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WARNING
The current limiter on the side with the operating generator will most
likely fail when the engine start disengage button is pressed. This will
cause items powered by the crossfeed, battery, and opposite side
generator busses to lose power when the battery is disconnected with
only one generator available. Most avionics systems will remain
powered.
3. Speed Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT USE
4. Land as soon as practical. Refer to SINGLE ENGINE APPROACH AND LANDING,
LANDING GEAR WILL NOT EXTEND, HYD PRESS LO and FLAPS INOPERATIVE
APPROACH AND LANDING as required.
SHUTDOWN
5. PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET or Wheels - CHOCK
6. L and R GEN Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
7. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
8. Battery (in tailcone) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
9. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
10. STBY INST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
11. Ground Power Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT CONNECT
PROCEDURE COMPLETED
• IF STARTER DOES DISENGAGE
PROCEDURE COMPLETED
510FM-07 AA 3-55
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
ENGINE DOES NOT RESPOND TO THROTTLE MOVEMENT
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
2. FADEC RESET Switch . . . . . . . . . . . . . . . . . . . SELECT AFFECTED SIDE and RELEASE
• IF NO THROTTLE RESPONSE AND ENGINE OPERATION WITHIN
NORMAL LIMITS
3. Engine Instruments. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
4. Land as soon as practical.
5. Refer to Abnormal Procedures, ENGINE FAILURE/PRECAUTIONARY SHUTDOWN
procedure when required for descent, approach, landing, or taxi.
PROCEDURE COMPLETED
• IF ENGINE OPERATION OUTSIDE NORMAL LIMITS
3. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
4. Refer to Abnormal Procedures, ENGINE FAILURE/PRECAUTIONARY SHUTDOWN.
5. Land as soon as practical.
NOTE
The FADEC will command the fuel firewall shutoff valve to close during shutdown if
the engine does not respond to the normal shutdown command. This will result in the
F/W SHUTOFF L/R CAS message as appropriate.
PROCEDURE COMPLETED
• IF THROTTLE RESPONSE RETURNS TO NORMAL
PROCEDURE COMPLETED
HIGH SUSTAINED ITT DURING GROUND SHUTDOWN
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY CUTOFF
2. ENGINE START Button (affected side) . . . . . . . . . . . . . . . . . . . . . . . . PRESS momentarily
3. ENGINE START DISENG Button . . . . . . . . . . . . . . . . . . . . . . . . . PRESS after 15 seconds
PROCEDURE COMPLETED
3-56 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
OIL PRESSURE HIGH
(>170 PSI, AMBER OIL PRESS INDICATION)
NOTE
Oil pressure above 170 PSI is normal following engine start in cold conditions, until
the engine has warmed up. Refer to Normal Procedures, COLD WEATHER
OPERATIONS.
1. Throttle (affected engine) . . . . . . . . REDUCE to maintain oil pressure at or below 170 PSI
• IF THE INDICATION DOES NOT RESPOND OR INDICATION TURNS
RED
2. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
Refer to Abnormal Procedures, ENGINE FAILURE/PRECAUTIONARY SHUTDOWN.
PROCEDURE COMPLETED
• IF THE INDICATION RESPONDS BUT PRESSURE IS ABOVE 170 PSI
AT IDLE
2. Oil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
IF OIL TEMPERATURE INCREASES
3. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
Refer to Abnormal Procedures, ENGINE FAILURE/PRECAUTIONARY
SHUTDOWN.
NOTE
Engine damage may result from poor lubrication due to the high oil pressure and
temperature.
PROCEDURE COMPLETED
IF OIL TEMPERATURE IS NORMAL
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Citation Mustang airplane flight manual 1(57)
