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5. ENGINE FIRE Switch . . . . . CHECK OPEN (F/W SHUTOFF CAS message not displayed)
6. AIR COND Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
7. AIR SOURCE SELECT Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPERATING ENGINE
8. GEN Switch (affected side). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(Continued Next Page)
3-50 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
INFLIGHT RESTART - ONE ENGINE (Continued)
• WITH STARTER ASSIST (ALTITUDE 20,000 FEET OR LOWER)
9. FUEL BOOST Switch (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
10. ENGINE START Button (affected side). . . . . . . . . . . . . . . . . . . . . . PRESS momentarily
11. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
12. Engine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
a. Abort Start if no ITT rise within 10 seconds or ITT limit exceeded
b. Abort Start if stabilized flight idle is not achieved within 45 seconds
13. ENGINE START Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LIGHT EXTINGUISHED
IF ENGINE DOES NOT START
14. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
15. ENGINE START DISENG Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
16. FUEL BOOST Switch (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
17. FUEL TRANSFER Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
18. Refer to Abnormal Procedures, ENGINE FAILURE/PRECAUTIONARY
SHUTDOWN and SINGLE-ENGINE APPROACH AND LANDING.
PROCEDURE COMPLETED
IF ENGINE DOES START
14. GEN Switch (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GEN
15. Engine Instruments/CAS Messages . . . . . . . . . . . . . . . . . . . . . . CHECK NORMAL
16. ENGINE ANTI-ICE and AIR COND Switches. . . . . . . . . . . . . . . . . . AS REQUIRED
17. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH
NOTE
The engine may be accelerated once a stable idle has been achieved. However, to
reduce the potential for turbine blade rub, remain at idle for at least 2 minutes after
routine engine starts if the engine has been operated above idle during the prior 30
minutes.
PROCEDURE COMPLETED
(Continued Next Page)
510FM-07 AA 3-51
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
INFLIGHT RESTART - ONE ENGINE (Continued)
• WINDMILLING AIRSTART
(AIRSPEED 225 KIAS MINIMUM, ALTITUDE 15,000 FEET OR
LOWER, 4% N2 MINIMUM, RAT -10°C OR WARMER)
NOTE
Use of the windmill start procedure for training or routine in-flight starts is not
recommended.
9. FUEL BOOST Switch (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
10. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE at 4% N2 (minimum)
11. Engine Instruments. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
a. Abort start if no ITT rise within 10 seconds or ITT limit exceeded.
b. Abort start if stabilized flight idle is not achieved within 90 seconds.
CAUTION
• The FADEC will cycle fuel flow and ignition to accelerate N2 to 20% while
maintaining ITT within limits. ITT and N2 will increase in a stair-step
manner and ITT may briefly exceed 830ºC. Once N2 reaches 20%, the
cycling should stop and the ITT should smoothly increase until peaking. If
ITT exceeds a start limit during this portion of the start sequence, the start
must be manually terminated.
• If the airspeed decreases below 225 KIAS during the windmill start
sequence, the start attempt should be terminated.
IF ENGINE DOES NOT START
12. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
13. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
14. Refer to the WITH STARTER ASSIST bullet in this procedure, or Abnormal
Procedures ENGINE FAILURE/PRECAUTIONARY SHUTDOWN, or SINGLEENGINE
APPROACH AND LANDING.
PROCEDURE COMPLETED
IF ENGINE DOES START
12. GEN Switch (affected side). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GEN
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Citation Mustang airplane flight manual 1(55)
