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13. FUEL BOOST Switch (affected side) . . . . . . . . . . . . NORM (after engine stabilizes)
14. Engine Instruments/CAS Messages . . . . . . . . . . . . . . . . . . . . . . CHECK NORMAL
15. ENGINE ANTI-ICE and AIR COND Switches. . . . . . . . . . . . . . . . . . AS REQUIRED
16. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH
PROCEDURE COMPLETED
3-52 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 ENGINE START MALFUNCTION (ENGINE DOES NOT START)
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
2. ENGINE START DISENG Button . . . . . . . . . . . PRESS 15 seconds after throttle CUTOFF
• IF UNABLE TO ATTEMPT ANOTHER START
 ON GROUND
PROCEDURE COMPLETED
 IN FLIGHT
3. Land as soon as practical. Refer to Abnormal Procedures, ENGINE FAILURE/
PRECAUTIONARY SHUTDOWN.
PROCEDURE COMPLETED
• IF ABLE TO ATTEMPT ANOTHER START
 ON GROUND
3. Refer to Abnormal Procedures, DRY MOTORING prior to making another start
attempt.
PROCEDURE COMPLETED
 IN FLIGHT
3. Refer to Abnormal Procedures, INFLIGHT RESTART - ONE ENGINE
PROCEDURE COMPLETED
 DRY MOTORING
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
2. IGNITION Switch (affected side). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
3. ENGINE START Button (affected side) . . . . . . . . . . . . . . . . . . . . . . . . PRESS momentarily
Motor engine for desired duration (observe starter limits, refer to Operating Limitations,
START CYCLE LIMITATIONS)
4. ENGINE START DISENG Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
PROCEDURE COMPLETED
510FM-07 AA 3-53
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 ENGINE STARTER DOES NOT DISENGAGE (ENGINE START L
OR R SWITCH LIGHT ON AFTER ENGINE START)
1. ENGINE START DISENG Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
• IF STARTER DOES NOT DISENGAGE AND ENGINE START SWITCH
LIGHT REMAINS ILLUMINATED (START RELAY STUCK)
 ON GROUND
2. L and R GEN Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. BATTERY DISCONNECT Switch . . . . . . . . . . . LIFT GUARD AND DISCONNECT
4. Ground Power Unit (if connected) . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
5. Throttle(s) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
6. Battery (in tailcone). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
7. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
8. STBY INST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
9. Ground Power Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT RECONNECT
PROCEDURE COMPLETED
 IN-FLIGHT / START SUCCESSFUL
2. Land as soon as practical.
SHUTDOWN
3. PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
4. L and R GEN Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
5. BATTERY DISCONNECT Switch . . . . . . . . . . . LIFT GUARD AND DISCONNECT
6. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
7. Battery (in tailcone). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
8. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
9. STBY INST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
10. Ground Power Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DO NOT CONNECT
PROCEDURE COMPLETED
(Continued Next Page)
3-54 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 ENGINE STARTER DOES NOT DISENGAGE (ENGINE START L
OR R SWITCH LIGHT ON AFTER ENGINE START) (Continued)
 IN-FLIGHT / START ABORTED
2. BATTERY DISCONNECT Switch . . . . . . . . . . . LIFT GUARD AND DISCONNECT
　
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