Cessna
Operational &
Maintenance
Procedures
CESSNA CE-560XL
THIS GUIDE IS CURRENT WITH THE MASTER MINIMUM EQUIPMENT LIST WHICH
IS ISSUED BY THE EUROPEAN AVIATION SAFETY AGENCY - REVISION 1 DATED
23 Oct, 2012, FOR THE ABOVE AEROPLANE OF THIS TYPE AS CERTIFIED BY THE
EUROPEAN AVIATION SAFETY AGENCY.
COPYRIGHT © 2012
23 Oct, 2012
CESSNA AIRCRAFT COMPANY
REVISION 1
WICHITA, KANSAS, USA
56XCOMPEU-01-00
56XCOMPEU-01-00
NOTICE
The Master Minimum Equipment List (MMEL) is issued by the European Aviation
Safety Agency for Aeroplane certified by the European Aviation Safety Agency
and operated under jurisdiction of European Aviation Safety Agency member
states National Authorities. This Master Minimum Equipment List OPERATIONAL
PROCEDURE and MAINTENANCE PROCEDURE Manual contains only the items
from the Master Minimum Equipment List, which have Operational (O) or
Maintenance (M) procedure requirements. Cessna does not support Minimum
Equipment List items not published in the MMEL.
Cessna’s policy is to revise this manual only to accommodate changes to a new
MMEL revision, which requires a change to, or a new, Operational (O) or
Maintenance (M) required procedure. If a revised MMEL is released, but does not
affect any required procedure, the Operational and Maintenance manual will not
be revised at that time. Cessna reserves the right to make format changes without
generating a new revision.
Operational (O) and Maintenance (M) procedures in this manual are recommended
by Cessna Aircraft Company. Most of the procedures in this guide have been
approved in some MEL’s. This document is not EASA approved, but is intended to
aid operators in writing and gain approval for their specific Minimum Equipment
List (MEL). The operator is responsible to make sure that all crew members are
properly trained in the use of MEL (O) and (M) procedures.
56XCOMPEU-01-00
i
For all provisos – unless the proviso requires a system to be verified, it is
assumed that all other systems are operative and no action is required to test
these systems.
Where ever a dash (-) is listed in column 2. Number installed or column 3. Number
required for dispatch, it is the responsibility of the operator to replace the dash (-)
with the actual number of each item, if any, installed on the aeroplane in question.
All inoperative items must be placarded in accordance with the applicable
operating regulations.
1. Placard(s) shall be placed above, adjacent to or on the affected/inoperative
annunciator, circuit breaker, control, component, gauge, indicator, knob,
light or switch. For missing equipment, a placard shall be placed so that all
personnel are made aware of the missing equipment.
2. If the inoperative equipment is not within view of the flight crew, an
additional placard shall be installed on the instrument panel in view of the
pilot(s) indicating the inoperative item and/or limitation(s).
Make an appropriate entry in the discrepancy report for each inoperative item.
Diagrams, drawings and/or pictures in this document may not reflect all possible
installations. Refer to the aeroplane equipment list, continuous history report
and/or STC for current installed equipment.
56XCOMPEU-01-00
ii
The MMEL may contain relief associated with a STC not supported by Cessna
Aircraft Co. For these relief items, Cessna will not provide a maintenance
procedure, operational procedure and/or placarding procedure. Operators will
need to contact the holder of the STC for MEL support.
The code of federal regulations, title 14, aeronautics and space, listed in this
document may not be up-to-date with the most current federal aviation
regulations. It is the responsibility of the operator to make sure all applicable 14
CFR parts are listed in their operational documents.
The maintenance procedures in this document may be different than those found
in the current revision of the Cessna maintenance manual for the associated
aeroplane model. In the event of conflict, use the more restrictive maintenance
procedure to accomplish the task.
56XCOMPEU-01-00
iii
Page Intentionally Left Blank
56XCOMPEU-01-00
iv
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-21-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Display Guidance Computer (DGC) Fan (IC FAN 1 or 2) (Units 50016000)
B/2/0
(O) May be inoperative provided operations are conducted per Aeroplane Flight Manual
limitations and IC FAN 1 or 2 abnormal procedures.
OPERATIONAL PROCEDURE
NOTE: Ground operation time is defined as anytime the avionics are being
powered for taxi, takeoff and landing.
Prior to engine start, the flight crew shall review the Abnormal Procedure for IC FAN 1
OR 2 (DISPLAY GUIDANCE COMPUTER COOLING FAN FAILURE DISPLAYED ON
MFD).
PLACARDING PROCEDURE
Place a placard stating “DGC FAN INOP” on instrument panel in front of both pilots.
21-21-02
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.
OPERATIONAL PROCEDURE
NOTE: Ground operation time is defined as anytime the avionics are being
powered.
Prior to engine start, the flight crew shall review the Abnormal Procedure for DU FAN 1,
2 OR 3 (DU FAN FAIL MESSAGE DISPLAYED ON MFD).
PLACARDING PROCEDURE
Place an INOP placard on the affected annunciator.
56XCOMPEU-01-00
21-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-21-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
NOTE: Ground operation time is defined as anytime the avionics are being
powered.
Prior to engine start, the flight crew shall review the Abnormal Procedure for RADOME
FAN (RADOME FAN FAILURE).
PLACARDING PROCEDURE
Place a placard stating “RADOME FAN INOP” on instrument panel in front of both pilots.
21-21-04
Cockpit Air Outlet
C/-/0
PLACARDING PROCEDURE
Place an INOP placard above/adjacent to affected Wemac.
21-21-05
Cabin Air Outlet
C/-/0
PLACARDING PROCEDURE
Place an INOP placard above/adjacent to affected Wemac.
21-21-06
Overhead Cabin Blower/Wemac Boost Fan (Units 5001-5500)
C/1/0
PLACARDING PROCEDURE
Place an INOP placard above the WEMAC BOOST switch.
56XCOMPEU-01-00
21-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-21-07
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cockpit Recirculation Fan
C/1/0
PLACARDING PROCEDURE
Place an INOP placard above the CKPT RECRC switch.
21-30-01
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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. MEA’s shall be taken into account for planned route.
3. Position Aeroplane in a suitable run-up area and chock both main landing gear.
4. Using AFM Normal Procedures, start the engines.
5. Place PRESS SOURCE select knob to OFF and verify no airflow through
wemacs.
6. Place PRESS SOURCE select knob to LH and verify airflow through cabin
wemacs.
7. Place PRESS SOURCE select knob to RH and verify airflow through cockpit
wemacs.
8. Place PRESS SOURCE select knob to NORM.
PLACARDING PROCEDURE
Place a placard stating “EMER PRESS INOP” adjacent to PRESS SOURCE controller.
56XCOMPEU-01-00
21-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-30-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning shall consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s shall be taken into account for planned route.
PLACARDING PROCEDURE
Place a placard stating “CABIN PRESSURIZATION INOP” above pressurization
controls.
56XCOMPEU-01-00
21-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-30-02-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Pressurization System 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) Aeroplane is operated at FL 410 or below.
PLACARDING PROCEDURE
Place a placard stating, “AUTO SCHEDULE INOP” above pressurization controls.
56XCOMPEU-01-00
21-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-30-02-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Pressurization System 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.
PLACARDING PROCEDURE
Place a placard stating “ISOBARIC MODE INOP” above pressurization controls.
56XCOMPEU-01-00
21-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-32-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Differential Pressure Gauge (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.
OPERATIONAL PROCEDURE
1. Refer to the conversion chart at the end of this section.
2. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place a placard stating “DIFF PRESS INOP” adjacent to the gauge.
56XCOMPEU-01-00
21-7
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-32-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Differential Pressure Gauge (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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning shall consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s shall be taken into account for planned route.
4. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place a placard stating “DIFF PRESS INOP” adjacent to the gauge.
56XCOMPEU-01-00
21-8
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-32-02-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Altimeter Pressurized flight
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.
OPERATIONAL PROCEDURE
1. Refer to the conversion chart at the end of this section.
2. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place a placard stating “CAB ALT INOP” adjacent to the gauge.
56XCOMPEU-01-00
21-9
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-32-02-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Altimeter (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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning shall consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s shall be taken into account for planned route.
4. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place a placard stating “CABIN ALT INOP” adjacent to the gauge.
56XCOMPEU-01-00
21-10
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-32-03-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Rate Indicator Pressurized flight
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.
PLACARDING PROCEDURE
Place an INOP placard on the rate indicator.
56XCOMPEU-01-00
21-11
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-32-03-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Rate Indicator Unpressurized flight
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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower
altitude and affect on range.
2. Flight planning shall consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s shall be taken into account for planned route.
4. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place an INOP placard on the affected gauge.
56XCOMPEU-01-00
21-12
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-33-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
NOTE:
If removing RH outflow valve, Cessna recommends removing the
aluminum tube that vents the vacuum ejector overboard through aft
pressure bulkhead and particulate trap aluminum tube that leads from
RH outflow valve to ejector. Cap all fittings and plug all lines. It should
not be necessary to disturb nylon plumbing.
1. Using the most current revision to the 560XL Maintenance Manual, section 2130-00 – PRESSURIZATION CONTROL – MAINTENANCE PRACTICES,
access either the primary or secondary outflow valve.
2. Remove the outflow valve from the Aeroplane. Cap all fittings, place outflow
valve in a bag and store in the baggage area for transport.
3. Cap, bag and stow all connectors/fittings on Aeroplane.
4. Reinstall all access areas and furnishings.
5. Re-engage the CABIN PRESSURE circuit breaker.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning shall consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s shall be taken into account for planned route.
4. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place a placard stating “OUTFLOW VALVES INOP” on the pressurization panel.
56XCOMPEU-01-00
21-13
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-33-02-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flow Control and Shutoff Valve (Unpressurized)
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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning shall consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s shall be taken into account for planned route.
4. Position Aeroplane in suitable run-up area and chock both main landing gear.
5. Using AFM Normal Procedures, start engine(s) supplying bleed air to failed flow
control and shutoff valve(s).
6. Select CKPT RECIRC OFF.
7. 560XL units 5001 thru 5372:
a. For Non-APU equipped Aeroplane, place AC-FANS knob to OFF.
b. For APU equipped Aeroplane, place FAN knob to OFF.
8. Turn PRESS SOURCE knob to OFF and verify valves are CLOSED. Absence of
wemac flow indicates valve is CLOSED. Leave PRESS SOURCE OFF for flight.
9. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place a placard stating “ACM INOP” above pressurization controls.
56XCOMPEU-01-00
21-14
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-33-02-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flow Control and Shutoff Valve (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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. MEA’s shall be taken into account for planned route.
3. Position Aeroplane in a suitable run-up area and chock main landing gear. If the
Aeroplane is preparing for dispatch, the crew may taxi the Aeroplane to a
suitable run-up area and set the PARK BRAKE. If crew taxis Aeroplane, proceed
to step 5.
4. Using AFM Normal Procedures, start both engines.
5. Place the CKPT RECIRC switch to OFF.
6. Place PRESS SOURCE select knob to OFF and verify no airflow through
wemacs.
7. Place PRESS SOURCE select knob to operative side and verify airflow through
wemacs.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SIDE) FLOW CONTROL AND SHUTOFF VALVES
INOP” adjacent to pressurization controller.
56XCOMPEU-01-00
21-15
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-50-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning shall consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s shall be taken into account for planned route.
4. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place a placard stating “ACM INOP” above pressurization controls.
56XCOMPEU-01-00
21-16
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-50-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Freon/R134a Air Conditioning System (Units 5001-5500) (If installed)
C/1/0
(M) May be inoperative provided Freon/R134a air conditioning system is deactivated.
MAINTENANCE PROCEDURE
Pull and secure AIR COND circuit breaker.
PLACARDING PROCEDURE
Place INOP placard adjacent to air conditioner controls.
56XCOMPEU-01-00
21-17
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-60-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cockpit/Cabin Air Temperature Control 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 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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning shall consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s shall be taken into account for planned route.
4. Set the pressurization controller as indicated in the proviso.
PLACARDING PROCEDURE
Place a placard stating “TEMP CONTROL INOP” on the temperature control panel.
56XCOMPEU-01-00
21-18
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-60-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cockpit/Cabin Air Temperature Control System Automatic Mode
C/2/0
May be inoperative provided the associated air temperature control system is operative
in manual mode.
PLACARDING PROCEDURE
Place an INOP placard above the AUTO section of the affected side (CKPT/CABIN)
temp selector knob.
21-60-01-02
Cockpit/Cabin Air Temperature Control System MANUAL Mode
C/2/0
May be inoperative provided the associated air temperature control system is operative
in automatic mode.
PLACARDING PROCEDURE
Place an INOP placard below the Manual section of the affected side (CKPT/CABIN)
temp selector knob.
56XCOMPEU-01-00
21-19
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-61-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Temperature Remote Controller System
D/1/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affect system controller.
21-62-01-01
Cabin Temperature Indicator Without Cabin Occupants
C/1/0
PLACARDING PROCEDURE
Place an INOP placard on the digital temperature display.
56XCOMPEU-01-00
21-20
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-62-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Temperature Indicator 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.
OPERATIONAL PROCEDURE
Use a portable temperature indicating device to determine appropriate cabin operational
temperatures.
PLACARDING PROCEDURE
Place an INOP placard on the digital temperature display.
56XCOMPEU-01-00
21-21
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
21-62-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cockpit Temperature Indicator
C/1/0
PLACARDING PROCEDURE
Place an INOP placard on the digital temperature display.
56XCOMPEU-01-00
21-22
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
CABIN ALTITUDE vs. CABIN PRESSURE DIFFERENTIAL CONVERSION
(Cabin Pressure Differential Display or Cabin Altimeter Inoperative)
CABIN ALTITUDE x 1000'
CABIN
ALT
X
1000'
11.0
10.5
10.0
9.5
9.0
8.5
8.0
7.5
7.0
6.5
6.0
5.5
5.0
4.5
4.0
3.5
3.0
2.5
2.0
1.5
1.0
0.5
0.0
-0.5
-1.0
AEROPLANE PRESSURE ALTITUDE  1000'
0
5
0.0
0.0 0.3
0.3 0.6
0.5 0.8
10
15
20
25
0.0
0.2
0.4
0.6
0.8
1.0
1.2
1.5
1.7
1.9
2.1
2.4
2.6
2.8
3.1
3.3
3.6
3.8
4.1
4.3
4.6
4.9
5.1
1.4
1.6
1.8
2.0
2.2
2.4
2.6
2.8
3.0
3.3
3.5
3.7
3.9
4.2
4.4
4.6
4.9
5.1
5.4
5.6
5.9
6.1
6.4
6.7
6.9
3.0
3.2
3.4
3.6
3.8
4.0
4.2
4.4
4.6
4.8
5.0
5.2
5.5
5.7
5.9
6.2
6.4
6.7
6.9
7.2
7.4
7.7
7.9
8.2
8.5
4.3
4.5
4.7
4.9
5.1
5.3
5.5
5.7
5.9
6.1
6.3
6.5
6.8
7.0
7.2
7.5
7.7
8.0
8.2
8.5
8.7
9.0
9.2
9.5
9.8
28
31
33
35
37
39
41
43
45
47
49
51
4.9
5.1
5.3
5.5
5.7
5.9
6.1
6.4
6.6
6.8
7.0
7.2
7.5
7.7
7.9
8.2
8.4
8.6
8.9
9.1
9.4
9.7
9.9
10.2
10.5
5.6
5.8
6.0
6.2
6.4
6.6
6.8
7.1
7.3
7.5
7.7
7.9
8.2
8.4
8.6
8.9
9.1
9.3
9.6
9.8
10.1
5.9
6.1
6.3
6.5
6.7
6.9
7.1
7.3
7.5
7.8
8.0
8.2
8.4
8.7
8.9
9.1
9.4
9.6
9.9
10.1
6.3
6.4
6.6
6.8
7.0
7.2
7.5
7.7
7.9
8.1
8.3
8.5
8.8
9.0
9.2
9.5
9.7
10.0
10.2
6.6
6.8
7.0
7.2
7.4
7.6
7.8
8.0
8.2
8.4
8.6
8.9
9.1
9.3
9.5
9.8
10.0
6.9
7.1
7.3
7.5
7.7
7.9
8.1
8.3
8.5
8.7
8.9
9.1
9.4
9.6
9.8
10.1
7.1
7.3
7.5
7.7
7.9
8.1
8.3
8.5
8.7
9.0
9.2
9.4
9.6
9.9
10.1
7.4
7.5
7.7
7.9
8.1
8.3
8.6
8.8
9.0
9.2
9.4
9.6
9.9
10.1
7.6
7.8
8.0
8.2
8.4
8.6
8.8
9.0
9.2
9.4
9.6
9.9
10.1
7.8
8.0
8.2
8.4
8.6
8.8
9.0
9.2
9.4
9.6
9.8
10.1
8.0
8.1
8.3
8.5
8.7
8.9
9.2
9.4
9.6
9.8
10.0
8.1
8.3
8.5
8.7
8.9
9.1
9.3
9.5
9.7
10.0
*Data in this chart has been calculated using data found in the following document: U.S. STANDARD
ATMOSPHERE, 1976 (NASA-TM-X-74335). Published by the National Aeronautics and Space Administration.
EXAMPLE: Aeroplane is at FL 350 and Cabin Pressure Differential Gauge reads 8.8
PSID, Cabin Altitude is 5,000'.
EXAMPLE: Aeroplane Is At FL 350 and Cabin Altimeter reads 5,000', Cabin Pressure
Differential is 8.8 PSID.
56XCOMPEU-01-00
21-23
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
21-24
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
22-10-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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) Aeroplane is not operated RVSM.
MAINTENANCE PROCEDURE
Pull and secure the A/P SERVO circuit breaker.
OPERATIONAL PROCEDURE
1. Flight planning shall include consideration of enroute and approach operations
(including weather) without the autopilot.
2. Consider reduced range due to flight below RVSM airspace, if required.
PLACARDING PROCEDURE
Place a placard stating “AUTOPILOT INOP NO RVSM” on autopilot controller.
22-10-02
Yaw Damper
B/1/0
(M) (O) May be inoperative provided:
a) Yaw damper is deactivated,
b) Autopilot is considered inoperative, and
c) Aeroplane is not operated RVSM
MAINTENANCE PROCEDURE
Pull and secure the A/P SERVO circuit breaker.
OPERATIONAL PROCEDURE
1. Flight planning shall include consideration of enroute and approach operations
(including weather) without the autopilot.
2. Consider reduced range due to flight below RVSM airspace, if required.
PLACARDING PROCEDURE
Place a placard stating “YAW DAMP INOP NO RVSM” on autopilot controller.
56XCOMPEU-01-00
22-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
22-10-03-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Autopilot Disconnect Functions (Red, Yoke Mounted Quick Release
Controls)
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.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SIDE) QUICK DISCONNECT INOP” on the
instrument panel in view of the flight crew.
56XCOMPEU-01-00
22-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
22-10-03-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Autopilot Disconnect Functions (Red, Yoke Mounted Quick Release
Controls)
B/2/0
(M) (O) May be inoperative provided:
a) Autopilot is considered inoperative,
b) Electric trim is considered inoperative, and
c) Aeroplane is not operated RVSM.
MAINTENANCE PROCEDURE
1. Pull and secure the A/P SERVO circuit breaker.
2. Pull and secure the PITCH TRIM circuit breaker.
OPERATIONAL PROCEDURE
1. Flight planning shall include consideration of enroute and approach operations
(including weather) without the autopilot.
2. Consider reduced range due to flight below RVSM airspace, if required.
3. Pitch trim shall be actuated with the manual pitch trim wheel.
PLACARDING PROCEDURE
1. Place a placard stating “(AFFECTED SIDE) QUICK DISCONNECT INOP” on the
instrument panel in view of the flight crew.
2. Place a placard stating “ELECTRIC TRIM INOP” on the instrument panel in view
of the flight crew.
56XCOMPEU-01-00
22-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
22-10-04
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Go-Around Button
C/2/1
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SIDE) GO AROUND BUTTON INOP” on the
instrument panel in view of the flight crew.
56XCOMPEU-01-00
22-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
22-10-04
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Go-Around Button
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 go-around.
NOTE: FMS missed approach procedure must be activated via the FMS CDU.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SIDE) GO AROUND BUTTON INOP” on the
instrument panel in view of the flight crew.
56XCOMPEU-01-00
22-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
22-10-05
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Autopilot/Flight Director Touch Control Steering (TCS or AP SYNC)
C/2/0
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SIDE) TCS or AP SYNC BUTTON INOP” on the
instrument panel in view of the flight crew.
56XCOMPEU-01-00
22-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
VHF Communications System
C/-/1
May be inoperative provided:
a) COMM 1 is operative, and
b) Aeroplane is operated VFR over routes navigated by reference to visual
landmarks.
PLACARDING PROCEDURE
Place an INOP placard above/adjacent to the affected communications equipment.
23-00-02
Flight Phone System (If installed)
D/-/0
PLACARDING PROCEDURE
Place an INOP placard on the affected flight phone.
23-00-02-01
Flight Phone System Cockpit Handset (If installed)
D/-/0
PLACARDING PROCEDURE
Place an INOP placard on the affected handset.
23-00-02-02
Flight Phone System Cabin Handset (If installed)
D/-/0
PLACARDING PROCEDURE
Place an INOP placard on the affected handset.
56XCOMPEU-01-00
23-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-00-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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).
PLACARDING PROCEDURE
Place a placard stating “RADIO TUNING INOP” on radio tuning section of the affected
CCP.
23-00-04
SATCOM (If installed)
D/-/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place an INOP placard above/adjacent or on the affected SATCOM component.
56XCOMPEU-01-00
23-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-00-05
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
1. Prior to flight, flight crew shall discuss new radio tuning procedures using only the
operational RMU and Aux COM/NAV CDU.
2. Prior to each flight, a crew member shall check for proper reception and
transmission by use of the Auxiliary Com/Nav Control Display Unit to tune in at
least one Com channel and one Navigation aid.
PLACARDING PROCEDURE
Place an INOP placard on the affected RMU.
56XCOMPEU-01-00
23-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-00-06
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
PLACARDING PROCEDURE
Place a placard stating “CVR INOP” on the instrument panel in view of the flight crew.
23-10-01-01
High Frequency (HF) Communications System (If installed)
D/-/Any in excess of those required for the intended route, may be inoperative.
PLACARDING PROCEDURE
Place a placard stating “HF#_ INOP” adjacent to the affected system.
56XCOMPEU-01-00
23-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-10-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
High Frequency (HF) Communications System (If installed)
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.
OPERATIONAL PROCEDURE
1. Prior to each flight, a crew member shall make sure that SATCOM Data Link and
ACARS systems are operational for transmitting and receiving information from a
ground station.
2. Prior to each flight, a crew member shall review SATCOM system user’s
guide/manual to ensure coverage exists for the intended route of flight.
3. Prior to flight, a crew member shall coordinate with the appropriate ATC facility to
advise of intended flight without INMARSAT codes, if codes are not available.
PLACARDING PROCEDURE
Place a placard stating “HF#_ INOP” adjacent to the affected system.
56XCOMPEU-01-00
23-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-10-01-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
High Frequency (HF) Communications System (If installed)
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.
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.
OPERATIONAL PROCEDURE
1. Prior to each flight, a crew member shall make sure that SATCOM Data Link and
ACARS systems are operational for transmitting and receiving information from a
ground station.
2. Prior to each flight, a crew member shall review SATCOM system user’s
guide/manual to ensure coverage exists for the intended route of flight.
3. Prior to flight, a crew member shall coordinate with the appropriate ATC facility to
advise of intended flight without INMARSAT codes, if codes are not available.
PLACARDING PROCEDURE
Place a placard stating “HF#_ INOP” adjacent to the affected system.
56XCOMPEU-01-00
23-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-10-01-04
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
1. Inspect the horizontal and vertical stabilizers for structural damage.
2. Inspect elevator and rudder assemblies to make sure no portion of the antenna
damaged the flight controls.
3. If any damage is found, contact the Cessna Citation Customer Support
Structures group.
4. Pull and secure the appropriate HF Circuit breakers.
5. Cut the remaining antenna off making sure to secure all lose connections.
PLACARDING PROCEDURE
1. Place an INOP placard on the HF controller(s).
2. Place a placard stating “HF ANTENNA INOP” on the instrument panel in view of
the flight crew.
23-20-01-01
Selective Call (SELCAL) Systems (If installed)
D/-/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place an INOP placard on the affected SELCAL system.
23-20-01-02
Selective Call (SELCAL) Systems (If installed)
C/-/0
(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE
1. Flight crew shall advise ATC of inoperative SELCAL, as appropriate.
2. Flight crew shall monitor the appropriate radios at all times in the absence of
SELCAL. Consideration should be given to the effect of increased fatigue due to
this requirement and the possibility of having only one crew member monitor the
radios via headset (especially HF) if required for the given flight.
PLACARDING PROCEDURE
Place an INOP placard on the affected SELCAL system.
56XCOMPEU-01-00
23-7
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-20-02-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Individual SELCAL (VHF/UHF/HF) Channel (If installed)
D/-/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED CHANNEL) INOP” adjacent to the affected
SELCAL system.
23-20-02-02
Individual SELCAL (VHF/UHF/HF) Channel (If installed)
C/-/0
(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE
SELCAL frequencies must be manually tuned using the FREQ setting.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED CHANNEL) INOP” adjacent to the affected
SELCAL system.
23-20-03-01
Datalink (AFIS/ACARS/UNILINK) (If installed)
D/-/0
May be inoperative provided procedures do not require its use.
NOTE:
Subscription based service status does not constitute inoperative
equipment.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED FUNCTION) INOP” adjacent to the affected FMS
CDU.
56XCOMPEU-01-00
23-8
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-20-03-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Datalink (AFIS/ACARS/UNILINK) (If installed)
C/-/0
(O) May be inoperative provided alternate procedures are established and used.
NOTE:
Subscription based service status does not constitute inoperative
equipment.
OPERATIONAL PROCEDURE
1. Flight planning shall include briefing the loss of function for
AFIS/ACARS/UNILINK as applicable for the flight leg and the use of radio
communication to obtain the required flight information.
2. Crew shall use other available means to obtain weather information such as
HIWAS or FLIGHTWATCH as well as radar.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED FUNCTION) INOP” adjacent to the affected FMS
CDU.
23-40-01-01
Passenger Address (PA) System 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.
OPERATIONAL PROCEDURE
1. During Normal, Abnormal and/or Emergency situations or checklists requiring
use of PA system, a crew member shall face the passengers from the cockpit
and perform the appropriate announcements/instructions for the situation.
2. A crew member shall orally brief passengers on any items they would normally
use the PA system to brief.
PLACARDING PROCEDURE
Place an INOP placard adjacent to PA SELECT knob on both audio panels.
23-40-01-02
Passenger Address (PA) System Cargo Configuration
D/1/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place an INOP placard adjacent to PA SELECT knob on both audio panels.
56XCOMPEU-01-00
23-9
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-40-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Automatic Cabin Briefer (If installed)
D/1/0
(O) May be inoperative provided cabin occupants are briefed by alternate means.
OPERATIONAL PROCEDURE
A member of the flight crew shall use the PA system or direct conversation to brief the
passengers on those callouts the Automatic Cabin Briefer would normally be used for.
PLACARDING PROCEDURE
Place an INOP placard on the Automatic Cabin Briefer.
23-50-01
Cockpit Overhead Communications 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.
PLACARDING PROCEDURE
Place an INOP placard on the affected speaker.
23-50-02
Hand-Held Microphone
C/2/0
May be inoperative provided associated headset/boom microphone is operative.
PLACARDING PROCEDURE
Place an INOP placard on the affected hand-held microphone.
23-50-03
Headset with Boom Microphones
D/-/Any in excess of one headset (including boom microphone) for each required crew
member on flight deck duty may be missing or inoperative.
PLACARDING PROCEDURE
Place an INOP placard adjacent to/on the affected unit.
56XCOMPEU-01-00
23-10
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
23-60-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Static Wick Left Wing
C/6/5
Wingtip static wick must be operative.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected static wick location.
23-60-01-02
Static Wick Right Wing
C/6/5
Wingtip static wick must be operative.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected static wick location.
23-60-01-03
Static Wick Empennage Stinger
C/1/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected static wick location.
23-60-01-04
Static Wick Airborne Flight Information system (AFIS) (If installed)
C/1/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected static wick location.
56XCOMPEU-01-00
23-11
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
23-12
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
24-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Ground Power Dispatch Switch (If installed)
C/1/0
PLACARDING PROCEDURE
Place an INOP placard above/adjacent to the affected switch.
24-21-01
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.
OPERATIONAL PROCEDURE
Once the event has occurred either on the ground or in the air, all Aeroplane operations
in which the engines are operating shall be recorded to make sure the AFM limitation is
not exceeded.
PLACARDING PROCEDURE
Place a placard stating “AC BEARING (AFFECTED SIDE(S) ON. MONITOR
OPERATING TIME” on the instrument panel in view of flight/maintenance crew.
56XCOMPEU-01-00
24-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
24-31-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Battery Temperature Indicator (If installed)
C/1/0
PLACARDING PROCEDURE
NOTE:
Aeroplane that have been converted from Ni-Cad to lead acid batteries
will continue to have an operational battery temperature indicator that
will read a false indication. This is a normal condition and is the result of
a dummy temperature sensor being installed on the lead acid battery
case.
Place an INOP placard on the battery temperature indicator.
56XCOMPEU-01-00
24-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
24-35-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
1. Flight planning shall include 110 pph fuel burn for APU in fuel calculations to
make sure adequate fuel for intended route of flight.
2. Flight planning shall also include consideration for the increased fuel burn at
lower altitudes and the effect on range.
3. After starting APU, verify generator is producing proper output.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SIDE) GENERATOR INOP” on the instrument
panel in view of flight crew.
24-35-02
Auxiliary Power Unit (APU) Generating System (If installed)
C/1/0
May be inoperative provided APU generator switch remains off.
PLACARDING PROCEDURE
Place an INOP placard over the ON position of the APU GENERATOR switch.
24-40-01
External Power Receptacle
C/1/0
PLACARDING PROCEDURE
1. Place an INOP placard over the external power receptacle inside the access
door.
2. Place a placard stating “EXTERNAL POWER INOP” on the instrument panel in
view of the flight/maintenance crew.
56XCOMPEU-01-00
24-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
24-50-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
AC Cockpit Outlet (If installed)
C/-/0
(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE
1. If equipment that utilizes the affected power source is battery operated, make
sure that adequate battery life is available for installed battery and backup battery
(ies) for intended operating times.
2. Use alternate cockpit/cabin power source if power source is available and within
close proximity.
PLACARDING PROCEDURE
Place an INOP placard over the affected power source.
24-50-01-02
AC Cockpit Outlet (If installed)
D/-/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place an INOP placard over the affected power source.
56XCOMPEU-01-00
24-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
1. Place required documents in clear plastic bag.
2. Display documents in a manner that is visible to the crew, passengers and/or the
appropriate aviation authority.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected holder if broken, or
2. Place a placard stating “DOCUMENTS HOLDER MISSING” at the affected
location.
25-00-02
Security System (Securaplane) (If installed)
D/1/0
PLACARDING PROCEDURE
Place an INOP placard on the affected system controlling panel/head.
25-10-01-01
Flight Crew Seat (per seat) Armrests Remain in Aeroplane
C/-/0
May be inoperative provided
a) Seat position is acceptable for crew, and
b) Armrest is stowed in retracted position.
PLACARDING PROCEDURE
Place an INOP placard on the affected armrest(s) location of the affected seat.
56XCOMPEU-01-00
25-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-10-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flight Crew Seat (per seat) Armrests Removed from Aeroplane
C/-/0
(M) May be inoperative provided seat position is acceptable to the flight crew member.
NOTE: If an inoperative armrest will hinder an emergency evacuation or any other
flight duties is should be removed.
MAINTENANCE PROCEDURE
NOTE: Refer to the appropriate Cessna Maintenance Manual and/or Interiors
Manual for information of the individual Aeroplane installation.
Using the appropriate seat manual, remove and store the affected armrest(s).
PLACARDING PROCEDURE
Place an INOP placard on the affected armrest(s) location of the affected seat.
25-10-01-02
Flight Crew Seat (per seat) Lumbar Support (If installed)
C/1/0
PLACARDING PROCEDURE
Place an INOP placard above/adjacent to the lumbar adjustment.
25-10-01-03
Flight Crew Seat (per seat) 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.
MAINTENANCE PROCEDURE
Refer to the appropriate Cessna Maintenance Manual and/or Interiors Manual for
information of the individual Aeroplane installation.
Using the appropriate seat manual, secure the affected seat feature in a position
acceptable to the affected flightcrew member.
PLACARDING PROCEDURE
Place a placard stating “SEAT (AFFECTED FUNCTION) INOP” on the instrument panel
in front of the affected crew seat(s).
56XCOMPEU-01-00
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-10-01-04
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flight Crew Seat (per seat) Restraint Buckle Protective Padding (If
installed)
C/-/0
May be missing or inoperative.
PLACARDING PROCEDURE
Place a placard stating “RESTRAINT PADDING INOP/MISSING” on the instrument
panel in front of the affected crew seat(s).
25-10-01-05
Flight Crew Seat (per seat) Thigh Support
C/1/0
May be inoperative provided full flight control movement is available.
PLACARDING PROCEDURE
Place a placard stating “THIGH SUPPORT INOP” on the instrument panel in front of the
affected crew seat(s).
56XCOMPEU-01-00
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-10-01-06
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flight Crew Seat (per seat) Vertical Adjustment
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.
MAINTENANCE PROCEDURE
Refer to the appropriate Cessna Maintenance Manual and/or Interiors Manual for
information of the individual Aeroplane installation.
Using the appropriate seat manual, secure the affected seat feature in a position
acceptable to the affected flightcrew member.
PLACARDING PROCEDURE
Place a placard stating “SEAT VERT ADJUST INOP” on the instrument panel in front of
the affected crew seat(s).
56XCOMPEU-01-00
25-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-10-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
Figure 1 (View from Pilot’s seat)
Figure 2 (View from Pilot’s seat)
Continued Next Page
56XCOMPEU-01-00
25-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Continued
1. Prior to flight, a crew member shall occupy the affected seat and fasten the
restraining system to ensure the following conditions are met:
a. Make sure full flight control movement and brake application.
b. Make sure access to all necessary controls and equipment.
2. Position the affected seat(s) so the pilot aligns the eyeball locator bracket so that
the correct sight picture with the bracket is achieved (Figures 1 and 2):
a. Eyeball locator base is flat.
b. The flange opposite to the affected seat is aligned for a straight edge.
PLACARDING PROCEDURE
Place an INOP placard above eyeball locator.
25-10-03
Yoke Mounted Chart Holder (If installed)
C/2/0
PLACARDING PROCEDURE
Place an INOP placard on the affected chart holder.
25-10-04
Yoke Mounted Chart Holder Light (If installed)
C/2/0
PLACARDING PROCEDURE
Place a placard stating “LIGHT INOP” on the affected chart holder.
25-10-05-01
Cockpit Flashlight Holder Assembly (If installed) 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.
PLACARDING PROCEDURE
Place an INOP placard on the affected light holder.
56XCOMPEU-01-00
25-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-10-05-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cockpit Flashlight Holder Assembly (If installed) Holder Assembly
C/2/0
May be inoperative provided associated flashlight is stowed by alternate means.
PLACARDING PROCEDURE
Place an INOP placard on the affected light holder.
25-10-06
Cockpit Sunvisor System and/or Attach Mechanism
D/-/0
May be missing or inoperative provided pilot’s field of vision is not obstructed.
PLACARDING PROCEDURE
1. Make sure that the affected component does not interfere with Aeroplane
operation. If the failed component is the visor monorail, remove and stow the
monorail and sunvisor(s).
2. Place a placard stating “(AFFECTED COMPONENT) INOP” on the plastic
cockpit trim within close proximity of the component.
25-10-07
Cockpit Assist Handle
D/-/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected location.
56XCOMPEU-01-00
25-7
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-20-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Passenger Seat (Including Side Facing Seats)
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).
PLACARDING PROCEDURE
NOTE: Refer to the appropriate Cessna Maintenance Manual and/or Interiors
Manual for information of the individual Aeroplane installation.
Place a placard stating “DO NOT OCCUPY” on the affected seat. One method is to use
tape and run it across the seat from the seat bottom cushion to the seat back diagonally.
25-20-01-01-10
Passenger Seat (Including Side Facing Seats) Armrest 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.
MAINTENANCE PROCEDURE
NOTE: Refer to the appropriate Cessna Maintenance Manual and/or Interiors
Manual for information of the individual Aeroplane installation.
Using the appropriate seat manual, remove and store the affected armrest(s).
PLACARDING PROCEDURE
If armrest is inoperative, place an INOP placard on the affected armrest(s). If armrest is
missing, place a placard stating “ARMREST INOP” at the affected location.
56XCOMPEU-01-00
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-20-01-20
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Passenger Seat (Including Side Facing Seats) Armrest 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.
PLACARDING PROCEDURE
If armrest is inoperative, place an INOP placard on the affected armrest(s). If armrest is
missing, place a placard stating “ARMREST INOP” at the affected location.
25-20-01-02
Passenger Seat (Including Side Facing Seats) Headrest
C/-/May be inoperative and seat occupied provided headrest is failed in placarded taxi,
takeoff and landing position.
PLACARDING PROCEDURE
Place a placard stating “HEADREST INOP DO NOT MOVE” on the top of the headrest
so that a person occupying the affected seat cannot rub the placard off.
25-20-01-02
Passenger Seat (Including Side Facing Seats)Headrest
C/-/May be missing or inoperative in other than placarded taxi, takeoff, and landing position
provided affected seat is considered inoperative.
NOTE: Any damage to passenger seats and components must not be detrimental
to passenger safety.
PLACARDING PROCEDURE
Place a placard stating “DO NOT OCCUPY” on the top of the headrest so that a person
occupying the affected seat cannot rub the placard off.
56XCOMPEU-01-00
25-9
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-20-01-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Passenger Seat (Including Side Facing Seats)Recline Mechanism
C/-/May be inoperative and seat occupied provided seat back is immovable in the upright
position.
PLACARDING PROCEDURE
Place an INOP placard on the recline mechanism lever.
25-20-01-03
Passenger Seat (Including Side Facing Seats) Recline Mechanism
D/-/(M) May be inoperative and seat occupied provided seat back is secured in full upright
position.
MAINTENANCE PROCEDURE
NOTE: Refer to the appropriate Cessna Maintenance Manual and/or Interiors
Manual for information of the individual Aeroplane installation.
1. Place affected seat in the full upright position.
2. Using the appropriate passenger seat manual, disable the recline mechanism.
PLACARDING PROCEDURE
Place an INOP placard on the recline mechanism lever.
56XCOMPEU-01-00
25-10
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-20-01-04
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Passenger Seat (Including Side Facing Seats) 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 Aeroplane
aisle,
c) Seat is positioned so it will not affect emergency egress.
PLACARDING PROCEDURE
NOTE: The seat base tracking mechanism is located at the very bottom section of
the seat. This is not the mechanism built into the side of the seat or armrest.
1. Make sure the affected seat is immovable.
2. Place a placard stating “SEAT TRACKING INOP DO NOT MOVE LEVER”
adjacent to the seat tracking mechanism.
56XCOMPEU-01-00
25-11
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-20-01-05
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Passenger Seat (Including Side Facing Seats)Seat Tracking and
Swivel Mechanism
C/-/May be inoperative and seat occupied provided seat is failed immovable in placarded
taxi, takeoff and landing position.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED FUNCTION) INOP” above/adjacent to the affected
seat(s) mechanism.
25-20-02-01
Refreshment Center Hot Liquid Storage System Heater
C/1/0
(M) May be inoperative provided system is deactivated.
MAINTENANCE PROCEDURE
1. Using the appropriate interior manual for the Aeroplane configuration, access the
refreshment center circuit breakers.
2. Pull and secure the affected circuit protection for the appropriate refreshment
center configuration.
PLACARDING PROCEDURE
Place a placard stating, “(AFFECTED SYSTEM) HEATER INOP” next to the affected
equipment.
25-40-01
Ashtray
A/-/1
Any in excess of one may be inoperative for three flight days.
PLACARDING PROCEDURE
Place an INOP placard adjacent/on the affected ashtray locations.
25-60-01
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.
PLACARDING PROCEDURE
Place an INOP placard on the affected equipment.
56XCOMPEU-01-00
25-12
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-60-02-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Emergency Medical Equipment Automatic External Defibrillator
(AED) and/or Associated Equipment
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.
OPERATIONAL PROCEDURE
NOTE:
Do not repack any equipment that has been used and may be
contaminated or may be a bio-hazard threat. Dispose of any bio-hazard
materials using approved disposal procedures/techniques.
1. Repack unit in original container. If provided, follow manufacturer’s instructions.
2. Secure a placard on the unit stating its condition and any missing contents.
3. A crew member shall brief all occupants on the operating condition of the
affected unit and available items.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected equipment.
2. If kit is available and operative but incomplete, place a placard stating
“(AFFECTED ITEMS) ARE NOT CONTAINED IN THIS KIT” on the kit’s lid.
3. If AED is missing, place a placard stating “AED MISSING” at the location.
25-60-02-02
Emergency Medical Equipment Emergency Medical Kit (EMK) and/or
Associated Equipment
OPERATIONAL PROCEDURE
NOTE: Do not repack any equipment that has been used and may be contaminated
or may be a bio-hazard threat. Dispose of any bio-hazard materials using
approved disposal procedures/techniques.
1. Repack unit in original container. If provided, follow manufacturer’s instructions.
2. Secure a placard on the unit stating its condition and any missing contents.
3. A crew member shall brief all occupants on the operating condition of the
affected unit and available items.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected equipment.
2. If kit is available and operative but incomplete, place a placard stating
“(AFFECTED ITEMS) ARE NOT CONTAINED IN THIS KIT” on the kit’s lid.
3. If EMK is missing, place a placard stating “EMERGENCY MEDICAL KIT
MISSING” at the location.
56XCOMPEU-01-00
25-13
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-60-02-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Emergency Medical Equipment First Aid Kit (FAK) and/or Associated
Equipment
D/-/1
Any in excess of those required may be incomplete or missing.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected equipment.
2. If kit is available and operative but incomplete, place a placard stating
“(AFFECTED ITEMS) ARE NOT CONTAINED IN THIS KIT” on the kit’s lid.
3. If FAK is missing, place a placard stating “FIRST AID KIT MISSING” at the
location.
25-61-01
Life Jackets (Crew and Passenger) (If installed)
D/-/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.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected equipment if left in the Aeroplane.
2. If equipment is to be removed from the Aeroplane, place a placard stating
“LIFEJACKET INOP/MISSING” on the access door/panel/stowage location.
25-62-01-01
Emergency Locator Transmitter (ELT) 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.
MAINTENANCE PROCEDURE
1. Access the affected ELT and remove it from the Aeroplane. Stow and tag the
ELT so that it cannot be mistaken for an operative piece of equipment.
2. If operating rules require that an operative survival type ELT be carried onboard
the Aeroplane, replace the affected ELT with an operative one prior to dispatch.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected ELT.
2. If ELT is missing, Place a placard stating “ELT MISSING” at the affected location
56XCOMPEU-01-00
25-14
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-62-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Emergency Locator Transmitter (ELT) Fixed ELTs (If installed)
D/-/(M) Any in excess of those required by operating requirements may be missing or
inoperative provided system is deactivated.
MAINTENANCE PROCEDURE
1. Remove electrical power from the airplane.
2. Gain access to the ELT by removing access panel 340AR.
3. Identify and disconnect antenna coax connector and electrical connector from
ELT.
4. Cap, bag and stow the loose ELT connector.
5. Reinstall access panel 340AR.
PLACARDING PROCEDURE
Place an INOP placard on the ELT control panel.
25-62-01-02
Emergency Locator Transmitter (ELT) Fixed ELTs (If installed)
A/-/0
May be inoperative provided repairs are made within 6 further flights or 25 flying hours,
whichever occurs first.
PLACARDING PROCEDURE
Place an INOP placard on the affected ELT.
56XCOMPEU-01-00
25-15
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
25-64-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Life Raft (If installed)
C/-/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.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected equipment if unit is in excess of operating
requirements and is left in the Aeroplane for transport to a servicing facility.
2. If equipment is to be removed from the Aeroplane, place a placard stating “LIFE
RAFT MISSING” on the access door/panel/stowage location.
56XCOMPEU-01-00
25-16
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
26-10-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
APU Fire Detection System (If installed)
C/1/0
May be inoperative provided APU is considered inoperative
PLACARDING PROCEDURE
NOTE: Although this relief does not have an associated (M) procedure, Cessna
recommends that a maintenance technician or appropriately trained
member of the flight crew pull and secure the APU master circuit breaker.
Place an INOP placard on the APU FIRE annunciator.
26-11-01
Baggage Smoke Detector (If installed)
C/-/Any in excess of those required by regulations may be inoperative.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected smoke detector.
2. Place a placard stating “BAGG SMOKE DETECT INOP” on the instrument panel
in view of the flight crew.
26-12-01
Lavatory Smoke Detector (If installed)
C/-/Any in excess of those required by regulations may be inoperative.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected smoke detector.
2. Place a placard stating “LAV SMOKE DETECT INOP” on the instrument panel in
view of the flight crew.
26-22-01
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.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected equipment if unit is in excess of operating
requirements and is left in the Aeroplane for transport to a servicing facility.
2. If equipment is to be removed from the Aeroplane, place a placard stating “FIRE
EXTINGUISHER INOP/MISSING” on the access door/panel/stowage location
and store the affected equipment out of sight.
56XCOMPEU-01-00
26-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
26-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
27-20-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
1. Make sure nose wheel is positioned for forward travel.
2. Adjust rudder pedals for equal travel and positioning.
3. Secure upper half of rudder pedal adjustment mechanism into place preventing
unintended movement.
4. Make sure full rudder pedal and brake travel is available on both sides.
OPERATIONAL PROCEDURE
1. Prior to flight, a crew member shall occupy the affected seat and fasten the
restraining system to make sure the following conditions are met:
a. Full unobstructed flight control movement and brake application.
b. Access to all necessary controls and equipment.
PLACARDING PROCEDURE
Place a placard stating “RUDDER PEDAL ADJUSTMENT MECHANISM INOP DO NOT
ADJUST RUDDER PEDALS” on the instrument panel in front of affected pilot.
56XCOMPEU-01-00
27-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
27-31-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
NOTE 1:
Autopilot shall be considered inoperative.
NOTE 2:
If electric trim is inoperative, it should be confirmed that the issue is
not in the manual (mechanical) trim system in the airplane and that the
failure is not affecting the manual trim. The manual trim should be run
throughout its travel limits to check for binding and proper operation.
1. Pull and secure PITCH TRIM and AUTOPILOT circuit breakers.
2. Determine if any mechanical damage exists, causing interference with controls
precluding dispatch.
3. Check manual trim throughout range of travel for smooth operation.
OPERATIONAL PROCEDURE
1. Consider reduced range due to flight below RVSM airspace, if required.
2. Flight planning shall include consideration of enroute and approach operations
(including weather) without the autopilot.
3. Crew coordination and briefings shall include operational considerations due to
inoperative electric trim and autopilot.
PLACARDING PROCEDURE
Place a placard stating “ELECTRIC TRIM INOP – AUTOPILOT DISABLED. NO RVSM”
on instrument panel in view of the flight crew.
27-31-02
Elevator Trim Position Indicator Tip
C/1/0
(M) May be missing provided an alternate means of marking Indicator Tip is established
and used.
MAINTENANCE PROCEDURE
Using tape or white RTV, mark the indicator tip for visibility.
PLACARDING PROCEDURE
Place an INOP placard above the control handle.
56XCOMPEU-01-00
27-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
27-42-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
1. To position the stabilizer in the negative (-) 2 degree position:
a. Make sure LANDING GEAR handle is in the DOWN position and flaps
are selected to 7 degrees or greater.
b. With electrical power applied (battery or GPU), select BATT switch ON.
c. Rotate Rotary Test knob to ANNUN and verify STAB MIS COMP
annunciator illuminates. Rotate Rotary Test knob to OFF and verify STAB
MIS COMP annunciator is extinguished.
d. To verify horizontal stabilizer is in the negative (-) 2 degree position,
visually inspect inboard leading edge of horizontal stabilizer and ensure
the stab position indicator is aligned with lower indicator on vertical
stabilizer. If correct position is confirmed, go to step 2. If horizontal
stabilizer is NOT in the negative (-) 2 degree position:
i. Select BATT to OFF and remove electrical power from Aeroplane.
ii. Access horizontal stabilizer by removing RH forward and lower
wiper panels and RH lower side panel on vertical stabilizer.
iii. Access manual drive gear in actuator by opening diamond shaped
access cover located on forward side of actuator gear box cover
adjacent to hydraulic motor fluid line connection.
iv. Station a second technician in cockpit, connect power to
Aeroplane, and place BATT switch to ON.
v. Using a ¼ inch hex drive torque wrench set to less than 125 inch
pounds to prevent damage to stab actuator, rotate the manual
drive gear clockwise until STAB MIS COMP annunciator
extinguishes. Horizontal stabilizer position indicator on leading
edge should align with lower position indicator on vertical
stabilizer.
vi. Place the BATT switch to OFF and remove power from Aeroplane.
vii. Reinstall all access covers and wiper panels.
2. Pull and secure STAB CONTROL circuit breaker.
Continued Next Page
56XCOMPEU-01-00
27-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
OPERATIONAL PROCEDURE
Continued
OPERATIONAL PROCEDURE
Prior to each takeoff a member of the crew shall visually verify that the horizontal
stabilizer is in the correct position (-2 degree) for flight. (Make sure the stab position
indicator is aligned with the bottom limit of the indicating band on the vertical stab)
PLACARDING PROCEDURE
Place a placard stating “HORIZONTAL STABILIZER IS LOCKED IN THE NEGATIVE (-)
2 DEGREE (TAKEOFF) POSITION. MAXIMUM AIRSPEED: 200 KIAS/.62M MAXIMUM
ALTITUDE FL410” on instrument panel in front of both pilots.
27-51-01
Flap Position Indicator Tip
C/1/0
(M) May be missing provided an alternate means of marking Indicator Tip is established
and used.
MAINTENANCE PROCEDURE
Using tape or white RTV, mark the indicator tip for visibility.
PLACARDING PROCEDURE
Place an INOP placard above the control handle.
56XCOMPEU-01-00
27-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
27-60-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
Pull and secure SPEEDBRAKE circuit breaker.
OPERATIONAL PROCEDURE
1. Prior to each takeoff a crew member shall visually inspect upper and lower
speedbrake panels for security.
2. Flight crew shall brief that spoilers are not available for use during EMER
DESCENT. The limit of FL410 is in place as a result of the increased time to
descend.
PLACARDING PROCEDURE
1. Place an INOP placard on the speedbrake switch cover.
2. Place a placard stating “SPEEDBRAKES INOP NO FLIGHT ABOVE FL410” on
instrument panel in front of both pilots.
27-70-01
Control Lock System
C/1/0
(O) May be inoperative in the unlocked position provided full flight control and throttle
movement is available.
OPERATIONAL PROCEDURE
Prior to each flight the crew shall visibly verify full range of motion for all associated flight
controls and throttle levers.
PLACARDING PROCEDURE
Place an INOP placard above the control lock handle.
56XCOMPEU-01-00
27-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
28-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Single Point Refueling System
C/1/0
PLACARDING PROCEDURE
Place an INOP placard of the SPR refueling receptacle.
28-10-01
Over Wing Refueling Cap Lock (If installed)
D/-/0
PLACARDING PROCEDURE
1. If lock is failed in the locked position, place a placard stating “FUEL CAP LOCK
INOP REFUEL WITH SPR ONLY” adjacent to the affected lock.
2. If lock is failed in the unlocked position, place a placard stating “FUEL CAP
LOCK INOP” adjacent to the affected lock. A crew member shall visibly verify the
affected fuel cap is secure after fueling and prior to flight.
28-40-01
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.
OPERATIONAL PROCEDURE
1. Flight crew shall brief the loss of low fuel quantity warning system on the affected
side.
2. Flight crew shall monitor fuel balance during flight to make sure adequate fuel
remains in both wing fuel tanks for planned mission.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SIDE) FUEL LOW LEVEL INOP” on the instrument
panel in view of the flight crew.
28-43-01
Fuel Temperature Indication
PLACARDING PROCEDURE
Place a placard stating “FUEL TEMP INOP” on the instrument panel in view of the
flight crew.
56XCOMPEU-01-00
28-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
28-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
30-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Drain Mast Heater
C/-/0
(M) May be inoperative provided:
a) Refreshment center drains and lavatory basins are not used, and
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, if relief tube installed.
MAINTENANCE PROCEDURE:
1. Pull and secure the appropriate circuit breaker in the interior j-box.
2. Cover basin, sink, galley, etc.
3. Make sure all ice and liquid is removed from galley storage and drains are clear.
PLACARDING PROCEDURE:
Place a placard stating, “DRAIN HEAT INOP, DO NOT USE” on the instrument panel in
view of the flight crew.
30-00-02
Rosemount Ram Air Temperature (RAT) Probe Heater (Units 50016000)
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.
PLACARDING PROCEDURE
Place a placard stating “RAT HTR INOP” on instrument panel in view of the flight crew.
56XCOMPEU-01-00
30-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
30-10-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE:
CAUTION:
Operating the system on the ground on an extremely hot day with
engines at a setting of 70% N2 or greater may cause an over
temperature indication even without system failure.
1. Remove the over-wing fairing panel on the affected side to access the V-band
clamp on the up-stream side of the associated anti-ice bleed air pressure
regulating shutoff valve.
2. Remove the V-band clamp upstream of the valve and install a blanking plate with
the following specifications:
a. 301 stainless steel half hard.
b. 2.000”, +0.020/-0.000 in diameter.
c. .020” thick.
3. Re-install clamp and torque to appropriate values.
4. Position the Aeroplane in a suitable run-up area and chock both main landing
gear.
5. Station an additional technician outside of Aeroplane. Make sure appropriate
personal safety equipment is used and all personnel are briefed on hazards of
working with operating engines.
6. Using AFM Normal Procedures, start both engines. Ensure AFM Ground
Operation Limitations are observed.
7. Turn WING/ENGINE anti-ice ON. Have technician verify no heated airflow from
blanking plates.
8. Turn WING XFLOW to ON and have technician verify no heated airflow from
both wing bleed air exhaust vents.
9. Using AFM Normal Procedures, power down Aeroplane.
10. Re-install both lower fuselage-wing panels.
11. The associated circuit breakers must remain engaged for engine anti-icing
capabilities.
PLACARDING PROCEDURE:
Place a placard stating, “WING A/I INOP” above the WING/ENGINE anti ice switches.
56XCOMPEU-01-00
30-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
30-10-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
PLACARDING PROCEDURE
Place an INOP placard above the TAIL de-ice switch.
56XCOMPEU-01-00
30-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
30-20-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Engine Anti-Ice System 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.
MAINTENANCE PROCEDURE:
NOTE:
Since the engine inlet under temperature switch is set at 60ºF (15.56ºC),
testing on days where the ambient temperature approaches this set
point may lead to the annunciator not illuminating. Annunciator will only
illuminate under normal conditions in ambient temperature settings less
than 60ºF (15.56ºC).
CAUTION:
The wing engine anti-ice switches operate both the left and right
wing leading edge and engine air inlet systems. Do not operate the
system longer than 5 minutes followed by a 30 minute cooling off
period.
WARNING:
Use extreme care when touching heated surfaces. Severe burns to
hands could result.
1. Position Aeroplane in a suitable run-up area and chock both main landing gear.
2. Station an additional technician outside of Aeroplane. Make sure appropriate
personal safety equipment is used and all personnel are briefed on hazards of
working with operating engines.
3. Using AFM Normal Procedures, start both engines.
4. Ensure LH and RH ENGINE ANTI ICE circuit breakers are engaged.
5. Select the appropriate L or R ENGINE anti-ice switch to the ENGINE ON position
and verify the affected side indication(s) illuminates/display.
6. Slowly increase the affected side throttle to 70%N2 and verify the affected side
annunciator/CAS message extinguishes within one minute.
7. Switch the affected side ENGINE anti-ice switch to the OFF position and reduce
throttle to idle.
8. Repeat steps 4 thru 6 for the unaffected side.
9. Cautiously verify the temperature of the both engine inlets. The engine inlet
should be a minimum of outside air +50ºF (10ºC), verified by lightly touching the
surfaces. Another method is to verify heated airflow from the exhaust vent on the
side of the engine nacelle.
10. Using AFM Normal Procedures, power down Aeroplane
OPERATIONAL PROCEDURE:
1. Flight crew must make sure that ambient temperatures at takeoff/landing do not
exceed +10 degrees C.
2. Takeoff and landing performance calculations must be computed for anti-ice ON.
PLACARDING PROCEDURE:
Place a placard stating, “ENGINE INOP” below the ENGINE anti-ice switches.
56XCOMPEU-01-00
30-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
30-20-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Engine Anti-Ice System 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.
MAINTENANCE PROCEDURE:
CAUTION:
CAUTION:
Operating the system on the ground on an extremely hot day with
engines at a setting of 70% N2 or greater may cause an over
temperature indication even without system failure.
WARNING:
Use extreme care when touching heated surfaces. Severe burns to
hands could result.
1. Remove the over-wing fairing panels to access the V-band clamp on the upstream side of the associated anti-ice bleed air pressure regulating shutoff valve.
2. Remove the V-band clamp upstream of the valve and install a blanking plate with
the following specifications:
3. 301 stainless steel half hard.
4. 2.000”, +0.020/-0.000 in diameter.
5. .020” thick.
6. Re-install clamp and torque to appropriate values.
7. Position the Aeroplane in a suitable run-up area and chock both main landing
gear.
8. Station an additional technician outside of Aeroplane. Make sure appropriate
personal safety equipment is used and all personnel are briefed on hazards of
working with operating engines.
9. Using AFM Normal Procedures, start both engines. Ensure AFM Ground
Operation Limitations are observed.
10. Turn WING/ENGINE anti-ice ON. Have technician verify no heated airflow from
blanking plates.
11. Using AFM Normal Procedures, power down Aeroplane
12. Re-install both over-wing panels.
13. The associated circuit breakers must remain engaged for engine anti-icing
capabilities.
PLACARDING PROCEDURE:
Place an INOP placard below the ENGINE anti-ice switches.
56XCOMPEU-01-00
30-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
30-30-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Pilot and Copilot Pitot Heater (Standby Excluded)
B/2/1
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.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SYSTEM) PITOT HTR INOP” above the ANTI
ICE/DEICE panel.
30-30-02
Pilot and Copilot Pitot Static Port Heater (Standby Excluded)
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.
PROCEDURE
Place a placard stating “(AFFECTED SYSTEM) STATIC HEAT INOP” above the PITOT
& STATIC switch.
30-40-01
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.
PLACARDING PROCEDURE:
Place an INOP placard above the WINDSHIELD AIR switch.
56XCOMPEU-01-00
30-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
30-40-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SIDE) W/S A/I INOP” above the WINDSHIELD
anti-ice switches.
30-40-03
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.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SIDE) WINDSCREEN SURFACE SEAL INOP” on
the instrument panel in view of the flight crew.
56XCOMPEU-01-00
30-7
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
30-8
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
Disconnect, cap and stow all connectors from the affected equipment.
OPERATIONAL PROCEDURE
Operators will develop an alternate method of recording any required data.
PLACARDING PROCEDURE
Place a placard stating “QAR INOP” on the instrument panel in view of the flight crew.
31-10-01
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.
OPERATIONAL PROCEDURE:
During the Before Taxi checklist the flight crew must verify the AP ON indication is
displayed on both PFDs when the autopilot is engaged.
PLACARDING PROCEDURE:
Place a placard stating “AP BUTTON LIGHT INOP” on the instrument panel in view of
the flight crew.
56XCOMPEU-01-00
31-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-10-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Autopilot Mode Controller YD button Engage Light (units 5001-6000)
B/1/0
(O) May be inoperative provided flight crew verifies yaw damper is disconnected prior to
every flight.
OPERATIONAL PROCEDURE:
1. Flight crew must verify the yaw damper is disconnected prior to every landing.
2. Prior to landing press the AP/Trim disconnect button.
PLACARDING PROCEDURE:
Place a placard stating “YD BUTTON LIGHT INOP” on the instrument panel in view of
the flight crew.
31-20-01
Auxiliary Power Unit (APU) Hour Meter (If installed)
C/1/0
(O) May be inoperative provided APU operation time is tracked by alternate means.
OPERATIONAL PROCEDURE:
1. Flight crew must insert a sheet into Aerocraft Log showing Hobbs time at failure.
2. Record each APU START and STOP time (including time zone, if not recording
Zulu time).
3. Following each APU cycle, add APU time to total APU operations time to assure
compliance with maintenance and/or operations requirements.
PLACARDING PROCEDURE:
Place an INOP placard on APU hour meter.
56XCOMPEU-01-00
31-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-20-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
PLACARDING PROCEDURE
Place an INOP placard on the affected clock.
31-20-03
MAX-VIZ EVS-1000 Enhanced Vision System (EVS) (If installed)
C/1/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE:
Place a placard stating, “EVS SYSTEM INOP” on the instrument panel in view of the
flight crew.
31-20-04
Flight Hour Meter
C/1/0
(O) May be inoperative provided flight time is tracked by alternate means.
OPERATIONAL PROCEDURE:
The flight crew must use alternate time keeping methods for accurate timing
requirements.
PLACARDING PROCEDURE:
Place an INOP placard on the affected flight hour meter.
56XCOMPEU-01-00
31-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-20-05
CESSNA AIRCRAFT COMPANY
MODEL 560XL
N1 Reminder (Mechanical or Electric) (Units 5001-6000)
D/1/0
PLACARDING PROCEDURE:
Place an INOP placard on the affected N1 reminder. If desired, the flight crew can place
a placard on the instrument panel with the N1 power setting.
31-20-06
Throttle Detent Indicating Light/Indication (Units 5001-6000) (If
installed)
D/6/0
PLACARDING PROCEDURE:
NOTE:
This relief does not include the indication on the AMLCD display.
Place an INOP placard adjacent to the affected throttle detent indication (TO, CLB,
CRU).
56XCOMPEU-01-00
31-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-30-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flight Data Recorder (FDR) System (If installed)
A/-/0
One or more may be inoperative provided:
a) The aerocraft 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.
NOTE 1: 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 aircraft 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 aerocraft operator in
accordance with approved maintenance procedures.
PLACARDING PROCEDURE
Place a placard stating, “FDR INOP” on the instrument panel in view of the flight crew.
56XCOMPEU-01-00
31-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
AIR DUCT O’HEAT, CKPT or CAB Annunciator (Units 5001-6000)
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) Aerocraft is operated at 14,000 feet MSL or below.
OPERATIONAL PROCEDURE:
1. Flight planning must consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning must consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s must be taken into account for planned route.
4. Select PRESS SOURCE OFF.
5. Select Cabin EMER DUMP ON.
6. Set Cabin Altitude to 14,000 feet.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED ANNUNCIATOR) INOP” on the instrument panel
in view of the flight crew.
56XCOMPEU-01-00
31-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
APU Oil Service Light (If installed)
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.
MAINTENANCE PROCEDURE:
1. Before each APU operation, ensure proper APU oil servicing.
2. If Service Oil Level Light (amber) or Low Oil Level Light (red) is inoperative,
check oil level on rod cap gauge/dipstick (if installed).
3. If oil level shows “MAX” on near “MAX”, the APU may be operated.
4. Aerocraft without a dipstick may dispatch with amber light inoperative provided
red light illuminates during momentary BULB TEST and does not illuminate in
CHECK OIL LEVEL position.
5. Record all APU operation time.
OPERATIONAL PROCEDURE:
Record all APU operation time.
PLACARDING PROCEDURE:
1. Place an INOP placard on affected light.
2. Place a placard stating, “RECORD ALL APU OPERATING TIMES” on the APU
panel.
31-50-04-01
Battery Overtemp Indication BATT O’TEMP Annunciator (Units 50016000)
C/1/0
May be inoperative (failure to illuminate) provided aerocraft is equipped with a lead-acid
battery.
PLACARDING PROCEDURE:
Place a placard stating, “BATT O’TEMP ANNUN INOP” on the instrument panel in view
of the flight crew.
56XCOMPEU-01-00
31-7
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-04-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Battery Overtemp Indication BATTERY OVERTEMP Red CAS
Message (Units 6001 and on)
C/1/0
May be inoperative (failure to illuminate) provided aerocraft is equipped with a lead-acid
battery.
PLACARDING PROCEDURE
Place a placard stating “RED BATTERY OVERTEMP MSG INOP” adjacent to the
EICAS display.
31-50-05-01
Cabin Altitude Warning System Indication CAB ALT (Units 50016000)
C/1/0
(O) May be inoperative (failure to illuminate) provided is operated at 14,000 feet MSL or
below.
OPERATIONAL PROCEDURE:
1. Flight planning must consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning must consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s must be taken into account for planned route.
PLACARDING PROCEDURE:
Place an INOP placard over the red CAB ALT annunciator.
56XCOMPEU-01-00
31-8
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-05-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Altitude Warning System Indication CABIN ALTITUDE Red
CAS Message (Units 6001 and on)
C/1/0
(O) May be inoperative (failure to illuminate) provided aerocraft is operated at 14,000
feet MSL or below.
OPERATIONAL PROCEDURE:
1. Flight planning must consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning must consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s must be taken into account for planned route.
PLACARDING PROCEDURE:
Place a placard stating, “RED CABIN ALTITUDE CAS MSG INOP” on the instrument
panel in view of the flight crew.
31-50-06-01
Cabin Door Indication 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, and
d) Aerocraft is operated at FL 250 or below.
OPERATIONAL PROCEDURE:
1. Once the aerocraft has been boarded, a crew member must close and latch
cabin door.
2. Verify all green door pin flags are visible.
3. Locate an unscrew cabin vent door access cover on aft side of cabin door steps.
4. Depress cabin vent door lever to ensure vent door is CLOSED.
5. Replace vent door cover.
PLACARDING PROCEDURE:
Place a placard stating, “CABIN DOOR ANNUN INOP” on the instrument panel in view
of the flight crew.
56XCOMPEU-01-00
31-9
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-06-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Door Indication 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) Aerocraft is operated at FL 250 or below.
OPERATIONAL PROCEDURE:
1. Once the aerocraft has been boarded, a crew member must close and latch
cabin door.
2. Verify all green door pin flags are visible.
3. Locate an unscrew cabin vent door access cover on aft side of cabin door steps.
4. Depress cabin vent door lever to ensure vent door is CLOSED.
5. Replace vent door cover.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER CABIN DOOR CAS MSG INOP” adjacent to the EICAS
display.
31-50-06-03
Cabin Door Indication Light System (6-Pack)
B/10
(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) Aerocraft is operated at FL 250 or below.
OPERATIONAL PROCEDURE:
1. During AFM COCKPIT PREPARATION Normal Procedure, verify the CABIN
DOOR annunciator illuminates during Rotary Test procedure
2. Prior to Pitch Trim – CHECK/SET test, a crew member must close cabin door
and verify CABIN DOOR annunciator illuminates.
3. Once the aerocraft has been boarded, a crew member must close and latch
cabin door.
4. Verify all green door pin flags are visible.
5. Locate and unscrew cabin vent door access cover on aft side of cabin door
steps.
6. Depress cabin vent door lever to ensure vent door is CLOSED.
7. Replace vent door cover.
PLACARDING PROCEDURE:
56XCOMPEU-01-00
31-10
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Place an INOP placard on the affected light system.
31-50-07-01
Cabin Door Seal Indication DOOR SEAL Annunciation 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) Aerocraft is operated at FL 250 or below.
OPERATIONAL PROCEDURE:
CAUTION:
Extreme care must be exercised not to close door with door pins
extended. Damage will result.
CAUTION:
Holding the plunger longer that a few seconds can damage the seal.
The primary door seal and acoustic seal should inflate. The primary
seal should remain inflated when the plunger is released.
1. Position aerocraft in a suitable run-up area and chock both main landing gear.
2. With a member of the flight crew or a qualified technician in the Pilot seat and
using AFM Normal Procedures, start the APU or one engine (Right engine is
preferred).
3. With cabin door OPEN, move door handle to LOCKED position.
4. Momentarily depress door seal plunger located in the lower aft door pin
receptacle and allow door seals to inflate.
5. Move door handle to OPEN position and stow handle. Primary door seal should
deflate.
6. Using AFM Normal Procedures, power down aircraft.
PLACARDING PROCEDURE:
Place a placard stating, “DOOR SEAL ANNUN INOP” on the instrument panel in view of
the flight crew.
56XCOMPEU-01-00
31-11
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-07-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Door Seal Indication 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) Aerocraft is operated at FL 250 or below.
OPERATIONAL PROCEDURE:
CAUTION:
Extreme care must be exercised not to close door with door pins
extended. Damage will result.
CAUTION:
Holding the plunger longer than a few seconds can damage the seal.
The primary door seal and acoustic seal should inflate. The primary
seal should remain inflated when the plunger is released.
1. Position aerocraft in a suitable run-up area and chock both main landing gear.
2. With a member of the flight crew or a qualified technician in the Pilot seat and
using AFM Normal Procedures, start the APU or one engine (Right engine is
preferred).
3. With cabin door OPEN, move door handle to LOCKED position.
4. Momentarily depress door seal plunger located in the lower aft door pin
receptacle and allow door seals to inflate.
5. Move door handle to OPEN position and stow handle. Primary door seal should
deflate.
6. Using AFM Normal Procedures, power down aircraft.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER CABIN DOOR SEAL CAS MSG INOP” adjacent to the
EICAS display.
56XCOMPEU-01-00
31-12
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-08-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Emergency Pressurization Indication EMER PRESS Annunciator
(Units 5001-6000)
C/1/0
(M) May be inoperative (failure to illuminate) provided the emergency pressurization
system is verified operative.
MAINTENANCE PROCEDURE:
CAUTION:
Make sure the parking brake is set. The brakes will not function
when the squat switch is disabled or in the air position.
1. Position aerocraft in a suitable run-up area and chock both main landing gear.
2. Connect landing gear squat switch breakout box to LH GEAR WELL DISC
electrical connector.
3. Set PARK BRAKE.
4. Using AFM Normal Procedures, start left engine and advance throttle to 60% N2.
5. Select PRESS SOURCE to EMER.
6. Set squat switch on landing gear breakout box to IN AIR.
7. Listen for increased airflow in cabin.
8. Select PRESS SOURCE to OFF. Airflow should stop.
9. Bring the throttle to idle and set the squat switch breakout box to ON GROUND.
10. Using AFM Normal Procedures, power down aircraft.
PLACARDING PROCEDURE:
Place an INOP placard on EMER PRESS light.
56XCOMPEU-01-00
31-13
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-08-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Emergency Pressurization Indication 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.
MAINTENANCE PROCEDURE:
CAUTION:
Make sure the parking brake is set. The brakes will not function
when the squat switch is disabled or in the air position.
1. Position aerocraft in a suitable run-up area and chock both main landing gear.
2. Connect landing gear squat switch breakout box to LH GEAR WELL DISC
electrical connector.
3. Set PARK BRAKE.
4. Using AFM Normal Procedures, start left engine and advance throttle to 60% N2.
5. Select PRESS SOURCE to EMER.
6. Set squat switch on landing gear breakout box to IN AIR.
7. Listen for increased airflow in cabin.
8. Select PRESS SOURCE to OFF. Airflow should stop.
9. Bring the throttle to idle and set the squat switch breakout box to ON GROUND.
10. Using AFM Normal Procedures, power down aircraft.
PLACARDING PROCEDURE:
Place a placard stating, “(COLOR) EMERGENCY PRESSURIZATION CAS MSG INOP”
adjacent to EICAS display.
31-50-09-01
Engine Anti Ice Indication ENG ANTI-ICE, L or R Annunciator (Units
5001-6000)
C/2/1
One may be inoperative (failure to illuminate) provided:
a) Aerocraft is not operated in visible moisture with ram air temperature of +10
degrees C or below, and
b) Aerocraft is not operated in known or forecast icing conditions.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SYSTEM) ANNUN INOP” on the instrument panel
in view of the flight crew.
56XCOMPEU-01-00
31-14
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-09-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Engine Anti Ice Indication ENG ANTI ICE COLD L – R Amber or
ENG ANTI ICE COLD L – R White CAS Message (Units 6001 and on)
C/2/1
One may be inoperative (failure to illuminate) provided:
a) Aerocraft is not operated in visible moisture with ram air temperature of +10
degrees C or below, and
b) Aerocraft is not operated in known or forecast icing conditions.
PLACARDING PROCEDURE:
Place a placard stating, “(COLOR) ENG ANTI ICE (AFFECTED SIDE(S)) INOP”
adjacent to the EICAS display.
31-50-10-01
Exterior Door Unlocked Indication 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.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SYSTEM) ANNUN INOP” on the instrument panel
in view of the flight crew.
31-50-10-02
Exterior Door Unlocked Indication 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.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER NOSE DOOR CAS MSG INOP” adjacent to the EICAS
display.
56XCOMPEU-01-00
31-15
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-10-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Exterior Door Unlocked Indication 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.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER TAILCONE ACC DOOR CAS MSG INOP” adjacent to
the EICAS display.
31-50-10-04
Exterior Door Unlocked Indication 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.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER BATTERY DOOR CAS MSG INOP” adjacent to the
EICAS display.
31-50-10-05
Exterior Door Unlocked Indication 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.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER BAGGAGE DOOR CAS MSG INOP” adjacent to the
EICAS display.
56XCOMPEU-01-00
31-16
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-12-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Generator (D.C.) Indication 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.
OPERATIONAL PROCEDURE:
1. Prior to each takeoff the pilot must turn the affected generator system OFF and
turn voltage select knob to the affected side and check for normal bus voltage. If
bus voltage is normal, turn unaffected side ON and check for shared amperage
load.
2. During all phases of aerocraft operation, the pilot must check for correct voltage
and amperage at least every 15 minutes.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SYSTEM) INOP” over the GEN OFF annunciator.
31-50-12-02
Generator (D.C.) Indication 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.
OPERATIONAL PROCEDURE:
1. Prior to each takeoff the pilot must turn the affected generator system OFF and
turn voltage select knob to the affected side and check for normal bus voltage. If
bus voltage is normal, turn unaffected side ON and check for shared amperage
load.
2. During all phases of aerocraft operation, the pilot must check for correct voltage
and amperage at least every 15 minutes.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER (AFFECTED SYSTEM) DC GEN OFF CAS MSG
INOP” adjacent to the EICAS display.
56XCOMPEU-01-00
31-17
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-13-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Hydraulic Flow Indication LO HYD FLOW, L or R Annunciator (Units
5001-6000)
C/21/
(O) May be inoperative (failure to illuminate) provided hydraulic system operation is
verified with only the affected side engine operating prior to each flight.
OPERATIONAL PROCEDURE:
1.
2.
3.
4.
Verify adequate hydraulic fluid level.
Position aerocraft in suitable run-up area and chock both main landing gear.
Using AFM Normal Procedures start engine on affected side.
Cycle speed brakes and thrust reversers on operating engine and flaps to verify
normal actuation times, hydraulic system on affected side is functional and that
this is only an indication issue.
5. Using AFM Normal Procedures, power down aircraft.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SYSTEM) LO HYD FLOW ANNUN INOP” on the
instrument panel in view of the flight crew.
31-50-13-02
Hydraulic Flow Indication HYDRAULIC FLOW LOW Amber CAS
Message (Units 6001 and on)
C/2/1
(O) May be inoperative (failure to illuminate) provided hydraulic system operation is
verified with only the affected side engine operating prior to each flight.
OPERATIONAL PROCEDURE:
1.
2.
3.
4.
Verify adequate hydraulic fluid level.
Position aerocraft in suitable run-up area and chock both main landing gear.
Using AFM Normal Procedures start engine on affected side.
Cycle speed brakes and thrust reversers on operating engine and flaps to verify
normal actuation times, hydraulic system on affected side is functional and that
this is only an indication issue.
5. Using AFM Normal Procedures, power down aircraft.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER (AFFECTED SYSTEM) HYDRAULIC FLOW LOW
CAS MSG INOP” adjacent to the EICAS display.
56XCOMPEU-01-00
31-18
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-14-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Hydraulic Fluid Level Indication 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.
OPERATIONAL PROCEDURE:
Before each flight, a crew member must visually verify hydraulic fluid level for proper
servicing.
PLACARDING PROCEDURE:
Place a placard stating, “LO HYD LEVEL ANNUN INOP” on the instrument panel in view
of the flight crew.
31-50-14-02
Hydraulic Fluid Level Indication 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.
OPERATIONAL PROCEDURE:
Before each flight, a crew member must visually verify hydraulic fluid level for proper
servicing.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER HYDRAULIC FLUID LOW CAS MSG INOP” adjacent
to the EICAS display.
56XCOMPEU-01-00
31-19
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-15-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Lavatory Door Indication LAV DOOR Annunciator System (Units
5001-6000)
B/1/0
May be inoperative (failure to illuminate or extinguish) provided lavatory door is visually
verified latched or secured open prior to each taxi, takeoff, or landing.
OPERATIONAL PROCEDURE:
1. Prior to each taxi, takeoff or landing, a crew member must physically inspect the
lavatory door to ensure it is latched in the OPEN position.
2. On passenger-carrying flight:
a. Flight crew must brief passengers that the lavatory door must be kept
latched in the OPEN position while the lavatory is not in use, and that the
door must be latched OPEN for takeoff and prior to landing. Flight crew
may ask passengers to assist with this task.
b. Prior to takeoff and landing, a crew member must observe the lavatory
door and ensure it is latched OPEN. If there is any doubt, a passenger
may physically ensure the lavatory door is latched OPEN.
3. On non-passenger flights:
a. A crew member must physically verify the lavatory door is latched OPEN
prior to takeoff.
b. Following any biological visit to lavatory. The crew member must latch
lavatory door in OPEN position.
4. Prior to landing, a crew member must look through the cabin to ensure lavatory
door is still latched OPEN.
PLACARDING PROCEDURE:
Place a placard stating, “LAV DOOR ANNUN INOP” on the instrument panel in view of
the flight crew.
56XCOMPEU-01-00
31-20
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-15-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Lavatory Door Indication LAVATORY DOOR Amber CAS Message
(Units 6001 and on)
B/1/0
May be inoperative (failure to illuminate or extinguish) provided lavatory door is visually
verified latched or secured open prior to each taxi, takeoff, or landing.
OPERATIONAL PROCEDURE:
1. Prior to each taxi, takeoff or landing, a crew member must physically inspect the
lavatory door to ensure it is latched in the OPEN position.
2. On passenger-carrying flight:
a. Flight crew must brief passengers that the lavatory door must be kept
latched in the OPEN position while the lavatory is not in use, and that the
door must be latched OPEN for takeoff and prior to landing. Flight crew
may ask passengers to assist with this task.
b. Prior to takeoff and landing, a crew member must observe the lavatory
door and ensure it is latched OPEN. If there is any doubt, a passenger
may physically ensure the lavatory door is latched OPEN.
3. On non-passenger flights:
a. A crew member must physically verify the lavatory door is latched OPEN
prior to takeoff.
b. Following any biological visit to lavatory. The crew member must latch
lavatory door in OPEN position.
4. Prior to landing, a crew member must look through the cabin to ensure lavatory
door is still latched OPEN.
PLACARDING PROCEDURE:
Place a placard stating, “AMBER LAVATORY DOOR CAS MSG INOP” adjacent to the
EICAS display.
31-50-16-01
Master Warning/Caution Light System Master Warning Light (Failure
to Illuminate)
C/2/1
PLACARDING PROCEDURE:
Place an INOP placard on the affected master warning light.
56XCOMPEU-01-00
31-21
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-16-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Master Warning/Caution Light System Master Warning Reset
Function
C/2/1
PLACARDING PROCEDURE:
Place a placard stating, “MASTER WARN RESET INOP” adjacent to the affected master
warn system.
31-50-16-03
Master Warning/Caution Light System Master Caution Light
C/2/1
PLACARDING PROCEDURE:
Place an INOP placard on the affected master warning light.
56XCOMPEU-01-00
31-22
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-16-44
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Master Warning/Caution Light System Master Caution Reset
Function
C/2/1
PLACARDING PROCEDURE:
Place a placard stating, “MASTER CAUTION RESET INOP” adjacent to the affected
master warn system.
31-50-17-01
Pitot/Static Heater Indication P/S HTR, L or R or STBY P/S HTR
Annunciators (Units 5001-6000)
B/3/1
(O) May be inoperative (failure to illuminate) provided:
a) Pitot/static heater systems are verified operative before each takeoff,
b) Aerocraft is not operated in visible moisture with ram air temperature of +10
degrees C or below, and
c) Aerocraft is not operated in known or forecast icing conditions.
OPERATIONAL PROCEDURE:
During the EXTERIOR INSPECTION, a crew member must physically verify pitot/static
heaters are operative.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SYSTEM) ANNUN INOP” on the instrument panel
in view of the flight crew.
56XCOMPEU-01-00
31-23
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-17-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Pitot/Static Heater Indication PITOT/STATIC COLD L – R – STBY
Amber or PITOT/STATIC COLD L – R – STBY White CAS Message
(Units 6001 and on)
B/2/0
(O) May be inoperative (failure to illuminate) provided:
a) Pitot/static heater systems are verified operative before each takeoff,
b) Aerocraft is not operated in visible moisture with ram air temperature of +10
degrees C or below, and
c) Aerocraft is not operated in known or forecast icing conditions.
OPERATIONAL PROCEDURE:
During the EXTERIOR INSPECTION, a crew member must physically verify pitot/static
heaters are operative:
a. Pitot:
i. Left side – Pilot
ii. Right side – Copilot
iii. Right side aft probe – Standby
b. Static ports:
i. Left side forward lower port – Pilots primary
ii. Right side forward upper port – Pilot secondary
iii. Left side aft middle port – Pilots standby
iv. Right side forward lower port – Copilots primary
v. Left side forward upper port – Copilot secondary
vi. Right side aft middle port – Copilots standby
PLACARDING PROCEDURE:
Place a placard stating, “(COLOR) (AFFECTED SYSTEM) CAS MSG INOP” adjacent to
the EICAS display.
31-50-18
TAWS Annunciator (PULL UP, TERRAIN, BELOW G/S) Units 50015500)
B/-/0
May be inoperative (failure to illuminate) provided affected aural warning is operative.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SYSTEM) ANNUN INOP” adjacent to the affected
annunciator.
56XCOMPEU-01-00
31-24
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-19-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Wing Anti-Ice Indication WING ANTI-ICE, L or R Annunciator (Units
5001-6000)
C/2/1
One may be inoperative (failure to illuminate) provided:
a) Aerocraft is not operated in visible moisture with ram air temperature of +10
degrees C or below, and
b) Aerocraft is not operated in known or forecast icing conditions.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SYSTEM) ANNUN INOP” on the instrument panel
in view of the flight crew.
31-50-19-02
Wing Anti-Ice Indication WING ANTI-ICE COLD, L – R Amber or
WING ANTI-ICE COLD, L – R White CAS Message (Units 6001 and
on)
C/2/1
One may be inoperative (failure to illuminate) provided:
a) Aerocraft is not operated in visible moisture with ram air temperature of +10
degrees C or below, and
b) Aerocraft is not operated in known or forecast icing conditions.
PLACARDING PROCEDURE:
Place a placard stating, “(COLOR) (AFFECTED SYSTEM) CAS MSG INOP” adjacent to
the EICAS display.
56XCOMPEU-01-00
31-25
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
31-50-21
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flight Director Mode Selector Annunciator (Units 5001-6000)
C/-/0
(O) May be inoperative provided flight crew verifies annunciation(s) displayed on the
PFD is appropriate to function selected.
OPERATIONAL PROCEDURE:
1. During flight, the crew member selecting a flight director mode must verbalize the
mode selected.
2. Second crew member must respond by verbalizing the flight director mode
displayed on the PFD.
PLACARDING PROCEDURE:
Place placards above both PFD’s stating, “XXX, XXX FD MODE LIGHTS INOP” where
“XXX, XXX” are the specific flight director mode lights that are inoperative.
56XCOMPEU-01-00
31-26
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-10-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cockpit and Instrument Lighting System (Excluding Internally
Lighted Annunciators and Buttons, and Standby Flight Instrument
Lighting)
C/-/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.
PLACARDING PROCEDURE:
Place a placard stating, “(AFFECTED SYSTEM) LIGHTS INOP” on the instrument panel
in view of the flight crew.
33-10-02-01
Windshield Ice Detect Light
C/2/1
(O) One may be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE:
During night operations, a crew member must inspect the windshield for ice
accumulation every fifteen (15) minutes using the operative ice detect light.
PLACARDING PROCEDURE:
Place an INOP placard adjacent to affected light.
33-10-02-02
Windshield Ice Detect Light
C/2/0
May be inoperative provided aerocraft is not operated at night.
PLACARDING PROCEDURE:
Place an INOP placard adjacent to the affected light
56XMELEUCL-01-01
33-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-20-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Interior Lighting System (Excludes Cabin Emergency Lighting
System)
C/-/(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.
OPERATIONAL PROCEDURE
1. Do not apply power to Aeroplane.
2. Prior to each flight, crew member shall select EMER LTS to ARM and INTERIOR
MASTER toggle to OFF.
3. Crew shall verify the following lights illuminate:
a. Cabin Overhead Lights:
i. Left Forward
ii. Right Forward
iii. Right mid-cabin
iv. Left aft
v. Emergency Exit Door
b. Exit Signs:
i. Above main cabin door
ii. Above Emergency exit door
iii. Left aft cabin/vanity divider
iv. Every third bulb of Left and Right forward section
v. Aft section dropped aisle lighting
c. Exit Indicators:
i. Forward and aft of main cabin door
ii. Below Emergency exit door
4. A member of the crew shall verify that there is sufficient lighting to perform
required duties.
PLACARDING PROCEDURE
Place an INOP placard on affected light(s).
56XMELEUCL-01-01
33-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-20-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Interior Lighting System (Excludes Cabin Emergency Lighting
System)
C/-/0
(O) May be inoperative provided:
a) Cabin emergency lighting is verified operative, and
b) No cabin occupants are carried.
OPERATIONAL PROCEDURE:
1. Do not apply power to aircraft.
2. Prior to each flight, crew member must select EMER LTS to ARM and INTERIOR
MASTER toggle to OFF.
3. Crew must verify the following lights illuminate:
a. Cabin Overhead Lights:
i. Left Forward
ii. Right Forward
iii. Right mid-cabin
iv. Left aft
v. Emergency Exit Door
b. Exit Signs:
i. Above main cabin door
ii. Above Emergency exit door
iii. Left aft cabin/vanity divider
iv. Every third bulb of Left and Right forward section
v. Aft section dropped aisle lighting
c. Exit Indicators:
i. Forward and aft of main cabin door
ii. Below Emergency exit door
PLACARDING PROCEDURE:
Place an INOP placard on affected light(s).
33-20-02-01
Divider Accent Light Incandescent
C/-/-
PLACARDING PROCEDURE
Place an INOP placard over the affected light.
56XMELEUCL-01-01
33-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-20-02-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Divider Accent Light LED
C/-/-
PLACARDING PROCEDURE
Place an INOP placard over the affected light.
33-20-03-01
Cabin Signs (Fasten Seat Belt and No Smoking Signs (Excludes
Cabin Emergency Lighting System)
C/-/(O) May be inoperative provided alternate procedures for notifying cabin occupants are
established and used.
OPERATIONAL PROCEDURE
A crew member shall use the PA system to make appropriate announcements.
PLACARDING PROCEDURE
Place an INOP placard on the affected light/sign.
33-20-03-02
Cabin Signs (Fasten Seat Belt and No Smoking Signs (Excludes
Cabin Emergency Lighting System)
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.
OPERATIONAL PROCEDURE
A crew member shall use the PA system to make appropriate announcements.
PLACARDING PROCEDURE
Place an INOP placard on the affected light/sign.
56XMELEUCL-01-01
33-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-20-03-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Signs (Fasten Seat Belt and No Smoking Signs (Excludes
Cabin Emergency Lighting System)
C/-/0
May be inoperative provided no passengers are carried.
PLACARDING PROCEDURE
Place an INOP placard on the affected light/sign.
33-20-04
Exit Sign Lighting (Incandescent)
C/-/Two light bulbs may be inoperative in each fixture.
PLACARDING PROCEDURE
Place a placard stating “(# BULBS) INOP” adjacent to the affected light.
33-20-05
Light Source for Pyramid Exit Sign (LED) (Units 5501 and on)
C/16/14
PLACARDING PROCEDURE
Place a placard stating “(# OF ELEMENTS) INOP” adjacent to the affected exit sign.
33-40-01
Anti-Collision Lights (Wing-Tip Strobe Lights)
C/-/May be inoperative provided the Aeroplane is not operated at night.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light (s).
33-40-02-01
Fuselage Mounted Taxi/Landing Light (No night)
C/2/0
May be inoperative provided the Aeroplane is not operated at night.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
56XMELEUCL-01-01
33-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-40-02-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Fuselage Mounted Taxi/Landing Light
C/2/1
50% of taxi lights may be inoperative for night operations.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-03
Ground Recognition Light (Flashing Beacon)
C/1/0
(O) May be inoperative for daylight operations provided all white anti-collision lights are
operative.
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.
OPERATIONAL PROCEDURE
If Aeroplane is operated at night, make sure all personnel in the vicinity of the Aeroplane
are made aware of intended Aeroplane operations.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch
33-40-04
Logo Light (If installed)
C/2/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-05
Navigation/Position Lights
C/1/0
May be inoperative provided aeroplane is not operated at night.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
56XMELEUCL-01-01
33-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-40-06
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Pulse Light System (If installed)
D/1/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-07
Tail Cone Baggage Compartment Light
C/3/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-08
Tail Cone Maintenance Compartment Light
C/1/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-09
Toilet Service Light
C/-/0
(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE
a) Empty toilet contents and do not refill through servicing vehicle.
b) Carefully pour two (2) gallons of toilet solution into toilet.
c) Repeat procedure for each usage of toilet.
PLACARDING PROCEDURE
Place an INOP placard adjacent to toilet service lights.
56XMELEUCL-01-01
33-7
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-40-10-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Wing Illumination/Inspection Light
D/-/0
One or more may be inoperative for daylight operations.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-10-02
Wing Illumination/Inspection Light
C/2/1
One may be inoperative provided ground deicing procedures do not require its use.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-11-01
Wing Leading Edge Landing Light
C/-/0
All may be inoperative for daylight operations.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-11-02
Wing Leading Edge Landing Light
B/2/1
One may be inoperative for night operations provided fuselage mounted taxi/landing light
on associated side is operative.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-40-12-01
Wingtip Mounted Recognition Light
C/2/0
May be inoperative provided aeroplane is not operated at night.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
56XMELEUCL-01-01
33-8
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-40-12-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Wingtip Mounted Recognition Light
C/2/1
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light switch.
33-50-01
Exterior Emergency Light
B/3/0
May be inoperative for daylight operations.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SYSTEM) INOP” on the instrument panel in view
of the flight crew.
33-50-03-01
Floor Proximity Emergency Escape Path Marking System Light Left
Forward Half incandescent bulbs (Emergency Lighting)
B/-/Up to six bulbs (three pairs) may be inoperative provided no two adjacent pairs are
inoperative.
PLACARDING PROCEDURE
Place a placard stating “(# BULBS) EMER PATH LIGHTS INOP” on the side of the cabin
seat floorboard directly above the affected light(s).
33-50-03-02
Floor Proximity Emergency Escape Path Marking System Light Left
Forward Half LED (Emergency Lighting)
B/-/Up to four elements may be inoperative within any two foot length.
PLACARDING PROCEDURE
Place a placard stating “(# LEDs) EMER PATH LIGHTS INOP” on the side of the cabin
seat floorboard directly above the affected light(s).
56XMELEUCL-01-01
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-50-03-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Floor Proximity Emergency Escape Path Marking System Light Left
Half Aft
B/-/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light system.
33-50-03-04
Floor Proximity Emergency Escape Path Marking System Light
Right Aft Half incandescent bulbs (Emergency Lighting)
B/-/Up to six bulbs (three pairs) may be inoperative provided no two adjacent pairs are
inoperative.
PLACARDING PROCEDURE
Place a placard stating “(# BULBS) EMER PATH LIGHTS INOP” on the side of the cabin
seat floorboard directly above the affected light(s).
33-50-03-05
Floor Proximity Emergency Escape Path Marking System Light
Right Aft Half LED (Emergency Lighting)
B/-/Up to four elements may be inoperative within any two foot length.
PLACARDING PROCEDURE
Place a placard stating “(# LEDs) EMER PATH LIGHTS INOP” on the side of the cabin
seat floorboard directly above the affected light(s).
33-50-03-06
Floor Proximity Emergency Escape Path Marking System Light
Right Half Aft
B/-/0
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected light system.
56XMELEUCL-01-01
33-10
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
33-50-04
CESSNA AIRCRAFT COMPANY
MODEL 560XL
LED Light Source for Emergency Exit (Escape Hatch) (If installed)
C/20/17
PLACARDING PROCEDURE
CAUTION:
LED elements are very bright. Use appropriate eye protection when
looking at a lighted LED assembly.
Place a placard stating “(# OF ELEMENTS) INOP” adjacent to the affected light.
56XMELEUCL-01-01
33-11
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XMELEUCL-01-01
33-12
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Course Selector Knob
B/2/1
One may be inoperative provided it is not required by procedures.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected knob.
34-00-02
Moving Map Display (If installed)
C/-/May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place a placard stating, “MOVING MAP INOP” adjacent to the affected display.
34-00-03-01
VHF Navigation System VOR
C/2/0
May be inoperative provided:
a) Procedures do not require its use, and
b) System is not required by regulations.
PLACARDING PROCEDURE
Place an INOP placard adjacent to/on the affected equipment.
34-00-03-02-10
VHF Navigation System ILS 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.
PLACARDING PROCEDURE
Place a placard stating “LOC INOP” adjacent to the affected equipment.
56XCOMPEU-01-00
34-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-00-03-02-20
CESSNA AIRCRAFT COMPANY
MODEL 560XL
VHF Navigation System ILS Glideslope
C/2/0
May be inoperative provided:
a) Procedures do not require its use, and
b) System is not required by regulations.
PLACARDING PROCEDURE
Place a placard stating “ILS GS INOP” adjacent to the affected equipment.
34-18-01
Angle of Attack Gauge (Units 5001-6000)
C/1/0
PLACARDING PROCEDURE
Place an INOP placard on the affected gauge.
34-18-02
Angle of Attack Indexer
C/1/0
PLACARDING PROCEDURE
Place an INOP placard on the affected indicator.
56XCOMPEU-01-00
34-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-18-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
PLACARDING PROCEDURE
Place a placard stating “AOA HTR INOP NO FLIGHT INTO KNOWN ICING” on the
instrument panel in view of the flight crew.
34-20-01
Slip-Skid Indicator (Bezel mounted inclinometer) (Units 5001-6000)
B/3/1
Two may be inoperative provided each pilot has either a bezel mounted slip indicator or
a PFD displayed slip indicator.
PLACARDING PROCEDURE
Place an INOP placard on the affected indicator.
34-23-01
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.
PLACARDING PROCEDURE
Place an INOP placard on the magnetic compass.
34-25-01-01-10
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) Descent Height/Minimum Descent
Altitude Select Knob (Units 5501-6000)
C/2/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place a placard stating “DH/MDA KNOB INOP” adjacent to the affected knob.
56XCOMPEU-01-00
34-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-01-01-15
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) Elapsed Time Function Switch
(Units 5001-6000)
C/2/0
PLACARDING PROCEDURE
Place a placard stating “ELAPSE TIME INOP” below to the affected switch.
34-25-01-01-20
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) FMS Source Selector Switch (Units
5001-6000)
C/2/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place a placard stating “FMS SOURCE SELECT INOP” below the affected switch.
34-25-01-01-25
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) Ground Speed/Time to Go
(GSPD/TTG) Switch (Units 5001-5500)
C/2/0
PLACARDING PROCEDURE
Place a placard stating “GSPD/TTG INOP” below the affected switch.
34-25-01-01-30
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) Horizontal Indicator Mode Selector
Switch (HIS) (Units 5501-6000)
C/2/0
NOTE: Weather radar requirements must be considered if ARC display modes are
inoperative on both PFDs and the MFD is inoperative.
PLACARDING PROCEDURE
Place a placard stating “HIS SWITCH INOP” below the affected switch.
56XCOMPEU-01-00
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-01-01-35
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) Preview Switch (Units 5501-6000)
C/2/0
PLACARDING PROCEDURE
Place a placard stating “PREVIEW INOP” below the affected switch.
34-25-01-01-40
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) RA/BARO Switch (Units 5001-6000)
(If installed)
C/2/0
May be inoperative provided the setting required for intended approach is available.
PLACARDING PROCEDURE
Place a placard stating “RA/BARO INOP” adjacent to the affected switch.
34-25-01-01-45
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) Radio Altitude Knob (Units 50015500)
C/2/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place a placard stating “RAD ALT KNOB INOP” adjacent to the affected knob.
34-25-01-01-50
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) Single Cue/Cross Pointer (SC/CP)
Switch (Units 5501-6000)
C/2/0
PLACARDING PROCEDURE
Place a placard stating “SC/CP SWITCH INOP” below the affected switch.
56XCOMPEU-01-00
34-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-01-01-55
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) “STANDARD” Barometer Pressure
Switch (Units 5001-6000)
C/2/0
PLACARDING PROCEDURE
Place an INOP placard over the affected switch.
34-25-01-01-60
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) 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.
PLACARDING PROCEDURE
Place a placard stating “VOR/LOC SOURCE SWITCH INOP” below the affected switch.
34-25-01-01-65
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) 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.
PLACARDING PROCEDURE
Place a placard stating WX/TERR SWITCH INOP” below the affected switch.
34-25-01-01-70
Display Controller – Honeywell Primary Flight Display (PFD)
Controller (Units 5001-6000) Bearing Pointer Select Knob (Units
5001-6000)
C/4/0
May be inoperative provided required bearing pointers are available for procedures.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected knob.
56XCOMPEU-01-00
34-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-01-02-10
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) Checklist Function Button (NORM,
EMER, RCL, PAG, SKP, ENT) (Units 5001-5500)
C/6/0
PLACARDING PROCEDURE
Place a placard stating “(FUNCTION) BUTTON INOP” below the affected button.
34-25-01-02-20
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) Checklist Function Button (NORM,
EMER, RCL, PAG, SKP, ESC) (Units 5501-6000)
C/6/0
PLACARDING PROCEDURE
Place a placard stating “(FUNCTION) BUTTON INOP” below the affected button.
34-25-01-02-30
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) 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.
PLACARDING PROCEDURE
Place a placard stating “KNOB INOP” adjacent to the affected knob.
34-25-01-02-40
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) ET ½ and ST ½ Button (Units 55016000)
C/4/0
PLACARDING PROCEDURE
Place an INOP placard over the affected button.
56XCOMPEU-01-00
34-7
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-01-02-50
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) Joystick Controller (Units 50015500)
C/1/0
PLACARDING PROCEDURE
Place a placard stating “JOYSTICK INOP” adjacent to the affected joystick.
34-25-01-02-55
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) Joystick Controller (Units 55006000)
C/1/0
May be inoperative provided PFD settings for baro set and metric alt are set correctly for
the intended flight.
PLACARDING PROCEDURE
Place a placard stating “JOYSTICK INOP” adjacent to the affected joystick.
34-25-01-02-60
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) MAP/PLAN SWITCH (Units 50016000)
C/1/0
PLACARDING PROCEDURE
Place a placard stating “MAP/PLAN SWITCH INOP” below the affected switch.
34-25-01-02-70
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) Range Selector (Units 5001-6000)
C/1/0
PLACARDING PROCEDURE
Place a placard stating “RANGE SELECT INOP” adjacent to the affected selector.
56XCOMPEU-01-00
34-8
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-01-02-80
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) Symbol Display Button (APT, VOR,
DAT) (Units 5001-5500)
C/3/0
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED FUNCTION) INOP” below the affected switch.
34-25-01-02-90
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) WX SWITCH (Units 5001-5500)
C/1/0
May be inoperative provided at least one PFD HSI switch operates normally.
PLACARDING PROCEDURE
Place an INOP placard over the affected switch.
34-25-01-02-95
Display Controller – Honeywell Multi Function Display (MFD)
Controller (Units 5001-6000) WX SWITCH (Units 5500-6000)
C/1/0
May be inoperative provided at least one PFD WX/TERR operates normally.
PLACARDING PROCEDURE
Place an INOP placard over the affected switch.
34-25-02
Multi Function Display Unit (MFD) (Units 5001 - 6000)
OPERATIONAL PROCEDURE
1. Verify both PFD’s are operational.
2. Prior to flight, each crew member shall verify all functions of their respective PFD
controller are operational.
3. If radar is required, it should be displayed on the PFD in 60 degree arc compass
rose presentation.
4. Traffic display on the MFD will be inoperative. Crew to brief response to any
aural alerts encountered. Crew also to brief use of alternate sources of display, if
available.
5. EGPWS display will be unavailable on MFD. Display should be selected on at
least one of the PFDs.
PLACARDING PROCEDURE
Place an INOP placard on the MFD.
56XCOMPEU-01-00
34-9
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-03-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Display Controller – Collins (Units 6001 and on) 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.
OPERATIONAL PROCEDURE:
Prior to flight, crew must brief on procedures to be used to accommodate controlling the
PFD via the applicable CCP.
PLACARDING PROCEDURE:
Place an INOP placard on the affected controller.
34-25-03-02
Display Controller – Collins (Units 6001 and on) 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.
OPERATIONAL PROCEDURE:
Prior to flight, crew must brief on procedures to be used to accommodate the loss of
function associated with the failed CCP.
PLACARDING PROCEDURE:
Place an INOP placard on the affected controller.
34-25-04
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.
OPERATIONAL PROCEDURE:
1. Verify both PFD’s are operational.
2. Make sure Engine instruments and CAS continue to be displayed appropriately.
PLACARDING PROCEDURE:
Place an INOP placard on the copilot’s MFD.
56XCOMPEU-01-00
34-10
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-05
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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, and
c) Autopilot is considered inoperative.
PLACARDING PROCEDURE
1. Make sure the command bars are not in view.
2. Place a placard stating “FLIGHT DIRECTOR INOP” adjacent to flight director.
34-25-06
Flight Director Mode Select Panel Functions (Units 6001 and on)
C/-/Individual functions may be inoperative provided:
a) Procedures do not require its use, and
b) AP XFER is operative.
PLACARDING PROCEDURE
Place a placard stating “(FUNCTION) INOP” adjacent to the affected flight director mode
select panel.
34-25-06-01
Flight Director Mode Select Panel Functions (Units 6001 and on) AP
(Autopilot)
B/1/0
May be inoperative provided:
a) Autopilot is considered inoperative, and
b) Aeroplane is not operated RVSM.
PLACARDING PROCEDURE
Place a placard stating “AP FUNC INOP/A/P INOP NO RVSM” above/adjacent to the
flight director mode select panel.
34-25-06-02
Flight Director Mode Select Panel Functions (Units 6001 and on) YD
(Yaw Damper)
B/1/0
May be inoperative provided autopilot and yaw damper can be engaged via AP push
button.
PLACARDING PROCEDURE
Place a placard stating “(YD INOP)” above the affected mode select button.
56XCOMPEU-01-00
34-11
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-25-07
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
Using tape, cover ONLY the heading data displayed so that it cannot be read by the
flight crew. Use caution so that the display face does not get scratched
PLACARDING PROCEDURE
Place a placard stating “HEADING DATA INOP” above the GH-3000 display.
34-25-08
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.
PLACARDING PROCEDURE
Place an INOP placard on the standby HSI.
34-25-09
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.
OPERATIONAL PROCEDURE
Prior to flight the crew shall make sure that heading and navigation information has
reverted to the GH-3000.
PLACARDING PROCEDURE
Place an INOP placard on the standby flight display.
56XCOMPEU-01-00
34-12
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-34-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
PLACARDING PROCEDURE
Place an INOP placard on the affected equipment.
34-35-01-01
Heads-Up Display (HUD) (If installed)
C/-/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place an INOP placard on the affected system
34-35-01-02
Heads-Up Display (HUD) (If installed)
C/-/0
(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE
If the HUD is integrated into normal procedures, especially during low visibility
operations, the crew must brief alternate procedures. The alternate procedures should
include increasing visibility requirements for the planned mission at the crew’s discretion.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
34-42-01
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.
PLACARDING PROCEDURE
Place an INOP placard on the weather radar controller.
56XCOMPEU-01-00
34-13
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-44-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
PLACARDING PROCEDURE
Place a placard stating “GPWS INOP” on the instrument panel in view of the flight crew.
34-44-01-01
Ground Proximity Warning System (GPWS) (If installed) 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.
PLACARDING PROCEDURE
Place a placard stating “GPWS MODE(S) (#) INOP” on the instrument panel in view of
the flight crew.
34-44-01-02
Ground Proximity Warning System (GPWS) (If installed) Test Mode
A/-/0
May be inoperative for a maximum of 6 flights or 25 flight hours or 2 calendar days,
whichever occurs first.
PLACARDING PROCEDURE
Place a placard stating “GPWS TEST INOP” on the instrument panel in view of the flight
crew.
34-44-01-03-10
Ground Proximity Warning System (GPWS) (If installed)
Glideslope Deviation (Mode 5)
B/-/0
May be inoperative.
PLACARDING PROCEDURE
Place a placard stating “GPWS GS INOP” on the instrument panel in view of the flight
crew.
56XCOMPEU-01-00
34-14
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-44-01-03-20
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Ground Proximity Warning System (GPWS) (If installed)
Glideslope Deviation (Mode 5)
C/-/0
May be inoperative for day VMC only.
PLACARDING PROCEDURE
Place a placard stating “GPWS GS INOP” on the instrument panel in view of the flight
crew.
34-44-01-04-10
Ground Proximity Warning System (GPWS) Terrain Awareness
Warning System (TAWS) (where required)
A/-/0
May be inoperative for a maximum of 10 calendar days provided the GPWS functions
are operative.
PLACARDING PROCEDURE
Place a placard stating “GPWS ADVISORY CALLOUTS INOP” on the instrument panel
in view of the flight crew.
34-44-01-04-20
Ground Proximity Warning System (GPWS) Terrain Awareness
Warning System (TAWS) (where required)
A/-/0
May be inoperative for a maximum of 6 flights or 25 flight hours or 2 calendar days,
whichever occurs first.
PLACARDING PROCEDURE
Place a placard stating “GPWS ADVISORY CALLOUTS INOP” on the instrument panel
in view of the flight crew.
56XCOMPEU-01-00
34-15
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-44-01-05
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Ground Proximity Warning System (GPWS) (If installed) Advisory
Callouts
C/-/0
(O) May be inoperative provided alternate procedures are established and used.
NOTE: Check Flight Manual limitations for approach minima.
OPERATIONAL PROCEDURE
Crew briefings shall include aural callouts through use of appropriate Aeroplane
equipment to make sure obstacle and terrain clearance.
PLACARDING PROCEDURE
Place a placard stating “GPWS ADVISORY CALLOUTS INOP” on the instrument panel
in view of the flight crew.
34-44-01-06
Ground Proximity Warning System (GPWS) (If installed) Windshear
Mode (If installed) 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.
OPERATIONAL PROCEDURE
1. Crew briefings shall include aural callouts through use of appropriate Aeroplane
equipment (airspeed, IVSI, etc.) and available weather reports for detection and
prompt resolution of windshear encounter.
2. Prior to each takeoff and approach, crew shall obtain weather reports to ensure
windshear conditions are neither reported or forecast for route of flight.
PLACARDING PROCEDURE
Place a placard stating “GPWS WINDSHEAR MODE INOP” on the instrument panel in
view of the flight crew.
56XCOMPEU-01-00
34-16
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-44-01-07
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Terrain Awareness Warning System (TAWS)/Ground Proximity
Warning System with Class B TAWS Required Runway Awareness &
Advisory System (RAAS)
C/1/0
PLACARDING PROCEDURE:
Place a placard stating, “RAAS INOP” on the instrument panel in view of the flight crew.
34-44-02
Radio Altimeter System
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.
PLACARDING PROCEDURE
Place a placard stating “TAWS/GPWS, RAD ALT INOP” on the instrument panel in view
of the flight crew.
34-44-03
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.
OPERATIONAL PROCEDURE
1. Flight planning shall consider the fuel burn associated with flight at lower altitude
and affect on range.
2. MEA’s shall be taken into account for planned route.
PLACARDING PROCEDURE
Place a placard stating “ALTITUDE ALERTING INOP” on the instrument panel in view of
the flight crew.
56XCOMPEU-01-00
34-17
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-45-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Airborne Collision Avoidance System (ACAS) ACAS System
A/-/0
(M) (O) May be inoperative for a maximum of 10 calendar days provided the system is
deactivated and secured.
MAINTENANCE PROCEDURE
Pull and secure ACAS circuit breaker.
OPERATIONAL PROCEDURE
Flight crew shall brief on operations without the use of ACAS.
PLACARDING PROCEDURE
Place a placard stating “ACAS INOP” on the instrument panel in view of the flight crew.
34-45-01-02
Airborne Collision Avoidance System (ACAS) 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.
OPERATIONAL PROCEDURE
Flight crew shall brief on see and avoid operations to prevent traffic conflicts.
PLACARDING PROCEDURE
Place a placard stating “ACAS TA/RA INOP” on the instrument panel in view of the flight
crew.
34-45-01-03-10 Airborne Collision Avoidance System (ACAS) Resolution
Advisory (RA) Display System(s)
C/-/1
(O) One may be inoperative on the non-flying pilot side.
OPERATIONAL PROCEDURE
Flying pilot shall monitor ACAS for TA guidance.
PLACARDING PROCEDURE
Place a placard stating “ACAS RA INOP” on the instrument panel in view of the flight
crew.
56XCOMPEU-01-00
34-18
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
34-45-01-03-20 Airborne Collision Avoidance System (ACAS) Resolution
Advisory (RA) Display System(s)
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.
OPERATIONAL PROCEDURE
Flight crew shall brief on operations with an inoperative RA system.
PLACARDING PROCEDURE
Place a placard stating “ACAS RA INOP” on the instrument panel in view of the flight
crew.
34-45-01-04-10
Airborne Collision Avoidance System (ACAS) Traffic Alert (TA)
Display System(s)
C/-/0
(O) One or more may be inoperative provided all installed RA display and audio
functions are operative.
OPERATIONAL PROCEDURE
Flight crew will brief on operations with an inoperative TA system.
PLACARDING PROCEDURE
Place a placard stating “ACAS TA INOP” on the instrument panel in view of the flight
crew.
34-45-01-04-20
Airborne Collision Avoidance System (ACAS) Traffic Alert (TA)
Display System(s)
C/-/1
One may be inoperative on non-flying pilot side.
PLACARDING PROCEDURE
Place a placard stating “ACAS TA INOP” on the instrument panel in view of the flight
crew.
56XCOMPEU-01-00
34-19
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-45-01-05
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Airborne Collision Avoidance System (ACAS) Audio Function
B/1/0
May be inoperative provided ACAS is considered inoperative.
PLACARDING PROCEDURE
Place a placard stating, “(AFFECTED FUNCTION) INOP” on the instrument panel in
view of the flight crew.
34-45-01-06
Airborne Collision Avoidance System (ACAS) Airspace Selection
Function (If installed)
C/-/0
PLACARDING PROCEDURE
Place a placard stating, “TCAS AIRSPACE INOP” on the instrument panel in view of the
flight crew.
34-46-01
Lightning Detection System (If installed)
C/1/Any in excess of those required by regulations may be inoperative.
PLACARDING PROCEDURE
Place an INOP placard on the affected equipment.
34-51-01
Distance Measuring Equipment (DME) Systems
C/1/Any in excess of those required by regulations may be inoperative.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
34-52-01-01-10
SSR Transponder Mode A/C Functions
C/-/Any in excess of those required for the route to be flown may be inoperative.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
56XCOMPEU-01-00
34-20
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-52-01-01-20
CESSNA AIRCRAFT COMPANY
MODEL 560XL
SSR Transponder Mode A/C Functions
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.
NOTE: Mode C function is required to be operative for RVSM operations.
OPERATIONAL PROCEDURE
1. Flight crew shall contact the appropriate ATC facilities having jurisdiction over the
planned route of flight and coordinate operations as required.
2. Make sure the affected system is turned OFF.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
34-52-01-02-10
SSR Transponder Mode S Functions
D/-/0
Any in excess of those required for the intended route, may be inoperative.
NOTE: A SSR transponder with an operative Mode S function is defined as a
transponder which can provide, at least, Elementary Surveillance
capability.
PLACARDING PROCEDURE
Place a placard stating “XPNDR INOP” on the affected system.
56XCOMPEU-01-00
34-21
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-52-01-02-20
CESSNA AIRCRAFT COMPANY
MODEL 560XL
SSR Transponder Mode S Functions
C/-/0
One or more may be inoperative provided permission is obtained from the Air Navigation
Service Provider(s) when required for the intended route.
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.
PLACARDING PROCEDURE
Place a placard stating “XPNDR INOP” on the affected system.
34-52-01-03-10
SSR Transponder Mode Enhanced Surveillance Functions (If
installed)
D/-/0
One or more Downlinked Aeroplane Parameters (DAP’s), which provide Enhanced
Surveillance, may be inoperative when not required for the intended route.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
34-52-01-03-20
SSR Transponder Mode Enhanced Surveillance Functions (If
installed)
OPERATIONAL PROCEDURE
Flight crew shall contact the appropriate ATC facilities having jurisdiction over the
planned route of flight and coordinate operations as required.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
56XCOMPEU-01-00
34-22
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-55-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Automatic Direction Finding (ADF) System
D/-/Any in excess of those required by regulations may be inoperative.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
34-57-01
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.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
34-60-01
Flight Management System (FMS)
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.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
56XCOMPEU-01-00
34-23
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-60-01-01-10
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flight Management System (FMS) Navigation Databases
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.
OPERATIONAL PROCEDURE
1. A crew member shall verify the type, suitability, and operational status of each
Navigational Facility to be used during route of flight, either by a current
Aeronautical Chart, Airport Facility Directory or verbally with the appropriate
personnel.
2. Once tuned, each navigational facility shall be identified using the audible signal
transmitted by the facility.
PLACARDING PROCEDURE
Place a placard stating “NAVIGATION DATABASE IS NOT CURRENT” adjacent to FMS
CDU Controller.
34-60-01-01-20
Flight Management System (FMS) Navigation Databases
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.
PLACARDING PROCEDURE
Place a placard stating “NAVIGATION DATABASE IS NOT CURRENT” adjacent to FMS
CDU Controller.
56XCOMPEU-01-00
34-24
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-60-01-01-30
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flight Management System (FMS) Navigation Databases
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.
OPERATIONAL PROCEDURE
1. A crew member shall verify the type, suitability, and operational status of each
Navigational Facility to be used during route of flight, either by a current
Aeronautical Chart, Airport Facility Directory or verbally with the appropriate
personnel.
2. Once tuned, each navigational facility shall be identified using the audible signal
transmitted by the facility.
PLACARDING PROCEDURE
Place a placard stating “NAVIGATION DATABASE IS NOT CURRENT” adjacent to FMS
CDU Controller.
56XCOMPEU-01-00
34-25
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
34-60-01-01-40
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Flight Management System (FMS) Navigation Databases
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.
OPERATIONAL PROCEDURE
1. A crew member shall verify the type, suitability, and operational status of each
Navigational Facility to be used during route of flight, either by a current
Aeronautical Chart, Airport Facility Directory or verbally with the appropriate
personnel.
2. Once tuned, each navigational facility shall be identified using the audible signal
transmitted by the facility.
PLACARDING PROCEDURE
Place a placard stating “NAVIGATION DATABASE IS NOT CURRENT” adjacent to FMS
CDU Controller.
34-60-01-02
Flight Management System (FMS) Fuel Planning and Indication
Function
C/-/May be inoperative provided fuel flow indicating systems are operative.
PLACARDING PROCEDURE
Place a placard stating “FUEL PLAN INOP” adjacent to the affected FMS.
56XCOMPEU-01-00
34-26
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
35-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Oxygen Tank Fill Port
C/-/0
(M) May be inoperative provided bottle is filled using alternate means, if service is
required.
MAINTENANCE PROCEDURE
WARNING:
While oxygen supports combustion, materials that will not normally
do not flash in the atmosphere will readily burn or explode in the
presence of concentrated oxygen.
WARNING;
Do not permit Smoking; open flame or potential sources of electrical
sparks should not be permitted near the airplane while maintenance
is being performed on the oxygen system. Make sure that all
electrical power is disconnected and that the airplane is properly
grounded.
WARNING:
Use extreme caution to make sure that all components are kept
thoroughly clean of oil, grease or solvent contamination. These or
similar products may explode or burn spontaneously when in
contact with pure oxygen.
1. Access the oxygen bottle cylinder, cut safety wire on bottle neck valve, and turn
oxygen bottle OFF.
2. Slowly disconnect line from fill port to bottle at bottle neck and purge line of any
oxygen.
3. Cap and/or plug any open lines.
4. Connect Oxygen cart hose to oxygen bottle ensuring a proper connection.
5. Station an additional qualified person in the copilot’s seat with the foul weather
window open for clear communications.
6. Turn Oxygen bottle ON and slowly begin to fill bottle. Once bottle has reached
the proper servicing pressure, turn Oxygen bottle valve OFF and turn OFF
oxygen cart. Allow the bottle to cool from thermal expansion for 30 minutes and
recheck servicing pressure.
7. Once Oxygen bottle is properly serviced, slowly disconnect oxygen cart and reconnect all oxygen lines.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the fill port.
56XCOMPEU-01-00
35-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
35-00-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Oxygen Servicing Panel Pressure Gauge (If installed)
C/-/0
(M) May be inoperative provided alternate procedures are used for servicing oxygen
system.
MAINTENANCE PROCEDURE
1. Station an additional qualified person in the copilot’s seat with the foul weather
window open for clear communications.
2. Service the oxygen system to appropriate pressure while personnel inside
Aeroplane monitors pressure gauge.
3. When the oxygen pressure reaches the desired quantity, stop the flow of oxygen
and allow the bottle to cool.
4. Recheck oxygen pressure and finish servicing to desired pressure.
PLACARDING PROCEDURE
Place an INOP placard on affect gauge.
35-00-03
Blowout Disc/Green Label
C/1/0
(O) May be missing or damaged provided oxygen pressure is verified prior to each flight.
OPERATIONAL PROCEDURE
1. During the EXTERIOR PREFLIGHT INSPECTION, the plastic oxygen blowout
disc must be verified installed.
2. The oxygen system pressure gauge(s) will be inspected to verify proper oxygen
system servicing.
PLACARDING PROCEDURE
1. Place a placard stating, “GREEN O2 LABEL MISSING/INOP” adjacent to the
oxygen system blowout disc.
2. Place a placard stating, “GREEN O2 LABEL MISSING/INOP” on the instrument
panel in view of the flight crew.
56XCOMPEU-01-00
35-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
35-10-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
1. During the COCKPIT/CABIN PREFLIGHT INSPECTION the affected oxygen
mask shall be tested for proper oxygen delivery.
2. Repack the affected oxygen mask as appropriate.
PLACARDING PROCEDURE
Place a placard stating “TENSION CONTROL INOP” on the affected mask holder.
35-20-01
Passenger Oxygen System
C/1/0
May be inoperative provided:
a) Aeroplane is operated without cabin occupants, and
b) Crew oxygen system is operative.
PLACARDING PROCEDURE
Place a placard stating “PAX O2 INOP” adjacent to the oxygen controls.
35-20-01-01
Passenger Oxygen System Mask
B/-/0
Individual oxygen masks or dispensers may be inoperative or missing provided
associated seats are placarded “DO NOT OCCUPY”.
PLACARDING PROCEDURE
1. Place a placard stating “(AFFECTED SYSTEM) INOP” adjacent to the affected
equipment.
2. Place a placard stating “DO NOT OCCUPY” across the seat(s) adjacent to the
affected equipment.
56XCOMPEU-01-00
35-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
35-20-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Passenger Oxygen System Drop Out Panel
C/-/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”.
MAINTENANCE PROCEDURE
1. Untie the drop out panel and stow.
2. Using the most current revision to the vendor documents, remove the affected
oxygen masks and stow.
PLACARDING PROCEDURE
1. Place a placard stating, “DROP OUT PANEL INOP” adjacent to the affected
equipment.
2. Place a placard stating, “DO NOT OCCUPY” adjacent to the affected seat.
56XCOMPEU-01-00
35-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
35-30-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Protective Breathing Equipment (PBE) (If installed) installed)
D/-/0
(M) (O) Any in excess of those required may be inoperative or missing provided:
a) Required distribution of operative unit is maintained throughout the aircraft,
b) The inoperative PBE and its location are placarded inoperative, removed from
the aerocraft 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 which cannot be stowed in an approve stowage is subject
to the requirements of the International Civil Aviation Organization’s
Technical Instructions for the Safe Transport of Dangerous Goods by
Air.
MAINTENANCE PROCEDURE
NOTE:
Any equipment considered as hazardous material shall be removed
from the aircraft.
1. Remove the affected equipment from its storage location.
2. Tag it as an unserviceable unit and place it so that it cannot be mistaken for a
serviceable unit. If the unserviceable unit cannot be left at the location the
discrepancy was noted, make sure all applicable storage/transportation concerns
are addressed prior to aerocraft operation.
3. If required, install a serviceable unit back at the affect location.
OPERATIONAL PROCEDURE
Prior to flight, the flight crew shall brief on any emergency concerns associated with
operation of an inoperative or missing PBE unit.
PLACARDING PROCEDURE
Place an INOP placard on the affected equipment if left in the aircraft. If equipment is
to be removed from the aircraft, place a placard stating, “PBE MISSING” on the access
door/panel/stowage location.
56XCOMPEU-01-00
35-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
35-30-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
PLACARDING PROCEDURE
Place an INOP placard on the affected equipment if left in the Aeroplane. If equipment is
to be removed from the Aeroplane, place a placard stating “PORTABLE O2 MISSING”
on the access door/panel/stowage location.
56XCOMPEU-01-00
35-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
38-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Overboard Drain
C/-/(M) May be inoperative provided the system associated with the drain has been drained
and deactivated.
MAINTENANCE PROCEDURE
1. Remove any liquids or solids from associated storage compartment(s) and make
sure system(s) is completely drained.
2. Pull and secure appropriate circuit breaker for affected system(s).
PLACARDING PROCEDURE
Place an INOP placard adjacent to the affected drain.
38-10-01-01
Potable Water Systems
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.
MAINTENANCE PROCEDURE
NOTE: Refer to the appropriate Cessna Maintenance Manual and/or Interiors
Manual for information of the individual Aeroplane installation.
1. Pull and secure water heater circuit breaker. For lower vanity tank with pump,
pull and secure the drawer lights/water circuit breaker located on the interior
electrical panel in the vanity.
2. Open/remove access panels from lower vanity or upper LH bulkhead closet as
needed to access tank.
3. Remove quick-disconnect fitting.
4. Remove canister and inspect for leaks and/or dampness. Empty canister if
necessary.
5. Tape over canister lid and install placard on tank stating “DO NOT SERVICE”.
6. Re-install canister and access panels.
PLACARDING PROCEDURE
Place an INOP placard near inoperative water system (faucet or spigot).
56XCOMPEU-01-00
38-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
38-10-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Potable Water Systems
C/-/(M) May be inoperative provided:
a) System is drained, and
b) Procedures are established to ensure system is not serviced.
MAINTENANCE PROCEDURE
NOTE: Refer to the appropriate Cessna Maintenance Manual and/or Interiors
Manual for information of the individual Aeroplane installation.
For Aft Vanity Water Storage Tank:
1. Pull and secure water heater circuit breaker. For lower vanity tank with pump,
pull and secure the drawer lights/water circuit breaker located on the interior
electrical panel in the vanity.
2. Open/remove access panels from lower vanity or upper LH bulkhead closet as
needed to access tank.
3. Remove quick-disconnect fitting.
4. Remove canister and inspect for leaks and/or dampness. Empty canister if
necessary.
5. Tape over canister lid and install placard on tank stating “DO NOT SERVICE”.
6. Re-install canister and access panels.
For Refreshment Center Liquid Storage Tanks:
1.
2.
3.
4.
Remove access panels from refreshment center as needed to access tank.
Slide tank out of its compartment, disconnect, and cap any electrical connectors.
Inspect tank and plumbing for leaks and dampness.
Replace tank without reconnecting any disconnected electrical or plumbing
connections.
5. Reinstall access panels.
PLACARDING PROCEDURE
Place an INOP placard near inoperative water system (faucet or spigot).
56XCOMPEU-01-00
38-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
38-30-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Lavatory Waste Systems
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.
MAINTENANCE PROCEDURE
1. Clean all components with disinfectant.
2. Prior to Aeroplane boarding, crew shall advise all passengers on the operational
status of the toilet.
For Flushing Toilet Internally Serviced:
1. Lift seat assembly or remove access cover to gain access to wiring.
2. Disconnect flush switch from toilet.
3. Insulate and label all exposed wires to prevent any shorts and to facilitate future
re-connection.
4. Visually inspect tank and reservoir for any leaks. Correct any leaks prior to flight.
For Externally Serviceable Toilets:
1. Gain access to the interior junction box through the aft bulkhead closet. Remove
junction box cover and disengage circuit breaker CB144V TOILET.
2. To check for leaks:
a. Remove toilet seat back and pad.
b. Raise toilet seat and remove screws.
c. Remove toilet cabinet top by removing screws and disconnecting flush
switch connector.
d. Check all hoses, connections, and general area for leaks.
e. Any leaked fluid must be removed from Aeroplane. If tank will not hold
fluid, go to step 6.
f. If desired, flush toilet manually as follows:
g. Observe fluid level under rubber flapper at bottom of bowl. If tank is full,
drain it using appropriate ground service procedure following the
instructions on toilet service placard on external toilet service door.
h. With toilet tank empty, pour two (2) gallons of toilet service solution into
toilet bowl.
i. If desired, service toilet using appropriate ground servicing procedure
following the instructions on toilet service placard on external toilet
service door.
Continued Next Page
56XCOMPEU-01-00
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Continued
3. Following servicing or flushing, re-inspect toilet system for leaks. If toilet drains
into drain line, leave tank empty and perform the followings steps:
i. Empty drain line into servicing cart to prevent damage from
freezing.
ii. Adjust Weight and Balance for missing fluid,
iii. Soft ballast such as lead shot bags can be placed in toilet bowl (in
a sturdy, sealed plastic bag, if possible). Other ballast options
include placing ballast in vanity cabinets distributing weight
appropriately.
4. Re-install toilet seat, cabinet cover, and upholstery.
5. Cover toilet seat and placard INOP
Service Instructions with an Inoperative Toilet Servicing System
(i.e., liquid level sensor, fill valve, frozen fill line, etc.):
1.
2.
3.
4.
5.
Pull and secure TOILET circuit breaker in Interior Electrical J-Box.
Remove toilet seat back and seat pad.
Raise toilet seat and remove screws.
Any leaked fluid must be removed. If tank will not hold fluid:
Following servicing or flushing, re-inspect toilet system for leaks. If toilet drains
into drain line, leave tank empty and perform the followings steps:
6. Empty drain line into servicing cart to prevent damage from freezing.
7. Adjust Weight and Balance for missing fluid
8. Re-install toilet seat, cabinet cover and upholstery.
9. If desired, service toilet using appropriate ground servicing procedure following
the instructions on toilet service placard on external toilet service door.
10. Do not re-fill tank from servicing cart.
11. Following any re-servicing, follow steps 4 thru 8 above
Lavatory Fluid (max capacity = 4.0 gallons)
Charge
Weight
Center of Gravity
1 gal
10.41 lbs
357.40 in
2 gal
20.82 lbs
357.40 in
3 gal
31.23 lbs
357.40 in
4 gal
41.65 lbs
357.40 in
PLACARDING PROCEDURE
Moment
3720.5 in-lbs
7441.1 in-lbs
11161.6 in-lbs
14885.7 in-lbs
1. Cover toilet or relief tube as appropriate and placard INOP.
2. Place a placard stating “DO NOT SERVICE” adjacent to toilet servicing
connectors inside toilet service door.
56XCOMPEU-01-00
38-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
45-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Maintenance Diagnostic Computer (MDC) System (Units 6001 and
on)
C/1/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place an INOP placard on the affected system.
56XCOMPEU-01-00
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
45-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
46-00-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Electronic Flight Bag (EFB) System (If installed) Class 3 EFBs
Integrated Flight Information System (IFIS) (Units 6001 and on)
Advanced File Graphics Server(Units 5501 – 6000)
C/-/(O) May be inoperative provided alternate procedures are established and used.
NOTE: Any function, program or document which operates normally may be
used.
OPERATIONAL PROCEDURE
1. A member of the flight crew shall make sure the appropriate navigational
products (approach plates, VFR/IFR maps, AFDs, etc.) are available in the
Aeroplane for the intended flight.
2. If the affected equipment can be operated on an independent battery supply,
make sure that available batteries are fully charged and available for the flight
intended and possible extended flight to alternates.
PLACARDING PROCEDURE
1. Place an INOP placard on the affected equipment if left in the Aeroplane.
2. If equipment is to be removed from the Aeroplane, place a placard stating “EFB
MISSING” on the access door/panel/stowage location.
46-00-01-02
Electronic Flight Bag (EFB) System (If installed) Data Connectivity
(Class 2)
C/-/(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE
1. Prior to each takeoff, a crew member will ensure that the battery installed in EFB
and back up battery has sufficient charge for intended usage during flight.
2. If sufficient battery charge cannot be determined, appropriate and current
navigational publications for route of flight and alternates must be carried
onboard.
PLACARDING PROCEDURE
Place an INOP placard on the affected equipment.
56XCOMPEU-01-00
46-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
46-00-01-03
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Electronic Flight Bag (EFB) System (If installed) Power
Connection(Class 1 & 2)
C/-/(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE
1. Prior to each takeoff, a crew member will ensure that the battery installed in EFB
and back up battery has sufficient charge for intended usage during flight.
2. If sufficient battery charge cannot be determined, appropriate and current
navigational publications for route of flight and alternates must be carried
onboard.
PLACARDING PROCEDURE
Place an INOP placard on the affected equipment.
46-00-01-04
Electronic Flight Bag (EFB) System (If installed) Mounting Device
(Class 2)
C/-/0
(M) (O) May be inoperative provided:
a) Associated EFB and hardware is secured by an alternate means or removed
from the aircraft, and
b) Alternate procedures are established and used.
MAINTENANCE PROCEDURE
1. If able, remove the affected mounting devise from its location.
2. Secure any loose connectors and/or attachments.
3. If the affected EFB system does not have an internal source of power and is not
operative, store it so it cannot be mistaken for a functional unit.
OPERATIONAL PROCEDURE
1. The affected flight crew member(s) will determine an adequate storage location
for the EFB(s) prior to flight.
2. The flight crew will brief on alternate EFB usage for the intended flight.
PLACARDING PROCEDURE
Place an INOP placard over the affected mounting location.
56XCOMPEU-01-00
46-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
46-00-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Electronic Checklist System (If installed)
D/-/0
May be inoperative provided equivalent checklist is available.
PLACARDING PROCEDURE:
1. Make sure the appropriate aerocraft checklist is in the aerocraft and available to
the flight crew.
2. Place a placard stating, “CHECKLIST INOP” adjacent to the affected checklist
control system.
46-00-04-01
Dedicated EFB Power Connection (does not include AC Cockpit
Outlet) (If installed)
C/-/0
(O) May be inoperative provided alternate procedures are established and used.
OPERATIONAL PROCEDURE
1. If appropriate, use a power source in the cockpit to power the EFB. This can
include, but is not limited to, the AC outlet in the Jepp case (if installed).
2. Prior to each takeoff, a crew member shall ensure that the battery installed in
EFB and back up battery has sufficient charge for intended usage during flight.
3. If sufficient battery charge cannot be determined, appropriate and current
navigational publications for route of flight and alternates shall be carried
onboard.
4. Cover the affected power outlet so that it cannot be mistaken for a functional
item.
PLACARDING PROCEDURE
Place a placard stating “EFB POWER OUTLET INOP” adjacent to the base of the
affected outlet.
56XCOMPEU-01-00
46-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
46-00-04-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Dedicated EFB Power Connection (does not include AC Cockpit
Outlet) (If installed)
D/-/0
May be inoperative provided procedures do not require its use.
PLACARDING PROCEDURE
Place a placard stating “EFB POWER OUTLET INOP” adjacent to the base of the
affected outlet.
56XCOMPEU-01-00
46-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
49-20-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
Pull and secure MASTER APU circuit breaker.
PLACARDING PROCEDURE
Place an INOP placard on APU panel.
56XCOMPEU-01-00
49-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
49-30-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
MAINTENANCE PROCEDURE
NOTE: It is not possible to secure the shutoff valve OPEN or CLOSED. If the APU
starts, the valve has not failed CLOSED. If the APU will not shutdown,
then both this valve, and the valve downstream of the FCU are failed
OPEN. Two procedures are offered. One to electrically prevent the valve
from opening and one to check for fuel flow through the valve.
1.
2.
3.
4.
5.
Pull and secure MASTER APU circuit breaker.
Station an additional technician outside of Aeroplane at empennage.
Select BATT switch to ON.
Select FUEL BOOST R ON.
After 3 minutes, have technician inspect APU drain line and inspection panels
between flaps for evidence of fuel. Fuel exiting the drain line indicates the fuel
shutoff valve and APU fuel solenoid valves are OPEN. Fuel dripping from wing
center section and/or empennage belly indicates a leak possibly at the shutoff
valve. Either condition must be corrected prior to dispatch. If no fuel leaks/drips
are found, procedure is complete.
6. Select FUEL BOOST R to OFF.
7. Select BATT to OFF.
Alternate Procedure to make sure Valve is Failed CLOSED
1. Electrically ground Aeroplane prior to performing this procedure and keep all
sources of ignition away from Aeroplane.
2. Locate and remove appropriate access panel to access fuel shutoff valve.
3. Disconnect APU fuel line from output of shutoff valve. Use an appropriate
container to catch fuel from line.
4. Station additional technician in pilot seat.
5. Select BATT switch to ON.
6. Select FUEL BOOST R to ON for approximately 5 seconds and select switch to
OFF.
7. Select BATT switch to OFF.
8. If no fuel flows from line, fuel shutoff valve is failed CLOSED.
9. Re-connect fuel line and re-install access panels.
10. Pull and secure MASTER APU circuit breaker.
PLACARDING PROCEDURE
Place an INOP placard on APU panel.
56XCOMPEU-01-00
49-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
49-50-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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.
OPERATIONAL PROCEDURE
1. Position Aeroplane in a suitable run-up area and chock both main landing gear.
2. Using AFM Normal Procedures, start the APU.
3. On the APU panel, turn the BLEED AIR switch to ON and verify no airflow in
cabin.
4. Turn BLEED AIR switch to OFF.
5. If desired, power down APU.
PLACARDING PROCEDURE
Place an INOP placard above the APU BLEED AIR switch.
56XCOMPEU-01-00
49-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
49-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
52-00-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cockpit Divider Door/Curtain Divider Door
C/2/0
May be inoperative provided door remains secured open.
PLACARDING PROCEDURE
1. Make sure the divider door is secured in the placarded taxi, takeoff, and landing
configuration. One method of securing would be to tape the door in the
appropriate position using caution not to damage the interior finish.
2. Place a placard stating “(AFFECTED SIDE) DOOR INOP” on the divider wall in
view of all Aeroplane occupants.
52-00-01-02
Cockpit Divider Door/Curtain - Curtain
C/2/0
May be missing or inoperative provided curtain remains secured open.
PLACARDING PROCEDURE
1. Make sure the divider door is secured in the placarded taxi, takeoff, and landing
configuration. One method of securing would be to tape the curtain in the
appropriate position using caution not to damage the interior finish.
2. Place a placard stating “(AFFECTED SIDE) CURTAIN INOP” on the divider wall
in view of all Aeroplane occupants.
52-10-01-01
Cabin Door Primary Seal (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) Aerocraft is operated at FL 250 or below.
OPERATIONAL PROCEDURE:
1. Position aerocraft in a suitable run-up area and chock main landing gear.
2. Station additional technicians inside and outside of cabin door. Ensure
appropriate personal safety equipment is used and all personnel are briefed of
hazards of working with an operating engine.
3. Using AFM Normal Procedures, start Right Engine or APU if equipped.
4. With cabin door OPEN locate the lower aft door pin receptacle and depress the
door seal inflation valve inside receptacle. Allow seal to fully inflate and release
inflation valve.
5. Close and latch cabin door and verify no interference from any door seal.
6. Using AFM Normal Procedures, power down aircraft.
PLACARDING PROCEDURE:
Place a placard stating, “CABIN DOOR PRIMARY SEAL INOP” adjacent to door handle.
56XCOMPEU-01-00
52-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
52-10-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Door Primary Seal (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.
OPERATIONAL PROCEDURE:
1. Flight planning must consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning must consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s must be taken into account for planned route.
4. Select Cabin EMER DUMP ON.
5. Set Cabin Altitude to 14,000 feet.
PLACARDING PROCEDURE:
Place a placard stating, “CABIN DOOR PRIMARY SEAL INOP” above pressurization
controls.
52-10-02-01
Cabin Door Secondary Seal (Pressurized)
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) Aerocraft is operated at FL 250 or below.
OPERATIONAL PROCEDURE:
1. Position aerocraft in a suitable run-up area and chock main landing gear.
2. Station additional technicians inside and outside of cabin door. Ensure
appropriate personal safety equipment is used and all personnel are briefed of
hazards of working with an operating engine.
3. Using AFM Normal Procedures, start Right Engine or APU if equipped.
4. With cabin door OPEN locate the lower aft door pin receptacle and depress the
door seal inflation valve inside receptacle. Allow seal to fully inflate and release
inflation valve.
5. Close and latch cabin door and verify no interference from any door seal.
6. Using AFM Normal Procedures, power down aircraft.
PLACARDING PROCEDURE:
Place a placard stating, “CABIN DOOR SECONDARY SEAL INOP” adjacent to door
handle.
56XCOMPEU-01-00
52-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
52-10-02-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Door Secondary Seal (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.
OPERATIONAL PROCEDURE:
1. Flight planning must consider the fuel burn associated with flight at lower altitude
and affect on range.
2. Flight planning must consider oxygen requirements associated with operating
regulations and altitudes.
3. MEA’s must be taken into account for planned route.
4. Select Cabin EMER DUMP ON.
5. Set Cabin Altitude to 14,000 feet.
6. Flight planning must consider the fuel burn associated with flight at lower altitude
and affect on range.
7. Flight planning must consider oxygen requirements associated with operating
regulations and altitudes.
8. MEA’s must be taken into account for planned route.
9. Select Cabin EMER DUMP ON.
10. Set Cabin Altitude to 14,000 feet.
PLACARDING PROCEDURE:
Place a placard stating, “CABIN DOOR SECONDARY SEAL INOP” above
pressurization controls.
52-10-03
Cabin Door Acoustic Seal
C/1/0
PLACARDING PROCEDURE
Place a placard stating “ACOUSTIC SEAL INOP” on the door frame inside the cabin.
56XCOMPEU-01-00
52-3
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
52-10-04
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Cabin Door Key Lock
D/1/0
May be inoperative in the unlocked position.
PLACARDING PROCEDURE
Place a placard stating “CABIN DOOR LOCK INOP” on the door frame inside the cabin
door.
52-10-05
Cabin Vent Door
C/1/0
(O) May be inoperative provided vent door is manually closed using appropriate AFM
procedure prior to each flight.
OPERATIONAL PROCEDURE
1. Once the Aeroplane has been boarded, a crew member shall close and latch
cabin door.
2. Verify all green door pin flags are visible.
3. Locate an unscrew cabin vent door access cover on aft side of cabin door
steps.
4. Depress cabin vent door lever to make sure vent door is CLOSED.
5. Replace vent door cover.
PLACARDING PROCEDURE
Place a placard stating “CABIN VENT DOOR INOP” on cabin steps.
52-30-01
Baggage Compartment Door Key Lock
D/1/0
May be inoperative in the unlocked position.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the key lock.
52-40-01
Left Nose Avionics Compartment Key Lock
D/1/0
May be inoperative in the unlocked position.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the key lock.
56XCOMPEU-01-00
52-4
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
52-40-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Right Nose Avionics Compartment Key Lock
D/1/0
May be inoperative in the unlocked position.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the key lock.
52-40-03
Tailcone Maintenance Access Door Key Lock
D/1/0
May be inoperative in the unlocked position.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the key lock.
52-42-01
Battery Compartment Door Key Lock for 560-5001 thru 5187, which
do not have SB560XL-52-09 incorporated.
D/1/0
May be inoperative in the unlocked position.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the key lock.
52-46-01-01
Single Point Refueling System Door Key Lock
D/1/0
May be inoperative in the unlocked position.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the key lock.
52-46-01-02
Single Point Refueling System Door Key Lock
D/1/0
May be inoperative in the locked position provided over wing refueling cap locks are not
failed in locked position.
PLACARDING PROCEDURE
Place an INOP placard adjacent to the key lock.
56XCOMPEU-01-00
52-5
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
52-6
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
73-30-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Fuel Flow Indicating System
A/2/1
One may be inoperative provided repairs are made within three flight days.
PLACARDING PROCEDURE
For Units 5001-6000:
Place an INOP placard over the affected indicating display.
For Units 6001 and on:
Place a placard stating “(AFFECTED SIDE) FUEL FLOW INOP” above the MFD.
56XCOMPEU-01-00
73-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
73-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
76-00-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Electronic Engine Control (EEC) (units 5001-6000)
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.
OPERATIONAL PROCEDURE
NOTE: In order to avoid a significant throttle split, both engines shall be started
in MANUAL when dispatching with an inoperative EEC AUTO mode.
Selecting MANUAL following failure of AUTO mode on one side, on the
ground while the engines are running will result in a significant throttle
split.
1. Prior to engine start, select EEC L/R switched to MANUAL.
2. Flight crew shall use the appropriate performance tables from the appropriate
AFM Supplement to make sure all takeoff and landing requirements are met.
3. Flight crew shall review AFM Normal and Abnormal Procedures in the
appropriate AFM Supplement during preflight briefing.
PLACARDING PROCEDURE
Place a placard stating “EEC AUTO MODE INOP” above EEC switches.
76-01-01
Engine Synchronizer System
C/1/0
May be inoperative failed off.
PLACARDING PROCEDURE
Place a placard stating “ENG SYNC INOP” adjacent to the engine sync controls.
56XCOMPEU-01-00
76-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Page Intentionally Left Blank
56XCOMPEU-01-00
76-2
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
77-14-01-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
N1 Indicators 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.
PLACARDING PROCEDURE
Place an INOP placard over the affected N1 display.
56XCOMPEU-01-00
77-1
MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
77-14-01-02
CESSNA AIRCRAFT COMPANY
MODEL 560XL
N1 Indicators 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.
PLACARDING PROCEDURE
Place an INOP placard over the affected N1 display.
77-32-01
Engine Vibration Monitor System
B/21/
One may be inoperative provided no abnormal vibration exists.
NOTE: White ENG VIB annunciator/CAS message may be annunciated/displayed.
MAINTENANCE PROCEDURE
Pull and secure ENG VIB MON circuit breaker on affected side.
PLACARDING PROCEDURE
Place a placard stating “(AFFECTED SIDE) ENG VIB MON INOP” on the instrument
panel in view of flight crew.
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
78-30-01
CESSNA AIRCRAFT COMPANY
MODEL 560XL
Thrust Reverser
C/2/0
(M) May be inoperative provided affected thrust reverser is secured in the forward thrust
position.
MAINTENANCE PROCEDURE:
Using the most current revision to the 560XL Maintenance Manual, section 78-31-00 –
THRUST REVERSER SYSTEM – SERVICING, perform the thrust reverser lockout
procedure for the affected thrust reverser.
OPERATIONAL PROCEDURE:
1. During flight planning, the flight crew will make sure adequate takeoff and landing
distances without the use of thrust reversers.
2. Flight crew will brief on the use of braking at all intended takeoff and landing
locations.
PLACARDING PROCEDURE:
1. Place a placard stating, “THRUST REVERSER INOP” on the appropriate thrust
reverser throttle quadrant lever.
2. Place an INOP placard on the affected thrust reverser annunciator.
3. Place a placard stating, “THRUST REV INOP” on the instrument panel in view of
the flight crew.
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MASTER MINIMUM EQUIPMENT LIST
OPERATIONAL AND MAINTENANCE PROCEDURES
CESSNA AIRCRAFT COMPANY
MODEL 560XL
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