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there is an internal failure of the pressurization controller.
1. PRESS CONT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - VERIFY NORM
• IF MESSAGE DOES NOT CLEAR
2. Cabin altitude, differential pressure,
and rate indications - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR
3. PRESS CONT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - STANDBY
(if cabin pressure not stable)
IF CABIN ALTITUDE INCREASING (RED CABIN ALTITUDE IS
DISPLAYED)
4. Consider emergency descent if required. Refer to EMERGENCY
DESCENT, Tab F3.
PROCEDURE COMPLETED
IF CABIN ALTITUDE DECREASING
4. Cabin Differential Pressure - - - - - - - - - - - - - - - - - - - - - MONITOR
Refer to OVERPRESSURIZATION (>8.5 PSI); Tab H2, if 8.5 PSI
is exceeded.
PROCEDURE COMPLETED
IF INDICATIONS ARE STABLE
4. Pressurization Instruments - - - - - - - - - - CONTINUE TO MONITOR
5. Land as soon as practical.
BEFORE LANDING
6. CABIN DUMP Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - DUMP
(if Cabin Differential Pressure not zero)
PROCEDURE COMPLETED
3 PRESS CTRL – AMBER (PRESSURIZATION CONTROL
FAULT)
510CLEAP-07 AA 41
I
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
Indicates that the tail cone temperature sensor has detected a tail cone temperature
over 82°C (180°F) which may indicate a bleed air leak or fire in the tailcone.
1. Left and Right ITT - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - NOTE
2. Throttle (engine with highest ITT) - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE
(If unable to determine a higher ITT, start procedure by retarding the left
engine to IDLE.)
• IF CAS MESSAGE EXTINGUISHES (INDICATES POSSIBLE BLEED
LEAK FROM IDLE ENGINE)
3. Throttle - - - - - - - - - - - - - - - - - - - - - - - MAINTAIN REDUCED POWER
(to keep message extinguished)
4. Land as soon as practical.
PROCEDURE COMPLETED
• IF MESSAGE DOES NOT CLEAR
3. Throttle (idle engine) - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
4. Throttle (opposite engine) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE
IF CAS MESSAGE CLEARS (INDICATES POSSIBLE BLEED LEAK
FROM IDLE ENGINE)
5. Throttle - - - - - - - - - - - - - - - - - - - - MAINTAIN REDUCED POWER
(to keep message extinguished)
6. Land as soon as practical.
PROCEDURE COMPLETED
IF CAS MESSAGE STILL DOES NOT CLEAR (INDICATES
POSSIBLE TAILCONE/BAGGAGE FIRE OR MAJOR BLEED LEAK)
5. Use minimum symmetric power as required for descent and landing.
Consider the potential of baggage or tailcone fire and subsequent
need for emergency evacuation after landing.
6. Land as soon as possible.
PROCEDURE COMPLETED
1 TAIL CONE BLEED LEAK (RED TAIL CONE BLD LK CAS
MESSAGE)
42 AA 510CLEAP-07
J
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
6. AIR COND Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
7. FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
8. Exit icing environment if required.
9. Land as soon as possible (within 30 minutes). Refer to BEFORE
LANDING, this procedure.
WARNING
With the battery switch in EMER, wing and tail deice systems will be
inoperative. Avoid entering or exit icing conditions as required. STALL
WARNING-HIGH landing data is provided and must be used in the event
any ice remains on the wings and/or tail during approach and landing.
• IF ONLY ONE GENERATOR COMES ON LINE
4. Electrical Load - - - - - - - - - - - - - - - - - - - - - - REDUCE AS REQUIRED
(300A FL300 / 280A > FL300)
5. Land as soon as practical.
PROCEDURE COMPLETED
• IF BOTH GENERATORS COME ON LINE
PROCEDURE COMPLETED
BEFORE LANDING
1. Landing Data - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CONFIRM
a. Airspeed
VREF (KIAS)
(Continued Next Page)
2 DUAL GENERATOR FAILURE (RED GEN OFF L-R CAS
MESSAGE)
1. L and R GEN Switches - - - - - - - - - - - - - - - - - - - - - - - RESET THEN OFF
2. Generator Voltages - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
3. L and R GEN Switches - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON
• IF NEITHER GENERATOR COMES ON LINE
4. AP/TRIM DISC Button - - - - - - - - - - - - - - - - - - - - - - - - - - - - - PRESS
5. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - RAPIDLY SELECT EMER
FLAPS STALL
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Citation Mustang checklist EMERGENCY/ABNORMAL PROCEDURES(23)
