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limit and level off at 15,000 feet MSL. The flight crew must then retract the speed
brakes and landing gear and apply thrust to resume normal flight. If the airplane
slows to stall warning the autopilot will disconnect.
• The autopilot EDM is annunciated by a red EDM message in the PFD autopilot
status box. This mode can only be cancelled by disengaging the autopilot.
6. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MMO/VMO
7. Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMERGENCY
8. OXYGEN CONTROL VALVE Knob . . . . . . . . . . . . . . . . . . . . . DROP MASK (as required)
(make sure passengers are receiving oxygen)
9. PAX SAFETY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PAX SAFETY
10. ATC. . . . . . . . . . . . . . . . . . . . . . . . ADVISE AND OBTAIN LOCAL ALTIMETER SETTING
11. Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE
12. Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15,000 MSL or MINIMUM SAFE ALTITUDE
WARNING
It is the pilot's responsibility to determine Minimum Safe Altitude and to
ensure that the autopilot does not turn the airplane into traffic, terrain or
hazardous weather.
NOTE
• Refer to the Crew and Passenger Oxygen Duration Charts in Section III, Normal
Procedures, Figure 3-4 or 3-5 for the available oxygen supply.
• Further descent to 10,000 feet MSL is recommended to increase the available
oxygen supply time for the pilot and copilot.
13. Descend (if conditions permit) to 10,000 feet MSL.
14. Passenger Briefing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
15. Land as soon as possible.
PROCEDURE COMPLETED
3-30 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
TAIL CONE BLEED LEAK
(RED TAIL CONE BLD LK CAS MESSAGE)
Indicates that the tail cone temperature sensor has detected a tail cone temperature over 82ºC
(180ºF) which may indicate a bleed air leak or fire in the tailcone.
1. L and R Engine 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
510FM-07 AA 3-31
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
BATTERY OVER-TEMPERATURE
(RED BATTERY O’TEMP CAS MESSAGE)
Indicates that the battery temperature is above 71°C (160°F). If the message turns amber, it
indicates a battery temperature between 63°C and 71°C (145°F and 160°F).
NOTE
If battery amps decrease, and battery voltage is 1 volt less than generator voltage
within 30 seconds to 2 minutes, monitor BATTERY O’TEMP message.
• IF BATTERY VOLTS/AMPS DECREASE
4. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
IF BATTERY O’TEMP MESSAGE DOES NOT CLEAR OR
MESSAGE TURNS AMBER
5. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAVE OFF
6. Land as soon as possible.
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Citation Mustang airplane flight manual 1(39)
