CE-525C
CJ4
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INSERT LATEST REVISED CARDS, DESTROY SUPERSEDED CARDS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.................JAN. 2011
REVISION............... 0.1.................NOV. 2011
REVISION............... 0.2................ AUG. 2012
REVISION................0.3................. OCT. 2012
REVISION................1.0................ MAR. 2014
Incorporates AFM Rev. 4..........5 JULY 2012
TOTAL NUMBER OF CARDS IN THIS SET IS 67
CONSISTING OF THE FOLLOWING:
*Revision
Card
No.
No.
Card
No.
*Revision
No.
Title........................................................ 1.0
L-11 – L-11A.......................................... 1.0
ii............................................................. 1.0
L-12 – L-42A.......................................... 0.2
E-1 – E-22A........................................... 0.2
AGI-1 – AGI-2A...................................... 0.2
L-1......................................................... 0.2
L-1A ...................................................... 0.3
L-2 – L-10A............................................ 0.2
*Zero in this column indicates an original card.
Revision 1.0
FOR TRAINING PURPOSES ONLY
ii
Emergency
BATTERY FAIL
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-1
BATTERY FAIL
1. Battery Amps and Volts .......................................................... Note
2. BATTERY Switch ..................................................................... OFF
3. Battery Amps ......................................................... Note Decrease
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-1A
Emergency
BATTERY OVERTEMP
or
BATTERY OVERTEMP > 71°C
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-2
BATTERY OVERTEMP
or
BATTERY OVERTEMP > 71°C
1. Battery Amps and Volts .......................................................... Note
2. BATTERY Switch ..................................................................... OFF
3. Battery Amps ......................................................... Note Decrease
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-2A
Emergency
CABIN ALTITUDE
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-3
CABIN ALTITUDE
1.
2.
3.
4.
Oxygen Mask(s) ..................................................... Don and 100%
OXYGEN MASK MIC Button(s) ................................................. On
Emergency Descent .................................................. As Required
OXYGEN CONTROL Selector ........... DROP MASK, As Required
(ensure passengers are receiving oxygen)
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-3A
Emergency
ENGINE FIRE L or R
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-4
ENGINE FIRE L or R
1. THROTTLE (affected side) ...................................................... IDLE
• If Light Remains On After 15 Seconds
2. Illuminated ENG FIRE Button ........................................... Push
□ If Light Remains On After Additional 15 Seconds
3. Illuminated BOTTLE ARMED Button ................................ Push
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-4A
Emergency
NO TAKEOFF
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-5
NO TAKEOFF
1. Takeoff ................................................................................... Abort
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-5A
Emergency
WINDSHEAR
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-6
WINDSHEAR
1. THROTTLES .............................................................................. TO
2. Pitch Attitude ..................................................... Smoothly Rotate
to an initial pitch attitude of 7.5°
(FD Go Around pitch command)
3. Speedbrakes ............................................................................ 0%
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-6A
Emergency
ENGINE FAILURE or OTHER
EMERGENCY/ABNORMAL
EVENT DURING TAKEOFF
SPEED BELOW V1 - TAKEOFF REJECTED
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-7
ENGINE FAILURE or OTHER
EMERGENCY/ABNORMAL
EVENT DURING TAKEOFF
SPEED BELOW V1 - TAKEOFF REJECTED
1. Takeoff ................................................................................... Abort
a. Brakes ............................................................................. Apply
b. THROTTLES ...................................................................... IDLE
c. Ground Spoilers ............................................................ Extend
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-7A
Emergency
ENGINE FAILURE or OTHER
EMERGENCY/ABNORMAL
EVENT DURING TAKEOFF
SPEED ABOVE V1 - TAKEOFF CONTINUED
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-8
ENGINE FAILURE or OTHER
EMERGENCY/ABNORMAL
EVENT DURING TAKEOFF
SPEED ABOVE V1 - TAKEOFF CONTINUED
1. Climb to safe altitude.
a. Accelerate to VR ............................................................. Rotate
b. Landing Gear (positive climb) ............................................... Up
c. Airspeed ............................................................... V2 Minimum
d. Flaps (clear of obstacles and V2+10) ..................................... 0°
e. Airspeed ............................................................................ VENR
2. WING XFLOW Button ................................................................ On
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-8A
Emergency
DUAL ENGINE RESTART
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-9
DUAL ENGINE RESTART
1. ENGINE RUN/STOP Buttons (both) ..................................... STOP
2. THROTTLES ........................................................................... IDLE
3. BATTERY Switch (if descent to FL250 will
take longer than 5 min) ......................................................... EMER
4. Altitude ..................................................................... Below FL250
5. BATTERY Switch ....................................................................... ON
6. ANTI-ICE Buttons (all)................................................................ Off
7. HYDRAULIC SHUTOFF Buttons (both) ................. Push (lights on)
8. Airspeed ......................... 250 KIAS Minimum (altitude permitting)
9. ENGINE RUN/STOP Buttons (both) ....................................... RUN
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-9A
Emergency
ELECTRICAL FIRE OR SMOKE
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-10
ELECTRICAL FIRE OR SMOKE
1. Oxygen Mask(s)/Goggles ..................................... Don and EMER
2. OXYGEN MASK MIC Button(s) ................................................. On
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-10A
Emergency
ENVIRONMENTAL SYSTEM
SMOKE OR ODOR
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-11
ENVIRONMENTAL SYSTEM
SMOKE OR ODOR
1. Oxygen Mask(s)/Goggles ..................................... Don and EMER
2. OXYGEN MASK MIC Button(s) ................................................. On
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-11A
Emergency
SMOKE REMOVAL
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-12
SMOKE REMOVAL
1. Oxygen Mask(s)/Goggles ..................................... Don and EMER
2. OXYGEN MASK MIC Button(s) ................................................. On
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-12A
Emergency
EMERGENCY DESCENT
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-13
EMERGENCY DESCENT
1. Initiate maximum rate of descent to a safe altitude.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-13A
Emergency
WHEEL BRAKE FAILURE
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-14
WHEEL BRAKE FAILURE
1.
2.
3.
4.
Brake Pedals ........................................................... Remove Feet
GROUND SPOILERS (after nosewheel touchdown) ....... EXTEND
EMER BRAKE Handle ......................................... Pull as Required
Directional Control .................. Maintain with Nosewheel Steering
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-14A
Emergency
AILERON TRIM RUNAWAY
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-15
AILERON TRIM RUNAWAY
1. AP TRIM DISC Button ........................................... Push and Hold
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-15A
Emergency
PRIMARY PITCH TRIM RUNAWAY
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-16
PRIMARY PITCH TRIM RUNAWAY
1. AP TRIM DISC Button ........................................... Push and Hold
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-16A
Emergency
UNCOMMANDED ROLL
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-17
UNCOMMANDED ROLL
1. AP TRIM DISC Button ........................................... Push and Hold
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-17A
Emergency
SECONDARY PITCH TRIM RUNAWAY
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-18
SECONDARY PITCH TRIM RUNAWAY
1. SECONDARY ELEV TRIM ENABLE Button ............................... Off
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-18A
Emergency
RUDDER TRIM RUNAWAY
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-19
RUDDER TRIM RUNAWAY
1. AP TRIM DISC Button ........................................... Push and Hold
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-19A
Emergency
AUTOPILOT MALFUNCTION
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-20
AUTOPILOT MALFUNCTION
1. AP TRIM DISC Button ........................................................... Push
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-20A
Emergency
INADVERTENT STALL
(STICK SHAKER, BUFFET, AND/OR ROLL-OFF)
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-21
INADVERTENT STALL
(STICK SHAKER, BUFFET, AND/OR ROLL-OFF)
1.
2.
3.
4.
5.
6.
AP TRIM DISC Button ........................................................... Push
Pitch Attitude ....................................... Reduce Approximately 5°
Roll Attitude................................................................ Wings Level
THROTTLES .............................................................................. TO
Speedbrakes ............................................................................ 0%
Airspeed ............................................ Increase 5 KIAS, Minimum
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-21A
Emergency
EMERGENCY EVACUATION
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-22
EMERGENCY EVACUATION
PARK BRAKE Handle ............................................................... Set
ENGINE RUN/STOP Buttons (both) ..................................... STOP
ENG FIRE Buttons (both) ...................................................... Push
BOTTLE ARMED Button (affected side, if fire suspected) .... Push
Emergency Locator Transmitter (ELT) ......... Activate as Required
BATTERY Switch ..................................................................... OFF
Airplane and Immediate Area .............. Determine Escape Route
and Direct Evacuation
8. Move away from airplane.
1.
2.
3.
4.
5.
6.
7.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
E-22A
Limitations
WEIGHT LIMITS
Maximum design ramp weight .......................................................... ?
Maximum design takeoff weight ....................................................... ?
Maximum design landing weight ....................................................... ?
Maximum design zero fuel weight ..................................................... ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-1
WEIGHT LIMITS
Maximum design ramp weight ................................... 17,230 Pounds
Maximum design takeoff weight ................................ 17,110 Pounds
Maximum design landing weight ................................ 15,660 Pounds
Maximum design zero fuel weight .............................. 12,500 Pounds
CE-525C CJ4
Revision 0.3
FOR TRAINING PURPOSES ONLY
L-1A
Limitations
WEIGHT LIMITS
Maximum baggage weight in nose compartment ............................. ?
Maximum baggage weight in tailcone compartment ........................ ?
Maximum load distribution
(nose baggage compartment) ...................................................... ?
Maximum load distribution
(tailcone baggage compartment) ................................................. ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-2
WEIGHT LIMITS
Maximum baggage weight in nose compartment ........... 400 Pounds
Maximum baggage weight in tailcone compartment ...... 600 Pounds
Maximum load distribution
(nose baggage compartment) ......... 35 Pounds per Square Foot
Maximum load distribution
(tailcone baggage compartment) .. 150 Pounds per Square Foot
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-2A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum altitude limit ...................................................................... ?
Maximum tailwind component .......................................................... ?
Takeoff is
with an amber ENGINE CTRL SYS FAULT L
and/or R message displayed.
The autopilot and
landing.
must be disengaged for takeoff and
Takeoff is prohibited if the antiskid system is
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
.
L-3
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Maximum altitude limit .................................................... 14,000 Feet
Maximum tailwind component ............................................ 10 Knots
Takeoff is prohibited with an amber ENGINE CTRL SYS FAULT L
and/or R message displayed.
The autopilot and yaw damper must be disengaged for takeoff and
landing.
Takeoff is prohibited if the antiskid system is inoperative.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-3A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Takeoff is prohibited until the battery charging amps is
less.
Cabin must be depressurized prior to
Takeoffs and landings are limited to
amps or
.
runway surfaces.
Except where required by AFM procedures, speed brakes must be
retracted prior to
feet AGL for landing.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-4
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Takeoff is prohibited until the battery charging amps is 20 amps or
less.
Cabin must be depressurized prior to landing.
Takeoffs and landings are limited to paved runway surfaces.
Except where required by AFM procedures, speed brakes must be
retracted prior to 500 feet AGL for landing.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-4A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Takeoff is limited to the flaps
configuration when Type II, III, or IV antiice fluid has been applied to the airplane.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-5
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Takeoff is limited to the flaps 0° configuration when Type II, III, or IV antiice fluid has been applied to the airplane.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-5A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Takeoff is prohibited with the following forms of contamination:
1. With frost adhering to the following critical areas:
b. Upper wing surface c. Windshield
a.
2. With ice, snow, or slush adhering to the following critical areas:
a.
b. Flight control
surfaces including all hinge gaps c. Horizontal stabilizer d. Vertical
stabilizer e. Engine inlets f. Top of engine pylons g. Top of fuselage
h. Windshield i. All pitot probes and static ports j. Angle of attack
vane k. Upper surface of nose forward of the windshield
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-6
TAKEOFF AND LANDING
OPERATIONAL LIMITS
Takeoff is prohibited with the following forms of contamination:
1. With frost adhering to the following critical areas:
a. Wing leading edge b. Upper wing surface c. Windshield
2. With ice, snow, or slush adhering to the following critical areas:
a. Wing leading edge and upper wing surface b. Flight control
surfaces including all hinge gaps c. Horizontal stabilizer d. Vertical
stabilizer e. Engine inlets f. Top of engine pylons g. Top of fuselage
h. Windshield i. All pitot probes and static ports j. Angle of attack
vane k. Upper surface of nose forward of the windshield
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-6A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
A visual and tactile (hand on surface) check of the wing leading edge and wing
upper surface must be performed to ensure the wing is free from
, ice,
snow, or slush when the outside air temperature is less than C or if it cannot
be determined that the wing fuel temperature is above 0°C and any of the
following conditions exist:
1. There is visible moisture present (rain, drizzle, sleet, snow, fog, etc.); or
2. Water is present on the
; or
3. The difference between the dew point and the outside air temperature is
3°C or less; or
4. The atmospheric conditions have been conducive to frost formation.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-7
TAKEOFF AND LANDING
OPERATIONAL LIMITS
A visual and tactile (hand on surface) check of the wing leading edge and wing
upper surface must be performed to ensure the wing is free from frost, ice,
snow, or slush when the outside air temperature is less than 5°C or if it cannot
be determined that the wing fuel temperature is above 0°C and any of the
following conditions exist:
1. There is visible moisture present (rain, drizzle, sleet, snow, fog, etc.); or
2. Water is present on the upper wing surface; or
3. The difference between the dew point and the outside air temperature is
3°C or less; or
4. The atmospheric conditions have been conducive to frost formation.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-7A
Limitations
TAKEOFF AND LANDING
OPERATIONAL LIMITS
The tactile check must be accomplished within
minutes of takeoff
under conditions where additional contamination may reasonably
be expected (rain, drizzle, sleet, snow, fog, active frost formation,
decreasing temperatures, etc.). If the aircraft is treated with the
appropriate deicing/anti-icing fluids (refer to Section VII), the tactile
check may be accomplished any time between final application of the
fluid and
, provided that time is within the maximum applicable
holdover time.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-8
TAKEOFF AND LANDING
OPERATIONAL LIMITS
The tactile check must be accomplished within five minutes of takeoff
under conditions where additional contamination may reasonably
be expected (rain, drizzle, sleet, snow, fog, active frost formation,
decreasing temperatures, etc.). If the aircraft is treated with the
appropriate deicing/anti-icing fluids (refer to Section VII), the tactile
check may be accomplished any time between final application of the
fluid and takeoff, provided that time is within the maximum applicable
holdover time.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-8A
Limitations
ENROUTE OPERATIONAL LIMITS
Maximum operating altitude .............................................................. ?
Maximum operating altitude with WING XFLOW on ......................... ?
Maximum altitude for extension of flaps and/or landing gear ........... ?
Maximum operating altitude with inoperative yaw damper .............. ?
Maximum operating altitude with
amber DC GENERATOR OFF L-R displayed ............................... ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-9
ENROUTE OPERATIONAL LIMITS
Maximum operating altitude ..................................................... FL450
Maximum operating altitude with WING XFLOW on ................ FL410
Maximum altitude for extension of flaps and/or landing gear .. FL180
Maximum operating altitude with inoperative yaw damper ..... FL240
Maximum operating altitude with
amber DC GENERATOR OFF L-R displayed ...................... FL350
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-9A
Limitations
FUEL LIMITS
Maximum demonstrated fuel imbalance for emergency return
following a fuel system malfunction is
lbs.
Maximum approved fuel imbalance for normal operation ................ ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-10
FUEL LIMITS
Maximum demonstrated fuel imbalance for emergency return
following a fuel system malfunction is 600 lbs.
Maximum approved fuel imbalance for normal operation ..... 200 lbs
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-10A
Limitations
SINGLE POINT REFUELING LIMITS
Single point refueling operations must be conducted per the procedures
contained on the placard installed on the single point refueling access door.
Refueling pressure range is
psi; maximum defuel pressure is -10 psi.
ENGINE OPERATING LIMITS
Takeoff thrust settings, which are normally limited to minutes duration
for all engine operating conditions, may be used for up to
minutes for
one engine inoperative operations. Timing begins when throttle lever is
advanced to the TO detent.
CE-525C CJ4
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-11
SINGLE POINT REFUELING LIMITS
Single point refueling operations must be conducted per the procedures
contained on the placard installed on the single point refueling access door.
Refueling pressure range is 10-55 psi; maximum defuel pressure is -10 psi.
ENGINE OPERATING LIMITS
Takeoff thrust settings, which are normally limited to 5 minutes duration
for all engine operating conditions, may be used for up to 10 minutes for
one engine inoperative operations. Timing begins when throttle lever is
advanced to the TO detent.
CE-525C CJ4
Revision 1.0
FOR TRAINING PURPOSES ONLY
L-11A
Limitations
APPROVED OILS
is the preferred oil.
Mixing of approved oils is
Approved oils include
.
&
.
Maximum oil consumption is
gallons per 1 hour period ( qt or
L per 8 hours). Refer to the aircraft maintenance manual when oil
consumption exceeds this value.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-12
APPROVED OILS
Mobil Jet II is the preferred oil.
Mixing of approved oils is permissible.
Approved oils include Mobil Jet II & Mobil 254.
Maximum oil consumption is 0.032 gallons per 1 hour period (1 qt or
1 L per 8 hours). Refer to the aircraft maintenance manual when oil
consumption exceeds this value.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-12A
Limitations
ENGINE START LIMITS
GENERAL
Amber ENGINE CTRL SYS FAULT message
displayed .......................................................................................... ?
Generator switches ................................................................................ ?
Time to light-off is defined as the time from first indication of fuel flow
until an
increase is observed.
Maximum time to light-off ...................................................................... ?
Minimum time prior to power increase above 80% N2 .......................... ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-13
ENGINE START LIMITS
GENERAL
Amber ENGINE CTRL SYS FAULT message
displayed ..................................................... Engine start prohibited
Generator switches ............................................... ON for engine starts
Time to light-off is defined as the time from first indication of fuel flow
until an ITT increase is observed.
Maximum time to light-off .................. 10 seconds (ground starts only)
Minimum time prior to power increase above 80% N2 ........... 2 minutes
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-13A
Limitations
ENGINE START LIMITS
GROUND STARTS
Maximum elevation for battery or cross generator starts ...................... ?
Maximum tailwind component ............................................................... ?
Maximum crosswind component ........................................................... ?
Minimum battery voltage for battery start .............................................. ?
Minimum/maximum external power current
capacity for start ............................................................................... ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-14
ENGINE START LIMITS
GROUND STARTS
Maximum elevation for battery or cross generator starts ..... 14,000 Feet
Maximum tailwind component .................................................. 19 Knots
Maximum crosswind component .............................................. 19 Knots
Minimum battery voltage for battery start ................................... 24 VDC
Minimum/maximum external power current
capacity for start ...................................................... 800/1200 AMPS
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-14A
Limitations
ENGINE START LIMITS
GROUND STARTS
Engine oil must be preheated to at least
°C prior to conducting a start.
Lithium batteries must be preheated to at least
(SYSTEMS 1 format/overlay on MFD).
°C prior to start
Nickel-cadmium and lead-acid batteries must be preheated to at least
°C prior to start (SYSTEMS 1 format/overlay on MFD).
If the airplane has been cold soaked in ambient temperatures below
-40°C, the FADECs must be warmed with electrical power for at least
minutes followed by a power cycle with the battery switch.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-15
ENGINE START LIMITS
GROUND STARTS
Engine oil must be preheated to at least -40°C prior to conducting a start.
Lithium batteries must be preheated to at least -10°C prior to start
(SYSTEMS 1 format/overlay on MFD).
Nickel-cadmium and lead-acid batteries must be preheated to at least
-20°C prior to start (SYSTEMS 1 format/overlay on MFD).
If the airplane has been cold soaked in ambient temperatures below
-40°C, the FADECs must be warmed with electrical power for at least 3
minutes followed by a power cycle with the battery switch.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-15A
Limitations
ENGINE START LIMITS
GROUND STARTS
Depending on battery condition, the MFD may momentarily blank
during MFD power up. If this condition is observed, the airplane must
be powered by a
to complete the preflight and engine
starts. Failure to power the airplane with a ground power unit may result
in insufficient power to the MFD, causing the MFD to blank during start.
This blanking will require the start to be
.
Minimum engine oil temperature (indicated on EIS) ............................... ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-16
ENGINE START LIMITS
GROUND STARTS
Depending on battery condition, the MFD may momentarily blank during
MFD power up. If this condition is observed, the airplane must be
powered by a ground power unit to complete the preflight and engine
starts. Failure to power the airplane with a ground power unit may result
in insufficient power to the MFD, causing the MFD to blank during start.
This blanking will require the start to be terminated.
Minimum engine oil temperature (indicated on EIS) ........................ -40°C
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-16A
Limitations
START CYCLE LIMITS
Engine starter limits ................................................................................ ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-17
START CYCLE LIMITS
Engine starter limits ...................... Three engine starts per 30 minutes.
Three cycles of operation with a
60-second rest period between
cycles is permitted.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-17A
Limitations
SPEED LIMITS
Maximum operating limit speeds
MMO (above 27,884 feet) .................................................................. ?
VMO (between 8000 and 27,884 feet) ............................................... ?
VMO (below 8000 feet) ...................................................................... ?
Maximum flap extended speed - VFE
Takeoff and approach position (15°) ................................................. ?
Landing position (35°) ....................................................................... ?
Maximum landing gear extended speed - VLE ....................................... ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-18
SPEED LIMITS
Maximum operating limit speeds
MMO (above 27,884 feet) ................................ Mach 0.77 (indicated)
VMO (between 8000 and 27,884 feet) .................................. 305 KIAS
VMO (below 8000 feet) ......................................................... 260 KIAS
Maximum flap extended speed - VFE
Takeoff and approach position (15°) .................................... 200 KIAS
Landing position (35°) .......................................................... 160 KIAS
Maximum landing gear extended speed - VLE .......................... 200 KIAS
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-18A
Limitations
SPEED LIMITS
Maximum landing gear operating speed - VLO
(Extending or Retracting) .................................................................. ?
Maximum speed brake operation speed - VSB ...................................... ?
Maximum autopilot operation speed ..................................................... ?
Minimum speed for sustained flight In icing conditions
(Flaps 0°) ........................................................................................... ?
Maximum tire ground speed .................................................................. ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-19
SPEED LIMITS
Maximum landing gear operating speed - VLO
(Extending or Retracting) ..................................................... 200 KIAS
Maximum speed brake operation speed - VSB .......................... No Limit
Maximum autopilot operation speed ................. 305 KIAS or Mach 0.77
Minimum speed for sustained flight In icing conditions
(Flaps 0°) .............................................................................. 160 KIAS
Maximum tire ground speed ................................................... 165 Knots
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-19A
Limitations
MANEUVER LIMITS
Acrobatic maneuvers, including spins, are
Intentional stalls are prohibited above
.
feet.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-20
MANEUVER LIMITS
Acrobatic maneuvers, including spins, are prohibited.
Intentional stalls are prohibited above 18,000 feet.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-20A
Limitations
BATTERY LIMITS
Lead-acid and nickel-cadmium batteries are approved for use in the CJ4.
Lithium batteries may
be used for ground or flight operations unless
approved by later AFM revision.
The battery temperature indicating system must be operational for all
and
operations.
If the red BATTERY OVERTEMP message displays during ground operations,
do not take off until the proper maintenance procedures have been
accomplished. Even if the message subsequently clears, dispatch is
until after the proper maintenance procedures have been accomplished.
Battery start limit ................................................................................................ ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-21
BATTERY LIMITS
Lead-acid and nickel-cadmium batteries are approved for use in the CJ4.
Lithium batteries may not be used for ground or flight operations unless
approved by later AFM revision.
The battery temperature indicating system must be operational for all ground
and flight operations.
If the red BATTERY OVERTEMP message displays during ground operations,
do not take off until the proper maintenance procedures have been
accomplished. Even if the message subsequently clears, dispatch is prohibited
until after the proper maintenance procedures have been accomplished.
Battery start limit ................................................. Three engine starts per hour
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-21A
Limitations
ELECTRICAL POWER SYSTEMS
Steady state generator limits are:
Ground .................................................................................................. ?
Air ≤ FL250 ............................................................................................ ?
> FL250 and ≤ FL450............................................................................. ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-22
ELECTRICAL POWER SYSTEMS
Steady state generator limits are:
Ground ................................................................................... 240 Amps
Air ≤ FL250 ............................................................................. 300 Amps
> FL250 and ≤ FL450.. Linear decrease from 300 Amps to 170 Amps
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-22A
Limitations
CABIN PRESSURIZATION LIMITS
Structural cabin pressurization
limits ................................................................................................. ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-23
CABIN PRESSURIZATION LIMITS
Structural cabin pressurization
limits ...................................... (-0.5 to 9.0 PSI) ± 0.1 PSI Differential
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-23A
Limitations
SUPPLEMENTAL OXYGEN SYSTEM
The use of medical oxygen is
.
Crew and passenger oxygen masks are not approved for use above
feet cabin altitude. Prolonged use of passenger masks above
25,000 feet cabin altitude is not recommended.
Prior to flight, the crew oxygen mask must be checked and stowed
properly in its receptacle to qualify as a
oxygen mask.
For single pilot operations, a crew oxygen mask
be available for
a passenger occupying the right crew seat. The mask must be checked
during preflight and passenger briefed on its use.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-24
SUPPLEMENTAL OXYGEN SYSTEM
The use of medical oxygen is prohibited.
Crew and passenger oxygen masks are not approved for use above
40,000 feet cabin altitude. Prolonged use of passenger masks above
25,000 feet cabin altitude is not recommended.
Prior to flight, the crew oxygen mask must be checked and stowed
properly in its receptacle to qualify as a quick donning oxygen mask.
For single pilot operations, a crew oxygen mask must be available for
a passenger occupying the right crew seat. The mask must be checked
during preflight and passenger briefed on its use.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-24A
Limitations
PASSENGER COMPARTMENT
For taxi, takeoff, and landing, all adjustable seats must be fully
and
; all occupied seats must have the head rest extended,
seat controls inboard, seat tracked away from the table and then
outboard, and passenger seat belts and shoulder harnesses must be
fastened.
The maximum number of occupants in the passenger compartment is
(
with the optional two-place side-facing couch installed).
The lavatory door must be latched
The lavatory is limited to
for taxi, takeoff, and landing.
occupant.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-25
PASSENGER COMPARTMENT
For taxi, takeoff, and landing, all adjustable seats must be fully upright
and outboard; all occupied seats must have the head rest extended,
seat controls inboard, seat tracked away from the table and then
outboard, and passenger seat belts and shoulder harnesses must be
fastened.
The maximum number of occupants in the passenger compartment is
eight (nine with the optional two-place side-facing couch installed).
The lavatory door must be latched open for taxi, takeoff, and landing.
The lavatory is limited to one occupant.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-25A
Limitations
GROUND OPERATIONAL LIMITS
Limit ground operation of pitot/static heat to
minutes to prevent
damage to the pitot tubes and angle of attack vane.
Ground operation at greater than 75% N2 engine RPM with wing
anti-ice on is limited to
minutes. Do not operate with wing antiice on more than
minute after the cyan or amber WING ANTI-ICE
COLD message(s) have extinguished during preflight checks.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-26
GROUND OPERATIONAL LIMITS
Limit ground operation of pitot/static heat to two minutes to prevent
damage to the pitot tubes and angle of attack vane.
Ground operation at greater than 75% N2 engine RPM with wing
anti-ice on is limited to two minutes. Do not operate with wing antiice on more than one minute after the cyan or amber WING ANTI-ICE
COLD message(s) have extinguished during preflight checks.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-26A
Limitations
GROUND OPERATIONAL LIMITS
Ambient surface temperature must be obtained from the
on
the cockpit displays, with either or both engines operating, or from an
appropriate ground station.
The control lock must not be set if the airplane will be exposed to
temperatures below
°C.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-27
GROUND OPERATIONAL LIMITS
Ambient surface temperature must be obtained from the SAT field on
the cockpit displays, with either or both engines operating, or from an
appropriate ground station.
The control lock must not be set if the airplane will be exposed to
temperatures below -10°C.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-27A
Limitations
RVSM OPERATIONS
AIRSPEED LIMITS
Minimum speed in RVSM airspace ........................................................ ?
WEIGHT LIMITS
Minimum weight in RVSM airspace ....................................................... ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-28
RVSM OPERATIONS
AIRSPEED LIMITS
Minimum speed in RVSM airspace ........................................... 130 KIAS
WEIGHT LIMITS
Minimum weight in RVSM airspace ................................ 11,050 Pounds
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-28A
Limitations
ROCKWELL COLLINS FCS-3000
INTEGRATED FLIGHT CONTROL SYSTEM
Category II approaches are
Operating in the
failure conditions.
approved.
mode is limited to training and display
the airplane is prohibited until all AHRS ground alignment is
completed.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-29
ROCKWELL COLLINS FCS-3000
INTEGRATED FLIGHT CONTROL SYSTEM
Category II approaches are not approved.
Operating in the composite mode is limited to training and display
failure conditions.
Taxiing the airplane is prohibited until all AHRS ground alignment is
completed.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-29A
Limitations
ROCKWELL COLLINS FCS-3000
INTEGRATED FLIGHT CONTROL SYSTEM
Autopilot:
a. Use of the autopilot or yaw damper is prohibited during takeoff or landing.
b. One pilot must remain seated with seat belt fastened during all autopilot operations.
c. The autopilot minimum engage height, during climb following takeoff or go-around,
is
feet AGL.
d. The autopilot minimum use height is:
(1) ILS approach (CAT I) & LPV/WAAS feet AGL (flaps 0°-35°)
(2) Other non-precision approach feet AGL
(3) Cruise feet AGL
e. Do not override the autopilot in pitch during normal operation.
f. Use of the autopilot is prohibited if primary elevator trim is inoperative.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-30
ROCKWELL COLLINS FCS-3000
INTEGRATED FLIGHT CONTROL SYSTEM
Autopilot:
a. Use of the autopilot or yaw damper is prohibited during takeoff or landing.
b. One pilot must remain seated with seat belt fastened during all autopilot operations.
c. The autopilot minimum engage height, during climb following takeoff or go-around,
is 300 feet AGL.
d. The autopilot minimum use height is:
(1) ILS approach (CAT I) & LPV/WAAS - 200 feet AGL (flaps 0°-35°)
(2) Other non-precision approach - 200 feet AGL
(3) Cruise - 1000 feet AGL
e. Do not override the autopilot in pitch during normal operation.
f. Use of the autopilot is prohibited if primary elevator trim is inoperative.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-30A
Limitations
ROCKWELL COLLINS FCS-3000
INTEGRATED FLIGHT CONTROL SYSTEM
VOR approaches must not be conducted in the
mode of the flight director.
Use the
mode, or manually track the approach course using the HDG mode.
This limit applies to both flight director only and autopilot coupled operation.
Autopilot coupled operation is prohibited during any portion of a VOR approach
in which the VOR is located behind the airplane by more than
miles, unless
the HDG mode of the flight director is being used to manually track the approach
course.
VOR approaches conducted without DME must be intercepted greater than
nautical miles from the VOR.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-31
ROCKWELL COLLINS FCS-3000
INTEGRATED FLIGHT CONTROL SYSTEM
VOR approaches must not be conducted in the NAV mode of the flight director.
Use the APPR mode, or manually track the approach course using the HDG mode.
This limit applies to both flight director only and autopilot coupled operation.
Autopilot coupled operation is prohibited during any portion of a VOR approach
in which the VOR is located behind the airplane by more than 15 miles, unless
the HDG mode of the flight director is being used to manually track the approach
course.
VOR approaches conducted without DME must be intercepted greater than 6
nautical miles from the VOR.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-31A
Limitations
ROCKWELL COLLINS 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 limit
will result in
Flight Director guidance. Use of the coupled side Flight
Director by itself will operate correctly.
When conducting an approach that utilizes a localizer (ILS, LOC, LOC-BC,
LDA, SDF), the approach mode
must not be selected until the course
deviation indicator (CDI) has clearly moved away from a full scale deflection
and the aircraft is within the published service volume for the approach. Failure
to observe this limit may result in capture of a false localizer lobe, resulting in
incorrect lateral guidance.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-32
ROCKWELL COLLINS 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 limit
will result in incorrect Flight Director guidance. Use of the coupled side Flight
Director by itself will operate correctly.
When conducting an approach that utilizes a localizer (ILS, LOC, LOC-BC,
LDA, SDF), the approach mode (APPR) must not be selected until the course
deviation indicator (CDI) has clearly moved away from a full scale deflection
and the aircraft is within the published service volume for the approach. Failure
to observe this limit may result in capture of a false localizer lobe, resulting in
incorrect lateral guidance.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-32A
Limitations
ANGLE-OF-ATTACK AND
STICK SHAKER SYSTEM
The angle-of-attack system may be used as a
, but does not
replace the airspeed display in the PFD as a primary instrument.
The angle-of-attack system can be used as a reference for approach
speed (VREF) at all airplane weights, CG locations, and flap positions.
VREF is indicated by approximately
on the AOA gauge, green circle
on AOA indexer (if installed), and by the green circle on the pilot and
copilot’s airspeed indicators.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-33
ANGLE-OF-ATTACK AND
STICK SHAKER SYSTEM
The angle-of-attack system may be used as a reference, but does not
replace the airspeed display in the PFD as a primary instrument.
The angle-of-attack system can be used as a reference for approach
speed (VREF) at all airplane weights, CG locations, and flap positions.
VREF is indicated by approximately 0.6 on the AOA gauge, green circle
on AOA indexer (if installed), and by the green circle on the pilot and
copilot’s airspeed indicators.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-33A
Limitations
COCKPIT SPEAKER MUTE
The pilot(s) must use a headset(s) when the overhead cockpit speaker
audio is
.
PULSELITE SYSTEM
The pulse light system must be OFF and remain OFF during the
following night ground and night flight operations: taxi, takeoff, and
landing approach at
feet AGL and below.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-34
COCKPIT SPEAKER MUTE
The pilot(s) must use a headset(s) when the overhead cockpit speaker
audio is muted.
PULSELITE SYSTEM
The pulse light system must be OFF and remain OFF during the
following night ground and night flight operations: taxi, takeoff, and
landing approach at 300 feet AGL and below.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-34A
Limitations
ICE AND RAIN PROTECTION
Icing conditions in flight exist when SAT is
°C or colder and visible
moisture in any form is present (such as clouds, fog with visibility of one mile
or less, rain, snow, sleet, or ice crystals).
Icing conditions on the ground exist with an OAT or SAT below °C or colder
and where surface snow, slush, ice or standing water may be ingested by the
engines or freeze on engine nacelles, or engine sensor probes.
The wing icing inspection light must be operative
forecast icing conditions at night.
to flight into known or
All anti-ice and de-ice systems must be
in flight when operating in icing
conditions, except tail deice must be off when SAT is below -30°C.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-35
ICE AND RAIN PROTECTION
Icing conditions in flight exist when SAT is +10°C or colder and visible
moisture in any form is present (such as clouds, fog with visibility of one mile
or less, rain, snow, sleet, or ice crystals).
Icing conditions on the ground exist with an OAT or SAT below +5°C or colder
and where surface snow, slush, ice or standing water may be ingested by the
engines or freeze on engine nacelles, or engine sensor probes.
The wing icing inspection light must be operative prior to flight into known or
forecast icing conditions at night.
All anti-ice and de-ice systems must be ON in flight when operating in icing
conditions, except tail deice must be off when SAT is below -30°C.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-35A
Limitations
ICE AND RAIN PROTECTION
Engine anti-ice must be ON during ground operations in icing
conditions, except selection of anti-ice on is prohibited for
after ground engine start (to ensure accurate RAT for takeoff). If engine
anti-ice was inadvertently turned ON prior to 1 minute of engine
operation, the anti-ice must be turned off for
before turning
it back on. If minor engine vibrations are felt or heard during ground
operations, the crew must momentarily increase engine speed (typically
20-30% N1) to assist with shedding the accumulated ice from the
spinner, fan, and stators.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-36
ICE AND RAIN PROTECTION
Engine anti-ice must be ON during ground operations in icing
conditions, except selection of anti-ice on is prohibited for 1 minute
after ground engine start (to ensure accurate RAT for takeoff). If engine
anti-ice was inadvertently turned ON prior to 1 minute of engine
operation, the anti-ice must be turned off for 2 minutes before turning
it back on. If minor engine vibrations are felt or heard during ground
operations, the crew must momentarily increase engine speed (typically
20-30% N1) to assist with shedding the accumulated ice from the
spinner, fan, and stators.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-36A
Limitations
ICE AND RAIN PROTECTION
When SAT is below
°C, the wing and engine anti-ice systems may be
operated in the ENG ONLY position if it can be visually verified that no
ice is accumulating.
Failure to operate engine anti-ice may result in amber ENG CTRL SYS
FAULT messages due to ice accumulation on the engine
probe.
Minimum temperature for operation of tail deicing boots (SAT) ............. ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-37
ICE AND RAIN PROTECTION
When SAT is below -40°C, the wing and engine anti-ice systems may be
operated in the ENG ONLY position if it can be visually verified that no
ice is accumulating.
Failure to operate engine anti-ice may result in amber ENG CTRL SYS
FAULT messages due to ice accumulation on the engine PT2/TT2
probe.
Minimum temperature for operation of tail deicing boots (SAT) ...... -30°C
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-37A
Limitations
ICE AND RAIN PROTECTION
Minimum airspeed for sustained flight in icing conditions (except takeoff,
approach, and landing) is
KIAS. If wing anti-ice protection has failed
and/or ice has accumulated on the wing leading edge, maintain
KIAS
minimum until approaching to land and disengage the autopilot prior to
extending flaps or reducing airspeed below
KIAS.
In icing conditions, operating the airplane at other than flaps 0° and
landing gear up for an extended period of time (except approach and
landing) is
.
Minimum engine N2 speed for effective wing anti-icing ........................... ?
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-38
ICE AND RAIN PROTECTION
Minimum airspeed for sustained flight in icing conditions (except takeoff,
approach, and landing) is 160 KIAS. If wing anti-ice protection has failed
and/or ice has accumulated on the wing leading edge, maintain 160 KIAS
minimum until approaching to land and disengage the autopilot prior to
extending flaps or reducing airspeed below 160 KIAS.
In icing conditions, operating the airplane at other than flaps 0° and
landing gear up for an extended period of time (except approach and
landing) is prohibited.
Minimum engine N2 speed for effective wing anti-icing ................ 75% N2
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-38A
Limitations
OPERATIONS IN SEVERE
ICING CONDITIONS
Operation in severe icing is
. The airplane has not been
designed or certified to provide protection against severe icing
conditions, including freezing drizzle, freezing rain, or severe conditions
of mixed or clear ice.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-39
OPERATIONS IN SEVERE
ICING CONDITIONS
Operation in severe icing is prohibited. The airplane has not been
designed or certified to provide protection against severe icing
conditions, including freezing drizzle, freezing rain, or severe conditions
of mixed or clear ice.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-39A
Limitations
OPERATIONS IN SEVERE
ICING CONDITIONS
Severe icing conditions that exceed those for which the airplane is
certificated shall be determined by the following visual cues:
1. Unusually extensive ice accumulation on the airframe and
in areas not normally observed to collect ice (such as the outboard
1/3 of forward
).
2. Unusual accumulation of ice on the upper surface of the
(significant accumulations on the heated surfaces, ridge formations
running inboard to outboard on the upper surface, runback ice
extending more than 18 inches aft of the heated leading edge).
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-40
OPERATIONS IN SEVERE
ICING CONDITIONS
Severe icing conditions that exceed those for which the airplane is
certificated 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 (such as the outboard
1/3 of forward windshield).
2. Unusual accumulation of ice on the upper surface of the wing
(significant accumulations on the heated surfaces, ridge formations
running inboard to outboard on the upper surface, runback ice
extending more than 18 inches aft of the heated leading edge).
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-40A
Limitations
OPERATIONS IN SEVERE
ICING CONDITIONS
If one or more of these visual cues exist:
1. Use of the autopilot is
.
2. Immediately request priority handling from Air Traffic Control to
facilitate a route or altitude change to exit the icing conditions.
3. Leave flaps in
position, do not extend or retract.
4. Avoid abrupt and excessive maneuvering that may aggravate control
problems.
5. If unusual or uncommanded roll control movement is observed,
reduce
.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-41
OPERATIONS IN SEVERE
ICING CONDITIONS
If one or more of these visual cues exist:
1. Use of the autopilot is prohibited.
2. Immediately request priority handling from Air Traffic Control to
facilitate a route or altitude change to exit the icing conditions.
3. Leave flaps in current position, do not extend or retract.
4. Avoid abrupt and excessive maneuvering that may aggravate control
problems.
5. If unusual or uncommanded roll control movement is observed,
reduce angle-of-attack.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-41A
Limitations
OPERATIONS IN SEVERE
ICING CONDITIONS
Since the autopilot, when installed and operating, may mask tactile cues
that indicate adverse changes in handling characteristics, use of the
autopilot is prohibited when:
1. Unusual
conditions.
2.
conditions.
trim is required while the airplane is in icing
warnings are encountered while the airplane is in icing
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-42
OPERATIONS IN SEVERE
ICING CONDITIONS
Since the autopilot, when installed and operating, may mask tactile cues
that indicate adverse changes in handling characteristics, use of the
autopilot is prohibited when:
1. Unusual lateral trim is required while the airplane is in icing
conditions.
2. Autopilot trim warnings are encountered while the airplane is in icing
conditions.
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
L-42A
Aircraft General
Items on the emergency bus are:
Hydraulic pressure indication
Audio Panels
ADC1
AHRS1
CDU1
Windshield heat controllers
Primary pitch, aileron, rudder trims
Cabin Dump
Flood lights
PASS LIGHTS SAFETY
Rudder Bias
Transponder 1
PFD1
Display Control Panel (DCP1)
NAV1/COM1
Pitot/Static Heat 1 (pilot and standby)
Ground Spoilers
Secondary pitch trim
Low fuel annunciators
DCU CH B
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
AGI-1
Items on the emergency bus are:
Hydraulic pressure indication
Landing gear control and indication
Audio Panels
ADC1
AHRS1
CDU1
Windshield heat controllers
Speedbrakes
Primary pitch, aileron, rudder trims
Cabin Dump
Flood lights
PASS LIGHTS SAFETY
Flaps
Rudder Bias
Transponder 1
PFD1
Display Control Panel (DCP1)
NAV1/COM1
Pitot/Static Heat 1 (pilot and standby)
Ground Spoilers
Secondary pitch trim
Low fuel annunciators
DCU CH B
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
AGI-1A
Aircraft General
Items not on the converted bus are:
R Windshield Heat
R Landing Light
Radio Altimeter (and TCAS)
Logo Light
Beacon Light
Strobe Lights
Interior Power (and climate control)
COM 3/Datalink WX (optional)
DME 2
XM Weather
Stormscope (optional)
Satellite phone (optional)
HF 9000 (optional)
GPS 2 (optional)
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
AGI-2
Items not on the converted bus are:
R Windshield Heat
R Landing Light
Wing Inspection Light
Logo Light
Beacon Light
Strobe Lights
Interior Power (and climate control)
COM 3/Datalink WX (optional)
Radio Altimeter (and TCAS)
NAV 2
DME 2
XM Weather
Stormscope (optional)
Satellite phone (optional)
HF 9000 (optional)
GPS 2 (optional)
CE-525C CJ4
Revision 0.2
FOR TRAINING PURPOSES ONLY
AGI-2A