CE-560XL
XLS+
Rev. 1.0
MEMORY FLASH CARDS
Copyright © 2014, FlightSafety International, Inc.
Unauthorized reproduction or distribution is prohibited. All rights reserved.
INSERT LATEST REVISED CARDS, DESTROY SUPERSEDED CARDS
LIST OF EFFECTIVE CARDS
ORIGINAL.................. 0................ AUG. 2008
REVISION.............. .01.................OCT. 2010
REVISION ..............0.2 ................OCT. 2010
REVISION................0.3................ AUG. 2012
REVISION................1.0................ JUN. 2014
Incorporates AFM Rev. 2 ......... 8 JAN. 2014
TOTAL NUMBER OF CARDS IN THIS SET IS 56
CONSISTING OF THE FOLLOWING:
*Revision
Card
No.
No.
Card
No.
Title........................................................
ii.............................................................
WA-1 – WA-7A......................................
E-1 – E-13A...........................................
L-1 – L-35A............................................
*Revision
No.
1.0
1.0
1.0
1.0
1.0
*Zero in this column indicates an original card.
Revision 1.0
FOR TRAINING PURPOSES ONLY
ii
Warning Annunciator
APU FIRE
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-1
APU FIRE
1. APU FIRE Button ................................................................... Push
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-1A
Warning Annunciator
BATTERY OVERTEMP >145 or >160
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-2
BATTERY OVERTEMP >145 or >160
1. Amperage ............................................................................... Note
2. NORM/EMER Button ............................................................ EMER
3. Amperage .............................................................. Note Decrease
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-2A
Warning Annunciator
CABIN ALTITUDE
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-3
CABIN ALTITUDE
1. Oxygen Masks ...................................................... DON and 100%
2. MIC SEL Buttons ................................................................. MASK
3. Emergency Descent .................................................. As Required
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-3A
Warning Annunciator
EMERGENCY DESCENT
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-4
EMERGENCY DESCENT
1. Initiate maximum rate of descent to a safe altitude.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-4A
Warning Annunciator
ENGINE FIRE L and/or R
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-5
ENGINE FIRE L and/or R
1. Throttle (affected side) ............................................................ IDLE
• If ENG FIRE Light Remains On
2. ENG FIRE Button (affected side) ................................... Push
3. Illuminated BOTTLE ARMED Button (either side) ......... Push
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-5A
Warning Annunciator
NO TAKEOFF
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-6
NO TAKEOFF
1. Takeoff ................................................................................... Abort
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-6A
Warning Annunciator
WINDSHEAR
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-7
WINDSHEAR
1. Immediately execute a maximum performance escape maneuver.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
WA-7A
Emergency
ENGINE FAILURE OR OTHER
EMERGENCY DURING TAKEOFF
Speed Below V1
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-1
ENGINE FAILURE OR OTHER
EMERGENCY DURING TAKEOFF
Speed Below V1
1. Takeoff ................................................................................... Abort
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-1A
Emergency
ENGINE FAILURE OR OTHER
EMERGENCY DURING TAKEOFF
Speed At or Above V1
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-2
ENGINE FAILURE OR OTHER
EMERGENCY DURING TAKEOFF
Speed At or Above V1
1. Climb to a safe altitude.
2. WING XFLOW (if wing anti-ice is ON) ....................................... ON
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-2A
Emergency
DUAL ENGINE FAILURE
If Below FL300
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-3
DUAL ENGINE FAILURE
If Below FL300
1. FUEL BOOST Buttons (both) .................................................... ON
2. ANTI-ICE Switches (all) ........................................................... OFF
3. Throttles (both) ............................................. CUT OFF, then IDLE
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-3A
Emergency
ENVIRONMENTAL SYSTEM
SMOKE OR ODOR
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-4
ENVIRONMENTAL SYSTEM
SMOKE OR ODOR
1. Oxygen Masks ..................................................... DON and EMER
2. MIC SEL Buttons (both)....................................................... MASK
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-4A
Emergency
ELECTRICAL FIRE OR SMOKE
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-5
ELECTRICAL FIRE OR SMOKE
1. Oxygen Masks/Goggles ...................................... DON and EMER
2. MIC SEL Buttons ................................................................. MASK
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-5A
Emergency
SMOKE REMOVAL
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-6
SMOKE REMOVAL
1. Oxygen Masks/Goggles ...................................... DON and EMER
2. MIC SEL Buttons ................................................................. MASK
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-6A
Emergency
EMERGENCY DESCENT
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-7
EMERGENCY DESCENT
1. Initiate maximum rate of descent to a safe altitude.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-7A
Emergency
THRUST REVERSER IN-FLIGHT
DEPLOYMENT
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-8
THRUST REVERSER IN-FLIGHT
DEPLOYMENT
1.
2.
3.
4.
Control Wheel .......................................................................... Grip
AP TRIM DISC Button ........................................................... Push
EMER STOW Switch (affected side) ..................................... EMER
Airspeed ..................................... Decrease to 140 KIAS or below
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-8A
Emergency
WHEEL BRAKE FAILURE
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-9
WHEEL BRAKE FAILURE
1. Brake Pedals............................................................ Remove Feet
2. EMERGENCY BRAKE Handle .................................................. Pull
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-9A
Emergency
AUTOPILOT MALFUNCTION
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-10
AUTOPILOT MALFUNCTION
1. AP TRIM DISC Button .......................................................... PUSH
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-10A
Emergency
ELECTRIC ELEVATOR RUNAWAY TRIM
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-11
ELECTRIC ELEVATOR RUNAWAY TRIM
1. AP TRIM DISC Button ........................................ PUSH and HOLD
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-11A
Emergency
INADVERTENT STALL
(STICK SHAKER, BUFFET,
AND/OR ROLL-OFF)
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-12
INADVERTENT STALL
(STICK SHAKER, BUFFET,
AND/OR ROLL-OFF)
1.
2.
3.
4.
Autopilot ...................................................................... Disconnect
Pitch Attitude ..................................................................... Reduce
Roll Attitude ........................................................................... Level
Throttles ........................................................................ TO Detent
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-12A
Emergency
EMERGENCY EVACUATION
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-13
EMERGENCY EVACUATION
Parking Brake ........................................................................... Set
Throttles (both) ............................................................... CUT OFF
NORM/EMER Button ........................................................... NORM
LEFT/RIGHT ENG FIRE Buttons (both) ................................. Push
BOTTLE 1 and BOTTLE 2 ARMED Buttons
(if fire suspected) .................................................................... Push
6. APU MASTER Button .............................................................. OFF
7. BATT Button .................................................................. BATT OFF
1.
2.
3.
4.
5.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
E-13A
Limitations
WEIGHT LIMITATIONS
Maximum Design Ramp Weight .................................................. ?
Maximum Design Takeoff Weight ................................................ ?
Maximum Design Landing Weight ............................................... ?
Maximum Design Zero Fuel Weight ............................................ ?
Minimum Flight Weight ................................................................ ?
Maximum Tailcone Baggage Weight ........................................... ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-1
WEIGHT LIMITATIONS
Maximum Design Ramp Weight ........................... 20,400 Pounds
Maximum Design Takeoff Weight ......................... 20,200 Pounds
Maximum Design Landing Weight ........................ 18,700 Pounds
Maximum Design Zero Fuel Weight ..................... 15,100 Pounds
Minimum Flight Weight ......................................... 12,400 Pounds
Maximum Tailcone Baggage Weight ......................... 700 Pounds
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-1A
Limitations
GROUND OPERATION
Continuous engine ground static operation up to and including
minutes at takeoff thrust is limited to ambient temperatures not
to exceed the lesser of 30°C or ISA+35°C. Above 30°C but at or
below ISA+35°C, static operation is limited to minutes at takeoff
thrust.
Limit ground operation of pitot-static heat to minutes to
preclude system damage to the pitot tubes and angle-of-attack
vane.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-2
GROUND OPERATION
Continuous engine ground static operation up to and including 5
minutes at takeoff thrust is limited to ambient temperatures not
to exceed the lesser of 30°C or ISA+35°C. Above 30°C but at or
below ISA+35°C, static operation is limited to 4 minutes at takeoff
thrust.
Limit ground operation of pitot-static heat to 2 minutes to
preclude system damage to the pitot tubes and angle-of-attack
vane.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-2A
Limitations
GROUND OPERATION
Operation of the avionics GROUND DISPATCH power system is
limited to
minutes while on airplane battery power only (i.e. no
generator on-line or external power connected). Operation of the
GROUND DISPATCH power system is prohibited when OAT is
colder than
.
Electrical load is limited to
amps per generator during ground
operations (transients up to 250 amps are permissible for up to 4
minutes).
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-3
GROUND OPERATION
Operation of the avionics GROUND DISPATCH power system is
limited to 25 minutes while on airplane battery power only (i.e. no
generator on-line or external power connected). Operation of the
GROUND DISPATCH power system is prohibited when OAT is
colder than -33°C.
Electrical load is limited to 200 amps per generator during ground
operations (transients up to 250 amps are permissible for up to 4
minutes).
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-3A
Limitations
GROUND OPERATION
and
indications are not accurate without at least one
engine running.
Timing for avionics ambient temperature limit begins when all
avionics are powered .
Ground operations with avionics power on for longer than hours
at ambient temperatures over 37.8°C (100°F) will require the
windshield rain removal fan to be turned on.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-4
GROUND OPERATION
RAT and SAT indications are not accurate without at least one
engine running.
Timing for avionics ambient temperature limit begins when all
avionics are powered on.
Ground operations with avionics power on for longer than 3 hours
at ambient temperatures over 37.8°C (100°F) will require the
windshield rain removal fan to be turned on.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-4A
Limitations
SINGLE POINT REFUELING LIMITATION
Single point refueling operations must be accomplished per
the procedures contained on the placard installed on the
single point refueling access door. Refueling pressure range
is
to
PSI, maximum defueling pressure is -10 PSI.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-5
SINGLE POINT REFUELING LIMITATION
Single point refueling operations must be accomplished per
the procedures contained on the placard installed on the
single point refueling access door. Refueling pressure range
is 10 to 55 PSI, maximum defueling pressure is -10 PSI.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-5A
Limitations
FUEL LIMITATIONS
The fuel boost pumps must be turned on when the FUEL LEVEL
LOW message illuminates or at
pounds or less indicated fuel.
Maximum lateral fuel imbalance is
pounds. A lateral fuel
imbalance of 800 pounds has been demonstrated for emergency
return.
UNUSABLE FUEL
Fuel remaining in the fuel tanks when the fuel quantity indicator
reads
is not usable in flight.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-6
FUEL LIMITATIONS
The fuel boost pumps must be turned on when the FUEL LEVEL
LOW message illuminates or at 400 pounds or less indicated fuel.
Maximum lateral fuel imbalance is 400 pounds. A lateral fuel
imbalance of 800 pounds has been demonstrated for emergency
return.
UNUSABLE FUEL
Fuel remaining in the fuel tanks when the fuel quantity indicator
reads zero is not usable in flight.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-6A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum Altitude Limit ............................................................... ?
Maximum Tailwind Component ................................................... ?
Maximum Ambient Temperature ................................................. ?
The autopilot and yaw damper must be
landing.
for takeoff and
Maximum Tire Ground Speed ..................................................... ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-7
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum Altitude Limit .............................................. 14,000 Feet
Maximum Tailwind Component ...................................... 10 Knots
Maximum Ambient Temperature .................................. ISA +35°C
The autopilot and yaw damper must be OFF for takeoff and
landing.
Maximum Tire Ground Speed ...................................... 165 Knots
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-7A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
The lavatory doors must be latched
for takeoff and landing.
Takeoff and landings are limited to
runway surfaces.
Takeoff from a wet runway, when using thrust reversers for
performance credit, is limited to a minimum runway width of
feet.
Antiskid must be operational for
.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-8
TAKEOFF AND LANDING
OPERATIONAL LIMITS
The lavatory doors must be latched open for takeoff and landing.
Takeoff and landings are limited to paved runway surfaces.
Takeoff from a wet runway, when using thrust reversers for
performance credit, is limited to a minimum runway width of
75 feet.
Antiskid must be operational for takeoff.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-8A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Rudder bias and the rudder bias heater must be operational for
, and a satisfactory preflight test must be performed in
accordance with Section III, Normal Procedures.
Pulse lights must be turned off (lights not pulsing) below
AGL.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
feet
L-9
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Rudder bias and the rudder bias heater must be operational for
takeoff, and a satisfactory preflight test must be performed in
accordance with Section III, Normal Procedures.
Pulse lights must be turned off (lights not pulsing) below 300 feet
AGL.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-9A
Limitations
ENROUTE OPERATIONAL LIMITS
Maximum Operating Altitude ...................................................... ?
Maximum Altitude for Flaps and Landing
Gear Extended ....................................................................... ?
Generator Load ........................................................................... ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-10
ENROUTE OPERATIONAL LIMITS
Maximum Operating Altitude ..................................... 45,000 Feet
Maximum Altitude for Flaps and Landing
Gear Extended ...................................................... 18,000 Feet
Generator Load .............................................. 300 Amps in Flight
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-10A
Limitations
PASSENGER COMPARTMENT
For all taxi, takeoff, and landings: track seat fully outboard with control
lever inboard, armrests down, seat back upright, seat belts and
harnesses
, and headrest
. Maximum number of
passenger seats is 12. The lavatory door must be latched open for taxi,
takeoff, and landing.
COCKPIT SPEAKER MUTE SYSTEM
pilots must be using headsets when the overhead cockpit speaker
audio is muted.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-11
PASSENGER COMPARTMENT
For all taxi, takeoff, and landings: track seat fully outboard with control
lever inboard, armrests down, seat back upright, seat belts and
harnesses secured, and headrest extended. Maximum number of
passenger seats is 12. The lavatory door must be latched open for taxi,
takeoff, and landing.
COCKPIT SPEAKER MUTE SYSTEM
Both pilots must be using headsets when the overhead cockpit speaker
audio is muted.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-11A
Limitations
REDUCED VERTICAL
SEPARATION MINIMUM
AIRSPEED LIMITS
Minimum airspeed in RVSM airspace is
KIAS.
WEIGHT LIMITS
Minimum weight in RVSM airspace is
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
pounds.
L-12
REDUCED VERTICAL
SEPARATION MINIMUM
AIRSPEED LIMITS
Minimum airspeed in RVSM airspace is 160 KIAS.
WEIGHT LIMITS
Minimum weight in RVSM airspace is 14,000 pounds.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-12A
Limitations
APPROVED OILS
Maximum oil consumption is quart per 10-hour period. When oil
consumption is greater than quart per 10-hour period, refer to
the aircraft Maintenance Manual.
Oil types or brands may
be mixed unless specifically
approved in the PW545C Maintenance Manual.
Should oils of nonapproved brands or of different viscosities
become intermixed,
and
complete oil system and
refill with an approved oil in accordance with Engine Maintenance
Manual instructions.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-13
APPROVED OILS
Maximum oil consumption is 1 quart per 10-hour period. When oil
consumption is greater than 1 quart per 10-hour period, refer to
the aircraft Maintenance Manual.
Oil types or brands may not be mixed unless specifically
approved in the PW545C Maintenance Manual.
Should oils of nonapproved brands or of different viscosities
become intermixed, drain and flush complete oil system and
refill with an approved oil in accordance with Engine Maintenance
Manual instructions.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-13A
Limitations
SPEED LIMITS
Maximum Operating Limit Speeds:
MMO (Above 26,515 Feet) ...................................................... ?
VMO (Between 8000 and 26,515 Feet) ................................... ?
VMO (Below 8000 Feet) ........................................................... ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-14
SPEED LIMITS
Maximum Operating Limit Speeds:
MMO (Above 26,515 Feet) .................... 0.75 Mach (Indicated)
VMO (Between 8000 and 26,515 Feet) ...................... 305 KIAS
VMO (Below 8000 Feet) .............................................. 260 KIAS
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-14A
Limitations
SPEED LIMITS
Maximum Flap Extended Speed - VFE:
Full Flaps - 35° Position.......................................................... ?
Partial Flaps - 7° and 15° Position.......................................... ?
Maximum Landing Gear
Extended Speed - VLE ............................................................ ?
Operating Speed - VLO (Extending)......................................... ?
- VLO (Retracting)......................................... ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-15
SPEED LIMITS
Maximum Flap Extended Speed - VFE:
Full Flaps - 35° Position............................................. 175 KIAS
Partial Flaps - 7° and 15° Position............................. 200 KIAS
Maximum Landing Gear
Extended Speed - VLE ............................................... 250 KIAS
Operating Speed - VLO (Extending)............................ 250 KIAS
- VLO (Retracting)............................ 200 KIAS
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-15A
Limitations
SPEED LIMITS
Maximum Speedbrake Operation Speed - VSB .......................... ?
Autopilot Operation ..................................................................... ?
Minimum Speed for Sustained Flight in Icing Conditions
(except takeoff, approach and landing) ................................. ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-16
SPEED LIMITS
Maximum Speedbrake Operation Speed - VSB .............. No Limit
Autopilot Operation ................................. 305 KIAS or 0.75 Mach
Minimum Speed for Sustained Flight in Icing Conditions
(except takeoff, approach and landing) .................... 160 KIAS
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-16A
Limitations
OPERATIONS IN SEVERE
ICING CONDITIONS
During flight, severe icing conditions that exceed those for which the
airplane is certified shall be determined by the following visual cues:
1. Unusually extensive ice accumulation on the
and
in areas not normally observed to collect ice.
2. Accumulation of ice on the upper surface of the wing aft of the
to
inches aft of the
protected area extending more than
heated leading edge.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-17
OPERATIONS IN SEVERE
ICING CONDITIONS
During flight, severe icing conditions that exceed those for which the
airplane is certified shall be determined by the following visual cues:
1. Unusually extensive ice accumulation on the airframe and
windshield in areas not normally observed to collect ice.
2. Accumulation of ice on the upper surface of the wing aft of the
protected area extending more than 12 to 18 inches aft of the
heated leading edge.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-17A
Limitations
OPERATIONS AUTHORIZED
This airplane is approved for day and night, VFR, IFR flight and
flight into
icing conditions.
This airplane is not approved for
25.801.
under 14 CFR Part
MINIMUM CREW
Minimum Flight Crew for All Operations ...................................... ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-18
OPERATIONS AUTHORIZED
This airplane is approved for day and night, VFR, IFR flight and
flight into known icing conditions.
This airplane is not approved for ditching under 14 CFR Part
25.801.
MINIMUM CREW
Minimum Flight Crew for All Operations ...... 1 Pilot and 1 Copilot
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-18A
Limitations
BATTERY AND STARTER
CYCLE LIMITATIONS
Engine Starter .............
engine start cycles per 30 minutes
with a 90-second rest period between
cycles is permitted.
APU Starter .................
APU start cycles per 30 minutes
with a 90-second rest period between
cycles is permitted.
Battery ........................
battery start cycles per hour.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-19
BATTERY AND STARTER
CYCLE LIMITATIONS
Engine Starter ............. Three engine start cycles per 30 minutes
with a 90-second rest period between
cycles is permitted.
APU Starter ................. Three APU start cycles per 30 minutes
with a 90-second rest period between
cycles is permitted.
Battery ........................ Three battery start cycles per hour.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-19A
Limitations
BATTERY AND STARTER
CYCLE LIMITATIONS
An engine start cycle using battery only (ground starts with no
generators on-line, APU generator on-line and avionics button
ON, or any in-flight starter-assisted start) is equal to
battery
start cycle.
A generator-assisted engine start cycle (ground starts with APU
generator on-line and avionics button OFF and/or one engine
generator on-line) or an APU start cycle are equal to
of a
battery start cycle.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-20
BATTERY AND STARTER
CYCLE LIMITATIONS
An engine start cycle using battery only (ground starts with no
generators on-line, APU generator on-line and avionics button
ON, or any in-flight starter-assisted start) is equal to one battery
start cycle.
A generator-assisted engine start cycle (ground starts with APU
generator on-line and avionics button OFF and/or one engine
generator on-line) or an APU start cycle are equal to 1/3 of a
battery start cycle.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-20A
Limitations
BATTERY AND STARTER
CYCLE LIMITATIONS
If external power is used for engine or APU start,
cycle is counted.
battery start
Use of an external power source with voltage in excess of 28 VDC
or current in excess of
amps can damage the engine or APU
starter. Minimum
amps for engine or APU start.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-21
BATTERY AND STARTER
CYCLE LIMITATIONS
If external power is used for engine or APU start, no battery start
cycle is counted.
Use of an external power source with voltage in excess of 28 VDC
or current in excess of 1000 amps can damage the engine or APU
starter. Minimum 800 amps for engine or APU start.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-21A
Limitations
CABIN PRESSURIZATION LIMITATIONS
Normal Cabin Pressurization ....................................................... ?
Pressure Relief Valve ................................................................... ?
Pressure Gage Red Line .............................................................. ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-22
CABIN PRESSURIZATION LIMITATIONS
Normal Cabin Pressurization .................................. 0.0 to 9.3 PSI,
+0.1 or –0.1 PSI Differential
Pressure Relief Valve ......................................................... 9.5 PSI,
+0.1 or –0.1 PSI Differential
Pressure Gage Red Line ..................................................... 9.7 PSI
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-22A
Limitations
AIRPLANE BATTERY
If the red BATTERY OVERTEMP message illuminates during
, do not takeoff until after the airplane
Maintenance Manual procedures have been accomplished.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-23
AIRPLANE BATTERY
If the red BATTERY OVERTEMP message illuminates during
ground operation, do not takeoff until after the airplane
Maintenance Manual procedures have been accomplished.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-23A
Limitations
AUTOPILOT
One pilot must remain in his seat with the seat belt fastened
during all autopilot or
operations.
The autopilot minimum engage height, during climb following
takeoff or go-around, is
feet AGL.
Do not override the autopilot in
The autopilot or
landing.
.
must not be used during takeoff or
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-24
AUTOPILOT
One pilot must remain in his seat with the seat belt fastened
during all autopilot or yaw damper operations.
The autopilot minimum engage height, during climb following
takeoff or go-around, is 300 feet AGL.
Do not override the autopilot in pitch.
The autopilot or yaw damper must not be used during takeoff or
landing.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-24A
Limitations
AUTOPILOT
The autopilot minimum use height is:
a. Precision Approach (ILS, LPV, L/V):
feet AGL.
(1) All flap positions except for 35° feet AGL.
(2) Flaps 35° b. Non-precision Approach feet AGL.
c. Cruise feet AGL.
The autopilot must not be used if
inoperative.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
trim is
L-25
AUTOPILOT
The autopilot minimum use height is:
a. Precision Approach (ILS, LPV, L/V):
(1) All flap positions except for 35° - 115 feet AGL.
(2) Flaps 35° - 80 feet AGL.
b. Non-precision Approach - 300 feet AGL.
c. Cruise - 1000 feet AGL.
The autopilot must not be used if electric elevator trim is
inoperative.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-25A
Limitations
ROCKWELL COLLINS PRO LINE 21
AVIONICS AND FCS-3000 INTEGRATED
FLIGHT CONTROL SYSTEM
Autopilot-coupled VOR approaches in APPR or NAV mode are
. VOR approaches may be flown using APPR mode
with flight director only or in HDG mode with the autopilot
coupled.
VOR approaches conducted without DME must be intercepted
greater than nautical miles from the VOR.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-26
ROCKWELL COLLINS PRO LINE 21
AVIONICS AND FCS-3000 INTEGRATED
FLIGHT CONTROL SYSTEM
Autopilot-coupled VOR approaches in APPR or NAV mode are
prohibited. VOR approaches may be flown using APPR mode
with flight director only or in HDG mode with the autopilot
coupled.
VOR approaches conducted without DME must be intercepted
greater than 6 nautical miles from the VOR.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-26A
Limitations
ROCKWELL COLLINS PRO LINE 21
AVIONICS AND FCS-3000 INTEGRATED
FLIGHT CONTROL SYSTEM
It is prohibited to display the non-coupled side flight director
unless the coupled side flight director is being
. Failure
to adhere to this limitation will result in incorrect flight director
guidance. Use of the coupled side flight director by itself will
operate correctly.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-27
ROCKWELL COLLINS PRO LINE 21
AVIONICS AND FCS-3000 INTEGRATED
FLIGHT CONTROL SYSTEM
It is prohibited to display the non-coupled side flight director
unless the coupled side flight director is being displayed. Failure
to adhere to this limitation will result in incorrect flight director
guidance. Use of the coupled side flight director by itself will
operate correctly.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-27A
Limitations
ROCKWELL COLLINS PRO LINE 21
AVIONICS AND FCS-3000 INTEGRATED
FLIGHT CONTROL SYSTEM
Nav and localizer captures must be accomplished with an
intercept angle of less than
.
AHRS 1 and AHRS 2 must be operational for
ADC 1 and ADC 2 must be operational for
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
.
.
L-28
ROCKWELL COLLINS PRO LINE 21
AVIONICS AND FCS-3000 INTEGRATED
FLIGHT CONTROL SYSTEM
Nav and localizer captures must be accomplished with an
intercept angle of less than 90°.
AHRS 1 and AHRS 2 must be operational for takeoff.
ADC 1 and ADC 2 must be operational for takeoff.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-28A
Limitations
SUPPLEMENTAL OXYGEN SYSTEM
Crew and passenger oxygen masks are not approved for
use above
feet cabin altitude. Prolonged operation
of passenger masks above
feet cabin altitudes is not
recommended.
The pressure demand crew oxygen masks must be properly
stowed in their containers to qualify as a
oxygen
mask.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-29
SUPPLEMENTAL OXYGEN SYSTEM
Crew and passenger oxygen masks are not approved for
use above 40,000 feet cabin altitude. Prolonged operation
of passenger masks above 25,000 feet cabin altitudes is not
recommended.
The pressure demand crew oxygen masks must be properly
stowed in their containers to qualify as a quick-donning oxygen
mask.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-29A
Limitations
THRUST REVERSERS
Reverse thrust must be decreased to the idle reverse detent
position at
KIAS on landing roll.
Maximum allowable thrust reverser deployed time is
any 10-minute period.
Engine static ground operation is limited to
reversers are deployed).
Use of thrust reversers is
landings.
power (if thrust
during touch-and-go
CE-560XL XLS+
Revision 1.0
minutes in
FOR TRAINING PURPOSES ONLY
L-30
THRUST REVERSERS
Reverse thrust must be decreased to the idle reverse detent
position at 60 KIAS on landing roll.
Maximum allowable thrust reverser deployed time is 3 minutes in
any 10-minute period.
Engine static ground operation is limited to idle power (if thrust
reversers are deployed).
Use of thrust reversers is prohibited during touch-and-go
landings.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-30A
Limitations
APU
APU operation is
until a satisfactory APU test has been
accomplished as contained in the Normal Procedures section.
Starting the APU is
whenever the APU FAIL
annunciator is illuminated or the APU FAIL message is displayed.
APU start attempt is
after a dual generator failure.
Following shutdown for any reason, APU restart must not be
attempted until
seconds after the RPM indicator reads 0%.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-31
APU
APU operation is prohibited until a satisfactory APU test has been
accomplished as contained in the Normal Procedures section.
Starting the APU is prohibited whenever the APU FAIL
annunciator is illuminated or the APU FAIL message is displayed.
APU start attempt is prohibited after a dual generator failure.
Following shutdown for any reason, APU restart must not be
attempted until 30 seconds after the RPM indicator reads 0%.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-31A
Limitations
APU
Applying deice (anti-ice fluid of any type) is prohibited with APU
.
Deployment of the thrust reversers for more than
the APU running is prohibited.
The APU is not approved for
operation.
CE-560XL XLS+
Revision 1.0
seconds with
FOR TRAINING PURPOSES ONLY
L-32
APU
Applying deice (anti-ice fluid of any type) is prohibited with APU
operating.
Deployment of the thrust reversers for more than 30 seconds with
the APU running is prohibited.
The APU is not approved for unattended operation.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-32A
Limitations
APU OPERATING LIMITS
Starting
Maximum Altitude .................................................................. ?
Ambient Temp ........................................................................ ?
Running
Maximum Altitude .................................................................. ?
Ambient Temp ........................................................................ ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-33
APU OPERATING LIMITS
Starting
Maximum Altitude .................................................... 20,000 FT
Ambient Temp ................................................. -54°C to +54°C
Running
Maximum Altitude .................................................... 30,000 FT
Ambient Temp ................................................. -54°C to +54°C
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-33A
Limitations
APU OPERATING LIMITS
Transient APU generator current greater than
amps, but not
exceeding
amps, is approved during or after a main engine
start.
APU ammeter instrument markings:
• Red triangle =
amps - ground
• Red Line =
amps - flight
APU will
if EGT limits are exceeded.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-34
APU OPERATING LIMITS
Transient APU generator current greater than 200 amps, but not
exceeding 350 amps, is approved during or after a main engine
start.
APU ammeter instrument markings:
• Red triangle = 200 amps - ground
• Red Line = 230 amps - flight
APU will automatically shut down if EGT limits are exceeded.
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-34A
Limitations
TAIL DEICE SYSTEM
Minimum Temperature for use
(Airspeed below 150 KIAS) ..................................................... ?
(Airspeed at or above 150 KIAS) ............................................ ?
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-35
TAIL DEICE SYSTEM
Minimum Temperature for use
(Airspeed below 150 KIAS) .......................... -40°C (-40°F) RAT
(Airspeed at or above 150 KIAS) ................. -35°C (-31°F) RAT
CE-560XL XLS+
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-35A