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• IF ENGINE CONTINUES TO SURGE AND/OR ITT EXCEEDS LIMIT
2. Throttle (affected engine) - - - - - - - - - - - - - - - - - - - - - - - - - - -CUTOFF
8  OIL PRESS LO L-R (LOW OIL PRESSURE, RED POINTER AND
DIGITS)
A
510CLEAP-07 AA 17
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
1. Throttle (affected engine) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF
C A U T I O NCAUTION
• If possible, the engines should remain at idle for a minimum of two minutes
prior to shutdown to allow the engine inter-turbine temperatures to stabilize
and avoid turbine blade rub.
• If the engine windmills for more than 15 minutes without a positive
indication of oil pressure, a notation is required in the engine
logbook and the engine must be inspected in accordance with the
pratt and whitney engine maintenance manual.
• If the engine windmills for more than 15 minutes with the firewall
shutoff closed or the boost pump turned off, the engine fuel pump
must be inspected in accordance with the Pratt and Whitney Engine
Maintenance Manual.
2. GEN Switch (affected side) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
3. IGNITION Switch (affected side) - - - - - - - - - - - - - - - - - - - - - - - - - - - NORM
4. Electrical Load - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REDUCE as required
(300A maximum FL300 / 280A > FL300)
5. Fuel TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
• IF ENGINE FIRE HAS OCCURRED (FIRE EXTINGUISHED, SECURE
ENGINE)
6. Verify ENGINE FIRE switch (affected side) is pushed (appropriate F/W
SHUTOFF L-R CAS message is displayed).
7. Land as soon as practical. Refer to Abnormal Procedures, SINGLEENGINE
APPROACH AND LANDING; Tab AB2.
PROCEDURE COMPLETED
• PRECAUTIONARY ENGINE SHUTDOWN (NO ENGINE FIRE)
6. Verify ENGINE FIRE switch is not depressed and firewall shutoff is open
(no F/W SHUTOFF CAS message).
7. FUEL BOOST Switch (affected side) - - - - - - - - - - - - - - - - - - - - - - ON
8. Land as soon as practical. Refer to Abnormal Procedures, SINGLEENGINE
APPROACH AND LANDING; Tab AB2.
PROCEDURE COMPLETED
1  ENGINE FAILURE/PRECAUTIONARY SHUTDOWN
B
18 AA 510CLEAP-07
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
1. Altitude - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BELOW 20,000 FEET
(Refer to Tab A5 for Airstart Envelope)
C A U T I O NCAUTION
Do not attempt to restart an engine if it is possible that ice has formed in the engine
or engine inlet. Significant damage to the engine can occur.
2. Throttle (affected engine)- - - - - - - - - - - - - - - - - - - - - - - - - - - - - -CUTOFF
3. FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
4. ENGINE ANTI-ICE (affected side) - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
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
• 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 ENGINE FAILURE / PRECAUTIONARY SHUTDOWN; Tab
B1, and SINGLE-ENGINE APPROACH AND LANDING; Tab AB2.
PROCEDURE COMPLETED
 IF ENGINE DOES START
14. GEN Switch (affected side) - - - - - - - - - - - - - - - - - - - - - - - - - -GEN
15. Engine Instruments/CAS Messages - - - - - - - - - -CHECK NORMAL
　
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