabilizer is in the
negative (–) 2 degree (takeoff)
position,
b) STAB CONTROL circuit breaker is
pulled and secured,
c) Airspeed is limited to 200 knots/.62
M or less,
d) Touch and go landings are not
conducted,
e) Aeroplane is operated at FL 410 or
below, and
f) Repairs are made within two flight
days.
-51-01
Flap Position Indicator Tip
C
1
0 (M) May be missing provided an alternate
means of marking Indicator Tip is
established and used.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 27 FLIGHT CONTROLS
Item
Page: 27-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-60-01
Speed Brake System
B
1
0 (M) (O) May be inoperative provided:
a) Speed brakes are secured stowed,
b) Aeroplane is operated at 41,000 feet
MSL or below,
c) Maximum airspeed for operation is
limited to Vmo/Mmo of 280 KIAS and
.70 mach respectively, and
d) Steep approaches are not
conducted.
-70-01
Control Lock System
C
1
0 (O) May be inoperative in the unlocked
position provided full flight control and
throttle movement is available.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 28 FUEL
Item
-00-01
-01
Single Point Refueling
System
Page: 28-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
1
0
Locking Dust Cap
Deleted revision 1.
-10-01
Over Wing Refueling Cap
Lock
(If installed)
D
-
0
-40-01
Fuel Low Level Indicating
System
A
2
1 (O) One may be inoperative provided:
a) Procedures for monitoring fuel
quantity are established and used,
and
b) Repairs are made within three flight
days.
-41-01
Wing Tank Fuel Quantity
Indicating System
-43-01
Fuel Temperature Indication
Deleted revision 1.
C
2
1
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 28 FUEL
Item
Revision No: 1
Page: 28-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 30 ICE AND RAIN PROTECTION
Item
Page: 30-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-00-01
Drain Mast Heater
C
-
0 (M) May be inoperative provided:
a) Refreshment center drains and
lavatory basins are not used,
b) Any remaining ice and/or fluid is
removed from the refreshment
center,
c) Hot liquid overfill drain is placarded
“DRAIN HEAT INOP, DO NOT
USE”, and
d) A placard is placed on the instrument
panel stating “Pilot Relief Tube
INOP” and Pilot Relief Tube is not
used.
-00-02
Rosemount Ram Air
Temperature (RAT) Probe
Heater
(Units 5001 – 6000)
C
1
0 May be inoperative provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
b) Aeroplane is not operated in known
or forecast icing conditions.
-10-01
Wing Bleed Air Anti-Ice
System Failed Off
(No Flow)
C
2
1 (M) One may be inoperative provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
b) Aeroplane is not operated in known
or forecast icing conditions.
-10-02
Pneumatic Tail De-Ice
System
C
1
0 May be inoperative provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
b) Aeroplane is not operated in known
or forecast icing conditions.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 30 ICE AND RAIN PROTECTION
Item
-20-01
Page: 30-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Engine Anti-Ice System
-01
Anti-Ice Failed On
(Flow)
C
2
0 (M) (O) May be inoperative provided:
a) Takeoff and landing field
temperatures are not in excess of
+10 degrees C, and
b) If only one system has failed, the
operational system is also selected
ON.
-02
Anti-Ice Failed Off
(No Flow)
C
2
1 (M) One may be inoperative provided:
a) Affected engine anti-ice is secured
for no flow,
b) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
c) Aeroplane is not operated in known
or forecast icing conditions.
-30-01
Pilot and Copilot Pitot Heater
(Standby Excluded)
B
2
1
-30-02
Standby Pitot Tube Heater
-30-03
Pilot and Copilot Pitot Static
Port Heater (Standby
Excluded)
May be inoperative provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or less in flight,
b) Aeroplane is not operated in known
or forecast icing conditions,
c) Aeroplane is operated VFR only, and
d) Aeroplane is not operated at night.
Deleted Revision 1.
B
4
3
(O) One may be inoperative provided:
a) Standby static port heater is verified
operative,
b) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or less in flight,
c) Aeroplane is not operated in known
or forecast icing conditions,
d) Aeroplane is operated VFR only, and
e) Aeroplane is not operated at night.
f) Aeroplane is not operated RVSM.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 30 ICE AND RAIN PROTECTION
Item
Page: 30-3
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-40-01
Rain Removal System
(Forced Air)
C
1
0 May be inoperative provided Aeroplane is
not operated in precipitation within 5 nautical
miles of airport used for takeoff or intended
landing.
-40-02
Windshield Anti-Ice System
C
2
1 One may be inoperative provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or less in flight, and
b) Aeroplane is not operated in known
or forecast icing conditions.
-40-03
Surface Seal Protection
System
C
2
0 May be inoperative provided operations are
not conducted in known or forecast
precipitation within the arrival and departure
areas.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 30 ICE AND RAIN PROTECTION
Item
Revision No: 1
Page: 30-4
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
Page: 31-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-00-01
Quick Access Recorder
(QAR)
(If installed)
C
1
0 (M) (O) May be inoperative for Flight Data
Monitoring (FDM) purposes provided
approved alternate procedures, if
appropriate to other programmes using
associated data, are established and used.
-10-01
Autopilot Mode Controller AP
Button Light
(units 5001-6000)
B
1
0 (O) May be inoperative provided flight crew
verifies AP ON indication is displayed on
both PFDs when the autopilot is engaged.
-10-02
Autopilot Mode Controller YD
Engage Light
(units 5001-6000)
B
1
0 (O) May be inoperative provided flight crew
verifies yaw damper is disconnected prior to
every flight.
-20-01
Auxiliary Power Unit (APU)
Hour Meter
(If installed)
C
1
0 (O) May be inoperative provided APU
operation time is tracked by alternate
means.
-20-02
Clock
C
-
0 May be inoperative provided an accurate
timepiece is operative on the flight deck
indicating the time in hours, minutes, and
seconds.
NOTE: On the basis that the timepiece
required does not need to be
approved, an accurate pilot’s
wristwatch which indicates hours,
minutes, and seconds would be
acceptable.
-20-03
MAX-VIZ EVS-1000
Enhanced Vision System
(EVS)
(If installed)
C
1
0 May be inoperative provided procedures do
not require its use.
-20-04
Flight Hour Meter
C
1
0 (O) May be inoperative provided flight time
is tracked by alternate means.
-20-05
N1 Reminder
(Mechanical or Electric)
(Units 5001 – 6000)
D
1
0
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
Page: 31-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-20-06
Throttle Detent Indicating
Light/Indication
(Units 5001 – 6000)
(If Installed)
D
6
0
-30-01
Flight Data Recorder (FDR)
System (If installed)
A
-
0 One or more may be inoperative provided:
a) The Aeroplane does not exceed 8
further consecutive flights with the
flight data recorder inoperable,
b) Not more than 72 hours have
elapsed since the flight data recorder
was found to be inoperable, and
c) Any cockpit voice recorder required
to be carried is operative.
NOTE1: The flight data recorder is
considered to be inoperative when
any of the following conditions
exist:
a) Loss of the flight recording function
is evident to the flight crew during
the pre-flight check e.g. by means of
a system status monitor, or
b) The need for maintenance has been
identified by the system monitors,
where available, with the setting of
an indicator and the cause of that
setting has not been determined, or
c) Analyses of recorded data or
maintenance actions have shown
that more than 5% of the total
number of individual parameters
(variable and discrete) required to be
recorded for the particular
Aeroplane, are not being recorded
properly.
NOTE 2: Where improper recording affects
5% of the parameters or less,
timely corrective action will need to
be taken by the Aeroplane operator
in accordance with approved
maintenance procedures.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
-50-01
AIR DUCT O'HEAT,
CKPT or CAB
Annunciator
(Units 5001 – 6000)
-50-02
AP ENGAGE Switch
Annunciator
(Units 5001 – 6000)
-50-03
APU Oil Service Light
(If Installed)
-50-04
Battery Overtemp Indication
-01
BATT O'TEMP Annunciator
(Units 5001 – 6000)
-02
BATTERY OVERTEMP Red
CAS Message
(Units 6001 and on)
Page: 31-3
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
2
0 (O) May be inoperative (failure to illuminate)
provided:
a) PRESS SOURCE selector switch
remains OFF,
b) Cabin EMER DUMP is selected on,
c) Cabin altitude is set to 14,000 feet,
and
d) Aeroplane is operated at 14,000 feet
MSL or below.
Moved to ATA 34
C
-
0 (M) (O) May be inoperative (failure to
illuminate) provided:
a) APU oil level is verified prior to each
flight, and
b) APU operating times are tracked.
C
1
0 May be inoperative (failure to illuminate)
provided Aeroplane is equipped with a leadacid battery.
Deleted Rev 1.
-50-05
Cabin Altitude Warning
System Indication
-01
CAB ALT Annunciator
(Units 5001 – 6000)
C
1
0 (O) May be inoperative (failure to illuminate)
provided Aeroplane is operated at 14,000
feet MSL or below.
-02
CABIN ALTITUDE
Red CAS Message
(Units 6001 and on)
C
1
0 (O) May be inoperative (failure to illuminate)
provided Aeroplane is operated at 14,000
feet MSL or below.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
-50-06
Page: 31-4
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Cabin Door Indication
-01
CABIN DOOR
Annunciator
(Units 5001 – 6000)
B
1
0 (O) May be inoperative (failure to illuminate
or extinguish) provided:
a) Lock flags are visible in sight glass
locations in the door,
b) Cabin door vent is verified closed
with the cabin door shut,
c) Internal and external door handles
are verified correctly stowed,
d) Passenger seat belt sign is on for
duration of flight, and
e) Aeroplane is operated at FL 250 or
below.
02
CABIN DOOR Amber CAS
Message
(Units 6001 and on)
B
1
0 (O) May be inoperative (failure to illuminate
or extinguish) provided:
a) Lock flags are visible in sight glass
locations in the door,
b) Cabin door vent is verified closed,
with the cabin door shut,
c) Internal and external door handles
are verified correctly stowed,
d) Passenger seat belt sign is on for
duration of flight, and
e) Aeroplane is operated at FL 250 or
below.
03
Light System (6-Pack)
B
1
0 (O) May be inoperative (failure to illuminate
or extinguish) provided:
a) Lock flags are visible in sight glass
locations in the door,
b) Internal and external door handles
are verified correctly stowed,
c) Cabin door vent is verified closed
with the cabin door shut,
d) Passenger seat belt sign is on for
duration of flight, and
e) Aeroplane is operated at FL 250 or
below.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
-50-07
Page: 31-5
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Cabin Door Seal Indication
-01
DOOR SEAL
Annunciator System
(Units 5001 – 6000)
B
1
0 (O) May be inoperative (failure to illuminate
or extinguish) provided:
a) Door seal inflation is verified prior to
each flight, and
b) Aeroplane is operated at FL 250 or
below.
-02
CABIN DOOR SEAL Amber
CAS Message
(Units 6001 and on)
B
1
0 (O) May be inoperative (failure to illuminate
or extinguish) provided:
a) Door seal inflation is verified prior to
each flight, and
b) Aeroplane is operated at FL 250 or
below.
-50-08
Emergency Pressurization
Indication
-01
EMER PRESS Annunciator
(Units 5001 – 6000)
C
1
0 (M) May be inoperative (failure to illuminate)
provided the emergency pressurization
system is verified operative.
-02
EMERGENCY
PRESSURIZATION
Amber CAS Message
(Units 6001 and on)
C
1
0 (M) May be inoperative (failure to illuminate)
provided the emergency pressurization
system is verified operative.
B
2
1 One may be inoperative (failure to
illuminate) provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
b) Aeroplane is not operated in known
or forecast icing conditions.
-50-09
-01
Engine Anti Ice Indication
ENG ANTI-ICE, L or R
Annunciator
(Units 5001 – 6000)
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
-50-09
Page: 31-6
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Engine Anti Ice Indication
(Continued)
-02
ENG ANTI-ICE COLD,
L - R Amber or White
CAS Message
(Units 6001 and on)
-50-10
Exterior Door Unlocked
Indication
B
2
1 One may be inoperative (failure to
illuminate) provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
b) Aeroplane is not operated in known
or forecast icing conditions.
-01
ACC DOOR UNLOCKED,
NOSE or TAIL
Annunciator System
(Units 5001 – 6000)
C
2
0 May be inoperative (failure to illuminate or
extinguish) provided flight crew verifies by
physical inspection the associated door is
closed and latched before each departure.
-02
NOSE DOOR Amber CAS
Message
(Units 6001 and on)
C
1
0 May be inoperative (failure to illuminate or
extinguish) provided flight crew verifies by
physical inspection the door is closed and
latched before each departure.
-03
TAILCONE ACC DOOR
Amber CAS Message
(Units 6001 and on)
C
1
0 May be inoperative (failure to illuminate or
extinguish) provided flight crew verifies by
physical inspection the door is closed and
latched before each departure.
-04
BATTERY DOOR
Amber CAS Message
(Units 6001 and on)
C
1
0 May be inoperative (failure to illuminate or
extinguish) provided flight crew verifies by
physical inspection the door is closed and
latched before each departure.
-05
AFT BAGGAGE DOOR
Amber CAS Message
(Units 6001 and on)
C
1
0 May be inoperative (failure to illuminate or
extinguish) provided flight crew verifies by
physical inspection the door is closed and
latched before each departure.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
-50-11
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Fuel Quantity Fault
Monitoring System
-01
FUEL GAUGE, L or R
Annunciator
(Units 5001 – 6000)
Deleted Revision 1.
-02
FUEL GAUGE, L – R Amber
CAS Message
(Units 6001 and on)
Deleted Revision 1.
-50-12
Page: 31-7
Generator (DC) Indication
-01
GEN OFF, L or R
Annunciator
(Units 5001 – 6000)
C
2
1 (O) One may be inoperative (failure to
illuminate) provided affected system is
verified operative prior to flight.
-02
DC GENERATOR OFF
L - R Amber CAS Message
(Units 6001 and on)
C
2
1 (O) One may be inoperative (failure to
illuminate) provided affected system is
verified operative prior to flight.
1 (O) May be inoperative (failure to illuminate)
provided hydraulic system operation is
verified with only the affected side engine
operating prior to each flight.
-50-13
Hydraulic Flow Indication
-01
LO HYD FLOW, L or R
Annunciator
(Units 5001 – 6000)
C
2
-02
HYDRAULIC FLOW LOW
Amber CAS Message
(Units 6001 and on)
C
2 1
-50-14
(O) May be inoperative (failure to illuminate)
provided hydraulic system operation is
verified with only the affected side engine
operating prior to each flight.
Hydraulic Fluid Level
Indication
-01
LO HYD LEVEL Annunciator
(Units 5001 – 6000)
C
1
0 (O) May be inoperative (failure to illuminate)
provided adequate fluid level is verified
before each flight.
-02
HYDRAULIC FLUID LEVEL
LOW Amber CAS Message
(Units 6001 and on)
C
1 0
(O) May be inoperative (failure to illuminate)
provided adequate fluid level is verified
before each flight.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
-50-15
Page: 31-8
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Lavatory Door Indication
-01
LAV DOOR
Annunciator System
(Units 5001 – 6000)
B
1
0 (O) May be inoperative (failure to illuminate
or extinguish) provided flight crew verifies
that the lavatory door is latched open prior
to every takeoff and landing.
-02
LAVATORY DOOR
Amber CAS Message
(Units 6001 and on)
B
1
0 (O) May be inoperative (failure to illuminate
or extinguish) provided flight crew verifies
that the lavatory door is latched open prior
to every takeoff and landing.
-50-16
Master Warning/Caution
Light System
-01
Master Warning Light
(Failure to illuminate)
C
2
1
-02
Master Warning Reset
Function
C
2
1
-03
Master Caution Light
C
2
1
-04
Master Caution Reset
Function
C
2
1
B
3
1 (O) May be inoperative (failure to illuminate)
provided:
a) Pitot/static heater systems are
verified operative before each
takeoff,
b) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
c) Aeroplane is not operated in known
or forecast icing conditions.
-50-17
-01
Pitot/Static Heater Indication
P/S HTR, L or R,
or STBY P/S HTR
Annunciators
(Units 5001 – 6000)
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
Page: 31-9
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-50-17
Pitot/Static Heater Indication
(Continued)
-02
PITOT/STATIC COLD
L - R-STBY Amber or White
CAS Message
(Units 6001 and on)
B
2
1 (O) May be inoperative (failure to illuminate)
provided:
a) Pitot/static heater systems are
verified operative before each
takeoff,
b) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
c) Aeroplane is not operated in known
or forecast icing conditions.
-50-18
TAWS Annunciator
(PULL UP, TERRAIN,
BELOW G/S)
(Units 5001 – 5500)
B
-
0 May be inoperative (failure to illuminate)
provided affected aural warning is operative.
-50-19
Wing Anti-Ice Indication
-01
WING ANTI-ICE, L or R
Annunciator
(Units 5001 – 6000)
C
2
1 One may be inoperative (failure to
illuminate) provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
b) Aeroplane is not operated in known
or forecast icing conditions.
-02
WING ANTI-ICE COLD,
L - R Amber or White
CAS Message
(Units 6001 and on)
C
2 1
One may be inoperative (failure to
illuminate) provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below, and
b) Aeroplane is not operated in known
or forecast icing conditions.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 31 RECORD & INDICATING
Item
-50-20
YD ENGAGE Switch
Annunciator
(Units 5001 – 6000)
-50-21
Flight Director Mode Selector
Annunciator
(Units 5001 – 6000)
Page: 31-10
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Moved to ATA 34
C
-
0 (O) May be inoperative provided flight crew
verifies annunciation(s) displayed on the
PFD is appropriate to function selected.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 33 LIGHTS
Item
-10-01
Flight Deck Lighting System
(Excluding Internally Lighted
Annunciators and Buttons,
and Standby Flight
Instrument Lighting)
-10-02
Windshield Ice Detect Light
Page: 33-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
-
-
-01
C
2
1 (O) One may be inoperative provided
alternate procedures are established and
used.
-02
C
2
0 May be inoperative provided aeroplane is
not operated at night.
-01
C
-
0 (O) Individual lights may be inoperative for
night operation 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.
-02
C
-
0 (O) May be inoperative provided:
a) Cabin emergency lighting verified
operative, and
b) No cabin occupants are carried.
-20-01
Individual lights may be inoperative provided
remaining lights are:
a) Sufficient to clearly illuminate all
required instruments, controls, and
other devices for which it is provided,
b) Positioned so that direct rays are
shielded from flight crewmembers
eyes,
c) Lighting configuration and intensity is
acceptable to the flight crew, and
d) Flight deck emergency (flood and
aux panel) lighting is operative.
Cabin Interior Lighting
System
(Excludes Cabin Emergency
Lighting System)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 33 LIGHTS
Item
-20-02
Page: 33-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Divider Accent Light
-01
Incandescent
C
-
-
-02
LED
C
-
-
-01
C
-
-
(O) May be inoperative provided alternate
procedures for notifying cabin occupants are
established and used.
-02
C
-
-
(O) May be inoperative provided:
a) Passenger Address System is
operative and can be clearly heard
throughout the cabin during flight,
and
b) Alternate procedures are established
and used to notify passengers when
seat belts must be fastened and
smoking is prohibited as appropriate.
-03
C
-
0 May be inoperative provided no passengers
are carried.
-
-
-20-03
Cabin Signs
(Fasten Seat Belt and No
Smoking Signs)
(Excludes Cabin Emergency
Lighting System)
-20-04
Exit Sign Lighting
(Incandescent)
C
-20-05
Light Source for Pyramid Exit
Sign (LED)
(Units 5501 and on)
C
-40-01
Anti-Collision Light System
(Strobes)
C
Two light bulbs may be inoperative in each
fixture.
16 14
-
-
May be inoperative provided the Aeroplane
is not operated at night.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 33 LIGHTS
Item
-40-02
Page: 33-3
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Fuselage Mounted
Taxi/Landing Light
-01
C
2
0 May be inoperative provided the Aeroplane
is not operated at night.
-02
C
2
1 50% of taxi lights may be inoperative for
night operations.
C
1
0 (O) May be inoperative for daylight
operations provided all white anti-collision
lights are operative.
-40-03
Ground Recognition Light
(Flashing Beacon)
NOTE:
If the red beacon light is
inoperative, alternative procedures
must be developed and used
when the aeroplane is on the
ground with the engine(s) running.
-40-04
Logo Light
C
2
0
-40-05
Navigation/Position Lights
C
1
0 May be inoperative provided aeroplane is
not operated at night.
-40-06
Pulse Light System
(If Installed)
D
1
0
-40-07
Tail Cone Baggage
Compartment Light
C
3
0
-40-08
Tail Cone Maintenance
Compartment Light
C
1
0
-40-09
Toilet Service Light
C
-
0 (O) May be inoperative provided alternate
procedures are established and used.
-40-10
Wing Illumination/Inspection
Lights
-01
D
-
0 One or more may be inoperative for daylight
operations.
-02
C
2
1 One may be inoperative provided ground
deicing procedures do not require its use.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 33 LIGHTS
Item
-40-11
Page: 33-4
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Wing Leading Edge Landing
Light
-01
C
-
0 All may be inoperative for daylight
operations.
-02
B
2
1 One may be inoperative for night operations
provided fuselage mounted taxi/landing light
on associated side is operative.
-01
C
2
0 May be inoperative provided aeroplane is
not operated at night.
-02
C
2
1
B
3
0 May be inoperative for daylight operations.
-40-12
Wingtip Mounted Recognition
Light
-50-01
Exterior Emergency Light
-50-02
Flight Deck Flashlight
-50-03
Floor Proximity Emergency
Escape Path Marking System
Light
Moved to chapter 25.
-01
Left Forward Half
incandescent bulbs
(Emergency Lighting)
B
-
-
Up to six bulbs (three pairs) may be
inoperative provided no two adjacent pairs
are inoperative.
-02
Left Forward Half LED
(Emergency Lighting)
B
-
-
Up to four elements may be inoperative
within any two foot length.
-03
Left Aft Half
B
-
0
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 33 LIGHTS
Item
-50-03
Page: 33-5
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Floor Proximity Emergency
Escape Path Marking System
Light (Continued)
-04
Right Aft Half incandescent
bulbs
(Emergency Lighting)
B
-
-
Up to six bulbs (three pairs) may be
inoperative provided no two adjacent pairs
are inoperative.
-05
Right Aft Half LED
(Emergency Lighting)
B
-
-
Up to four elements may be inoperative
within any two foot length.
-06
Right Forward Half
B
-
0
LED Light Source for
Emergency Exit
(Escape Hatch)
(If Installed)
C
-50-04
20 17
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 33 LIGHTS
Item
Revision No: 1
Page: 33-6
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
Page: 34-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-00-01
Course Selector Knob
B
2
1 One may be inoperative provided it is not
required by procedures or regulations.
-00-02
Moving Map Display
(If Installed)
C
-
-
-00-03
VHF Navigation System
C
2
0 May be inoperative provided:
a) Procedures do not require its use,
and
b) System is not required by
regulations.
-10 Localizer
C
2
0 May be inoperative provided:
a) Procedures do not require its use,
b) Associated glideslope is considered
inoperative, and
c) System is not required by
regulations.
-20 Glideslope
C
2
0 May be inoperative provided:
a) Procedures do not require its use,
and
b) System is not required by
regulations.
-01
VOR
-02
ILS
May be inoperative provided procedures do
not require its use.
-18-01
Angle of Attack Gauge
(Units 5001 – 5500)
C
1
0
-18-02
Angle of Attack Indexer
C
1
0
-18-03
Angle of Attack Probe Heater
B
1
0 May be inoperative provided:
a) Aeroplane is not operated in visible
moisture with ram air temperature of
+10 degrees C or below,
b) Aeroplane is not operated in known
or forecast icing conditions, and
c) Aeroplane is not operated at night.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
Page: 34-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-20-01
Slip-Skid Indicator (Bezel
mounted inclinometer)
(Units 5001 – 5500)
B
3
1 Two may be inoperative provided each pilot
has either a bezel mounted slip indicator or
a PFD displayed slip indicator.
-23-01
Non-Stabilized Magnetic
Compass (If Installed)
B
1
0 May be inoperative provided:
a) Both AHRS heading information
sources are operative, and
b) Standby HSI heading information is
operative.
-25-01
Display Controller –
Honeywell
-10 Descent Height/Minimum
Descent Altitude Select Knob
(Units 5501 – 6000)
C
2
0 May be inoperative provided procedures do
not require its use.
-15 Elapsed Time Function
Switch
(Units 5001 – 6000)
C
2
0
-20 FMS Source Selector Switch
(Units 5001 – 6000)
C
2
0 May be inoperative provided procedures do
not require its use.
-25 Ground Speed/Time to Go
(GSPD/TTG) Switch
(Units 5001 – 5500)
C
2
0
-30 Horizontal Indicator Mode
Selector Switch (HSI)
(Units 5001 – 6000)
C
2
0 NOTE: Weather radar requirements must
be considered if ARC display
modes are inoperative on both
PFDs and the MFD is inoperative.
-01
Primary Flight Display (PFD)
Controller
(Units 5001 – 6000)
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-25-01
-01
Page: 34-3
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Display Controller –
Honeywell (Continued)
Primary Flight Display (PFD)
Controller
(Units 5001 – 6000)
(Continued)
-35 Preview Switch
(Units 5501 – 6000)
C
2
0
-40 RA/BARO Switch
(Units 5001 – 6000)
(If Installed)
C
2
0 May be inoperative provided the setting
required for intended approach is available.
-45 Radio Altitude Knob
(Units 5001 – 5500)
C
2
0 May be inoperative provided procedures do
not require its use.
-50 Single Cue/Cross Pointer
(SC/CP) Switch
(Units 5001 – 6000)
C
2
0
-55 "STANDARD" Barometer
Pressure Switch
(PUSH STD)
(Units 5501 – 6000)
C
2
0
-60 VOR/Localizer Source
Selector Switch (NAV)
(Units 5001 – 6000)
C
2
-
May be inoperative provided procedures do
not require their use.
NOTE: Aeroplane powers up to the onside
VOR/LOC source, and cannot be
changed. If FMS selected,
VOR/LOC cannot be reselected.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-25-01
-01
Page: 34-4
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Display Controller –
Honeywell (Continued)
Primary Flight Display (PFD)
Controller
(Units 5001 – 6000)
(Continued)
-65 WX/TERR Switch
(Units 5501 – 6000)
C
2
0 NOTE: Weather radar requirements must
be considered if the WX/TERR
switches are inoperative on both
PFDs and the MFD is inoperative.
-70 Bearing Pointer Select Knob
(Units 5001 – 6000)
C
4
0 May be inoperative provided required
bearing pointers are available for
procedures.
-10 Checklist Function Button
(NORM, EMER, RCL, PAG,
SKP, ENT)
(Units 5001 – 5500)
C
6
0
-20 Checklist Function Button
(NORM, EMER, RCL, PAG,
SKP, ESC)
(Units 5501 – 6000)
C
6
0
-30 Data Set Knob
(Units 5501 – 6000)
C
1
0 May be inoperative provided PFD settings
for baro set and metric alt are set correctly
for the intended flight.
-40 ET1/2 and ST1/2 Button
(Units 5501 – 6000)
C
4
0
-02
Multi Function Display (MFD)
Controller – Honeywell
(Units 5001 – 6000)
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-25-01
-02
Page: 34-5
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Display Controller –
Honeywell (Continued)
Multi Function Display (MFD)
Controller – Honeywell
(Units 5001 – 6000)
-50 Joystick Controller (Units
5001 – 5500)
C
1
0
-55 Joystick Controller (Units
5501 – 6000)
C
1
0 May be inoperative provided PFD settings
for baro set and metric alt are set correctly
for the intended flight.
-60 MAP/PLAN SWITCH
(Units 5001 – 6000)
C
1
0
-70 Range Selector
(Units 5001 – 6000)
C
1
0
-80 Symbol Display Button (APT,
VOR, DAT)
(Units 5001 – 5500)
C
3
0
-90 WX SWITCH (Units 5001 –
5500)
C
1
0 May be inoperative provided at least one
PFD HSI switch operates normally.
-95 WX SWITCH (Units 5501 –
6000)
C
1
0 May be inoperative provided at least one
PFD WX/TERR operates normally.
C
1
0 (O) May be inoperative provided:
a) Alternate procedures are established
and used, and
b) All functions of the PFD controllers
are verified operative.
-25-02
Multi-Function Display Unit
(MFD)
(Units 5001 – 6000)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-25-03
Page: 34-6
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Display Controller – Collins
(Units 6001 and on)
-01
Display Control Panel (DCP)
(Units 6001 and on)
B
2
1 (O) One may be inoperative provided
a) Both cursor control panels (CCPs)
are operative,
b) Affected primary flight display (PFD)
is controlled by CCP, and
c) Copilot's multi function display (MFD)
is operative.
-02
Cursor Control Panel (CCP)
(Units 6001 and on)
B
2
1 (O) One may be inoperative provided:
a) Both display control panels (DCPs)
are operative,
b) Affected primary flight display (PFD)
is controlled by DCP, and
c) Copilot's multi function display (MFD)
is operative.
-25-04
Co-Pilot Multi Function
Display (MFD)
(Units 6001 and on)
C
1
0 (O) May be inoperative provided:
a) Alternate procedures are established
and used,
b) All functions of DCPs and CCP
controllers are verified operative, and
c) Right REV switch is set to PFD.
-25-05
Flight Director System
B
2
0 May be inoperative provided:
a) Command bars remain out of view,
b) Approach minimums do not require
use of flight director,
c) Autopilot is considered inoperative,
and
d) Aircraft is not flown RVSM.
-25-06
Flight Director Mode Select
Panel Function
(Units 6001 and on)
C
-
-
Individual functions may be inoperative
provided:
a) Procedures do not require its use,
and
b) AP XFER is operative.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-25-06
Page: 34-7
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Flight Director Mode Select
Panel Function
(Units 6001 and on)
(Continued)
-01
AP (Autopilot)
B
1
0 May be inoperative provided:
a) Autopilot is considered inoperative,
and
b) Aeroplane is not operated RVSM.
-02
YD (Yaw Damper)
B
1
0 May be inoperative provided autopilot and
yaw damper can be engaged via AP push
button.
-25-07
GH-3000 Electronic Standby
Instrument System Heading
Information
(Units 5001 – 6000)
(If Installed)
B
1
0 (M) May be inoperative provided:
a) Both AHRS heading information
sources are operative, and
b) Aeroplane is equipped with an
operative magnetic compass.
-25-08
Standby HSI Heading
Information
(Units 5001 – 6000)
B
1
0 May be inoperative provided:
a) Both AHRS heading information
sources are operative, and
b) Aeroplane is equipped with an
operative magnetic compass.
25-09
Standby Flight Display
(EHSI-4000)
(Units 6001 and on)
B
1
0 (O) May be inoperative provided flight crew
verifies prior to each flight that reversion of
heading information to the GH-3000 has
occurred appropriately.
-34-01
Marker Beacon Receiver
System
C
2
0 May be inoperative provided:
a) Approach procedures do not require
its use, and
b) Not required by regulations.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-35-01
Page: 34-8
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Heads-Up Display (HUD)
(If Installed)
-01
C
-
0 May be inoperative provided procedures do
not require its use.
-02
C
-
0 (O) May be inoperative provided alternate
procedures are established and used.
-42-01
Weather Radar System
C
1
-
May be inoperative provided the weather
reports or forecast available to the
commander indicate that cumulo-numbus
clouds or other potentially hazardous
weather conditions, which could be detected
by the system when in working order, are
unlikely to be encountered on the intended
route.
-44-01
Ground Proximity Warning
System (GPWS)
(If installed)
A
-
0 May be inoperative for a maximum of 6
flights or 25 flight hours or 2 calendar days,
whichever occurs first.
-01
Modes 1 to 4
A
-
0 May be inoperative for a maximum of 6
flights or 25 flight hours or 2 calendar days,
whichever occurs first.
-02
Test Mode
A
-
0 May be inoperative for a maximum of 6
flights or 25 flight hours or 2 calendar days,
whichever occurs first.
-03
Glideslope Deviation
(Mode 5)
-10
B
-
0 May be inoperative.
-20
C
-
0 May be inoperative for day VMC only.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-44-01
Ground Proximity Warning
System (GPWS)
(If installed) (Continued)
-04
Terrain Awareness &
Warning System (TAWS)
(where required)
Page: 34-9
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-10
A
-
0 May be inoperative for a maximum of 10
calendar days provided the GPWS functions
are operative.
-20
A
-
0 May be inoperative for a maximum of 6
flights or 25 flight hours or 2 calendar days,
whichever occurs first.
C
-
0 (O) May be inoperative provided alternate
procedures are established and used.
-05
Advisory Callouts
NOTE: Check Flight Manual limitations for
approach minima.
-06
Windshear Mode
(Reactive)
D
-
0 (O) May be inoperative provided alternate
procedures are established and used.
NOTE: For some designs, these functions
are dealt with by other systems.
-07
Runway Awareness and
Advisory System (RAAS)
C
1
0
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-44-02
Radio Altimeter System
Page: 34-10
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
A
1
0 May be inoperative provided:
a) Approach minimums or operating
procedures do not require its use,
b) GPWS is considered inoperative,
c) ACAS is considered inoperative, and
d) Repairs or replacements are carried
out within 5 further flights or 25 flying
hours or 2 calendar days, whichever
occurs first.
NOTE 1: Landing gear warning system will
function differently without radio
altimeter input.
NOTE 2: Aeroplane 6001 and on, TOPI and
LOPI operation will be affected.
-44-03
Altitude Alerting System
B
-
0 (O) May be inoperative provided an autopilot
with an altitude hold is operative.
NOTE: One altitude alerting system is
required to be operative for RVSM
operations.
-45-01
Airborne Collision Avoidance
System (ACAS)
-01
ACAS System
A
-
0 (M) (O) May be inoperative for a maximum
of 10 calendar days provided the system is
deactivated and secured.
-02
Combined TA and RA Dual
Displays
C
-
1 (O) May be inoperative on the non-flying
pilot side provided:
a) TA and RA elements and audio
functions are operative on flying
pilot’s side, and
b) TA and RA display indications are
visible to the non-flying pilot.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-45-01
-03
Page: 34-11
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Airborne Collision Avoidance
System (ACAS) (Continued)
Resolution Advisory (RA)
Display System(s)
-10
C
-
1 (O) One may be inoperative on the nonflying pilot side.
-20
C
-
0 (O) One or more may be inoperative
provided:
a) All Traffic Alert (TA) display elements
and voice command audio functions
are operative, and
b) TA only mode is selected by the
crew.
-10
C
-
0 (O) One or more may be inoperative
provided all installed RA display and audio
functions are operative.
-20
C
-
1 One may be inoperative on non-flying pilot
side.
-04
Traffic Alert (TA) Display
System(s)
-05
Audio Functions
B
1
0 May be inoperative provided ACAS is
considered inoperative.
-06
Airspace Selection Function
(If installed)
C
-
0
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
Page: 34-12
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-46-01
Lightning Detection System
(If Installed)
C
1
-
Any in excess of those required by
regulations may be inoperative.
-51-01
Distance Measuring
Equipment (DME) Systems
D
-
-
Any in excess of those required by
regulations may be inoperative.
-52-01
SSR Transponder
-10
C
-
-
Any in excess of those required for the route
to be flown may be inoperative.
-20
A
-
0 (O) May be inoperative for a maximum of 5
flights provided:
a) Permission is obtained from the Air
Navigation Service Provider(s) along
the route or any planned diversion,
and
b) Flight is conducted under VFR over
routes navigated by reference to
visual landmarks.
-01
Mode A/C Functions
NOTE: Mode C function is required to be
operative for RVSM operations.
-02
-10
Mode S Function
D
-
0 Any in excess of those required for the
intended route, may be inoperative.
NOTE:
-20
C
-
A SSR transponder with an
operative Mode S function is
defined as a transponder which
can provide, at least, Elementary
Surveillance capability.
0 One or more may be inoperative provided
permission is obtained from the Air
Navigation Service Provider(s) when
required for the intended route.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-52-01
Page: 34-13
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
SSR Transponder
(Continued)
NOTE 1: An SSR transponder with an
operative Mode S function is
defined as a transponder which
can provide, at least Elementary
Surveillance capability.
NOTE 2: Altitude reporting provided by an
SSR transponder Mode S
function is required for ACAS
operation.
NOTE 3: Altitude reporting provided by an
SSR transponder Mode S
function is required for flight into
RVSM airspace.
-03
Enhanced Surveillance
Functions (If installed)
-10
D
-
0 One or more Downlinked Aeroplane
Parameters (DAP’s), which provide
Enhanced Surveillance, may be inoperative
when not required for the intended route.
-20
C
-
0 One or more Downlinked Aeroplane
Parameters (DAP’s), which provide
Enhanced Surveillance, may be inoperative
when required for the intended route.
-55-01
Automatic Direction Finding
(ADF) System
D
-
-
Any in excess of those required by
regulations may be inoperative.
-57-01
Global Positioning System
(GPS/GNSS/SBAS)
C
-
-
Any in excess of those required by operating
requirements may be inoperative.
NOTE: Enhanced function of TAWS may
not be available.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-60-01
Flight Management System
(FMS)
Page: 34-14
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
-
-
Any in excess of those required by
regulations may be inoperative provided
functions are not required by other
procedures.
NOTE: Enhanced function of TAWS may
not be available.
-01
Navigation Database
(If installed)
NOTE: Any out of date
Database is to be
inoperative.
-10
C
-
-
(O) May be out of currency provided:
a) Current aeronautical information
(e.g. charts) is available for the entire
route and for the aerodromes to be
used, and
b) Navigation database information is
disregarded.
-20
C
-
1 Any in excess of one may be inoperative
provided the operative database is:
a) Up to date for routes, departures,
arrival and approach procedures that
require the use of navigation
Database for RNAV, and
b) This up to date Database is readily
available to the flight crew
member(s) responsible for
navigation.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-60-01
-01
-30
Page: 34-15
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Flight Management System
(FMS) (Cont.)
Navigation Database
(If installed) installed) (Cont.)
A
-
0 (O) One or more may be out of date for a
maximum of 10 calendar days provided:
a) Area Navigation (RNAV) departure,
arrival and approach procedures do
not depend on the data amended in
the current database cycle,
b) Before each flight, current
aeronautical information is used to
verify database Navigation Fixes,
coordinates, frequencies, status (as
applicable) and suitability of
Navigational Facilities required for
the intended route, and
c) Radio navigation aids, which are
required to be flown for departure,
arrival and approach procedures,
and which have been amended in
the current database cycle, are
manually tuned and identified.
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 34 NAVIGATION
Item
-60-01
-01
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Flight Management System
(FMS) (Cont.)
Navigation Database
(If installed) (Cont.)
-40
-02
Page: 34-16
Fuel Planning and Indicating
Function
A
-
0 (O) One or more may be out of date for a
maximum of 10 calendar days provided:
a)
Conventional (non-RNAV) departure,
arrival and approach procedures,
(when available), or ANSP
assistance are used as an
alternative to RNAV procedures
which have been amended in the
current database cycle,
b)
Before each flight, current
aeronautical information is used to
verify the database Navigation Fixes,
the coordinates, frequencies, status
(as applicable) and suitability of
Navigational Facilities required for
the intended route, and
c)
Radio navigation aids, which are
required to be flown for departure,
arrival and approach procedures and
which have been amended in the
current database cycle, are manually
tuned and identified.
C
-
-
May be inoperative provided fuel flow
indicating systems are operative.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 35 OXYGEN
Item
Page: 35-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-00-01
Oxygen Tank Fill Port
C
-
0 (M) May be inoperative provided bottle is
filled using alternate means, if service is
required.
-00-02
Oxygen Servicing Panel
Pressure Gauge
C
-
0 (M) May be inoperative provided alternate
procedures are used for servicing oxygen
system.
-00-03
Blowout Disc/Green Label
C
1
0 (O) May be missing or damaged provided
oxygen pressure is verified prior to each
flight.
-10-01
EROS Crew Oxygen Mask
Tension Control System
(If installed)
C
-
0 (O) May be inoperative provided oxygen
mask is verified operative prior to each
flight.
-20-01
Passenger Oxygen System
C
1
0 May be inoperative provided:
a) Aeroplane is operated without cabin
occupants, and
b) Crew oxygen system is operative.
-01
Mask
B
-
0 Individual oxygen masks or dispensers may
be inoperative or missing provided
associated seats are placarded “DO NOT
OCCUPY”.
-02
Drop Out Panel
B
-
0 (M) Individual panels may be out of normal
position provided:
a) Oxygen masks and drop out panel
are removed, and
b) Associated seats are placarded “DO
NOT OCCUPY”.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 35 OXYGEN
Item
-30-01
Protective Breathing
Equipment (PBE)
(If installed)
Page: 35-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
D
-
-
(M) (O) Any in excess of those required may
be inoperative or missing provided:
a) Required distribution of operative
unit is maintained throughout the
Aeroplane,
b) The inoperative PBE and its location
are placarded inoperative, removed
from the Aeroplane or retained in an
approved stowage or out of sight
location so it cannot be mistaken for
a functional unit, and
c) Procedures are established and
used to alert crew members of
inoperative or missing equipment.
NOTE: Some PBEs may be considered
hazardous material if they are
inoperative, and contain oxygen
generators or compressed gas.
-30-02
Portable Oxygen Bottles
C
-
-
Any in excess of those required by
regulations may be inoperative:
a) Required distribution of serviceable
bottles is maintained throughout the
Aeroplane, and
b) Bottles not properly serviced are
replaced, serviced, or removed at
the next available maintenance
facility.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 38 WATER/WASTE
Item
-00-01
Overboard Drain
-10-01
Potable Water Systems
-01
Page: 38-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
-
-
(M) May be inoperative provided the system
associated with the drain has been drained
and deactivated.
C
-
-
(M) Individual components may be
inoperative provided:
a) Associated components are
deactivated or isolated, and
b) Associated system components are
verified not to have leaks.
NOTE: Any portion of the system operating
normally may be used.
-02
-30-01
Lavatory Waste Systems
C
-
-
(M) May be inoperative provided:
a) System is drained, and
b) Procedures are established to
ensure system is not serviced.
C
-
-
(M) Individual components may be
inoperative provided:
a) Associated components are
deactivated or isolated, and
b) Associated system component is
verified not to have leaks.
NOTE: Any portion of the system operating
normally may be used.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 38 WATER/WASTE
Item
Revision No: 1
Page: 38-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 45 MAINTENANCE COMPUTER
Item
-00-01
Maintenance Diagnostic
Computer (MDC) System
(Units 6001 and on)
Page: 45-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
1
0 May be inoperative provided procedures do
not require its use.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 45 MAINTENANCE COMPUTER
Item
Revision No: 1
Page: 45-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 46 INFORMATION SYSTEMS
Item
-00-01
Electronic Flight Bag (EFB)
System
(If installed)
-01
Class 3 EFBs
Integrated Flight Information
System (IFIS) (Units 6001
and on) Advanced File
Graphics Server
(Units 5501 – 6000)
Page: 46-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
-
-
(O) May be inoperative provided alternate
procedures are established and used.
NOTE: Any function, program or document
which operates normally may be
used.
-02
Data Connectivity
(Class 2)
(if installed)
C
-
-
(O) May be inoperative provided alternate
procedures are established and used.
-03
Power Connection
(Class 1 & 2)
(If installed)
C
-
-
(O) May be inoperative provided alternate
procedures are established and used.
-04
Mounting Device
(Class 2)
(If installed)
C
-
0 (M) (O) May be inoperative provided:
a) Associated EFB and hardware is
secured by an alternate means or
removed from the aeroplane, and
b) Alternate procedures are established
and used.
-00-02
Electronic Checklist System
(If installed)
D
-
0 May be inoperative provided equivalent
checklist is available.
-00-03
Integrated Flight Information
system (IFIS)
(Units 6001 and on)
Deleted Revision 1.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 46 INFORMATION SYSTEMS
Item
-00-04
Page: 46-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Dedicated EFB Power
Connection (does not include
AC Cockpit Outlet) (If
installed)
-01
C
-
0 (O) May be inoperative provided alternate
procedures are established and used.
-02
D
-
0 May be inoperative provided procedures do
not require its use.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 49 AIBORNE AUXILIARY
Item POWER
Page: 49-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
-20-01
Auxiliary Power Unit (APU)
(If Installed)
C
1
0 (M) May be inoperative provided:
a) APU is deactivated, and
b) Procedures do not require its use.
-30-01
APU Fuel Shutoff Valve
(If Installed)
C
1
0 (M) May be inoperative provided:
a) Valve is verified closed,
b) Valve is deactivated, and
c) APU is considered inoperative.
-50-01
APU Bleed Air Valve
(If Installed)
C
1
0 (O) May be inoperative provided:
a) Valve is verified closed, and
b) APU system BLEED AIR switch
remains off.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 49 AIBORNE AUXILIARY
Item POWER
Revision No: 1
Page: 49-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 52 DOORS
Item
-00-01
Page: 52-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Cockpit Divider Door/Curtain
-01
Divider Door
C
2
0 May be inoperative provided door remains
secured open.
-02
Curtain
C
2
0 May be missing or inoperative provided
curtain remains secured open.
-10-01
Cabin Door Primary Seal
-01
(Pressurized)
C
1
0 (O) May be inoperative provided:
a) Primary seal does not interfere with
door operation,
b) Secondary door seal is verified
intact, and
c) Aeroplane is operated at FL 250 or
below.
-02
(Unpressurized)
C
1
0 (O) May be inoperative provided:
a) Primary seal does not interfere with
door operation,
b) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
c) Cabin EMER DUMP is operative and
selected to ON,
d) Cabin altitude is set to 14,000 feet,
and
e) Aeroplane is operated at 14,000 feet
MSL or below.
C
1
0 (O) May be inoperative provided:
a) Secondary seal does not interfere
with door operation,
b) Primary door seal is verified
operative, and
c) Aeroplane is operated at FL 250 or
below.
-10-02
-01
Cabin Door Secondary Seal
(Pressurized)
(Continued)
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 52 DOORS
Item
-10-02
-02
Page: 52-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Cabin Door Secondary Seal
(Continued)
(Unpressurized)
C
1
0 (O) May be inoperative provided:
a) Secondary seal does not interfere
with door operation,
b) Procedures for flight planning at
lower altitudes and supplemental
oxygen use are established and
used,
c) Cabin EMER DUMP is operative and
selected to ON,
d) Cabin altitude is set to 14,000 feet,
and
e) Aeroplane is operated at 14,000 feet
MSL or below.
-10-03
Cabin Door Acoustic Seal
C
1
0
-10-04
Cabin Door Key Lock
D
1
0 May be inoperative in the unlocked position.
-10-05
Cabin Vent Door
C
1
0 (O) May be inoperative provided vent door is
manually closed using appropriate AFM
procedure prior to each flight.
-10-06
Cabin Door Precatch
-30-01
Baggage Compartment Door
Key Lock
D
1
0 May be inoperative in the unlocked position.
-40-01
Left Nose Avionics
Compartment Key Lock
D
1
0 May be inoperative in the unlocked position.
-40-02
Right Nose Avionics
Compartment Key Lock
D
1
0 May be inoperative in the unlocked position.
-40-03
Tailcone Maintenance
Access Door Key Lock
D
1
0 May be inoperative in the unlocked position.
-42-01
Battery Compartment Door
Key Lock for 560-5001 thru
5187, which do not have
SB560XL-52-09 incorporated
(If Installed)
D
1
0 May be inoperative in the unlocked position.
Deleted Revision 1.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 52 DOORS
Item
-46-01
Page: 52-3
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
Single Point Refueling
System Door Key Lock
-01
D
1
0 May be inoperative in the unlocked position.
-02
D
1
0 May be inoperative in the locked position
provided over wing refueling cap locks are
not failed in locked position.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 52 DOORS
Item
Revision No: 1
Page: 52-4
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 73 ENGINE FUEL & CONTROL
Item
-30-01
Fuel Flow Indicating System
Page: 73-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
A
2
1 One may be inoperative provided repairs
are made within three flight days.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 73 ENGINE FUEL & CONTROL
Item
Revision No: 1
Page: 73-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 76 ENGINE CONTROLS
Item
-00-01
Electronic Engine Control
(EEC)
(Units 5001 – 6000)
Page: 76-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
2
0 (O) May be inoperative provided
a) Both EEC switches are set to
MANUAL to provide matched
throttles and similar engine
response,
b) Operations are conducted in
accordance with AFM Supplement,
and
c) Engine synchronizer system is
considered inoperative.
NOTE: Units 6001 and on cannot dispatch
with any ENGINE FAULT CAS
Message illuminated.
-01-01
Engine Synchronizer System
C
1
0 May be inoperative failed off.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 76 ENGINE CONTROLS
Item
Revision No: 1
Page: 76-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 77 ENGINE INDICATING
Item
-14-01
Page: 77-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
N1 Indicators
-01
N1 Digital Display Indicator
(Units 5001 – 6000)
B
2
1 One may be inoperative provided:
a) Corresponding N1 tape display is
operative,
b) All other engine indicators are
operative, and
c) EEC auto mode with throttle detents
is operative.
-02
N1 Tape Display Indicator
(Units 5001 – 6000)
B
2
1 One may be inoperative provided:
a) Corresponding digital display is
operative,
b) All other engine indicators are
operative, and
c) EEC auto mode with throttle detents
is operative.
-32-01
Engine Vibration Monitor
System
B
2
1 One may be inoperative provided no
abnormal vibration exists.
NOTE: White ENG VIB annunciator/CAS
message may be
annunciated/displayed.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 77 ENGINE INDICATING
Item
Revision No: 1
Page: 77-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Revision No: 1
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 78 ENGINE EXHAUST
Item
-30-01
Thrust Reverser
Page: 78-1
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
C
2
0 (M) May be inoperative provided thrust
reverser(s) is secured in the forward thrust
position.
EUROPEAN AVIATION SAFETY AGENCY
23 October 2012
MASTER MINIMUM EQUIPMENT LIST
Cessna Citation 560XL
(1) System & Sequence Numbers
ATA 78 ENGINE EXHAUST
Item
Revision No: 1
Page: 78-2
(2) Rectification Interval
(3) Number Installed
(4) Number required for dispatch
(5) Remarks or Exceptions
INTENTIONALLY LEFT BLANK