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4. FUEL BOOST Switch (affected side) - - - - - - - - - - - -OFF THEN NORM
 IF ENGINE FIRE LIGHT REMAINS ON (30 SECONDS)
5. Illuminated BOTTLE ARMED Switch - - - - - - - - - - - - - - - - - -PUSH
(BOTTLE ARMED Light goes off)
O IF ENGINE FIRE LIGHT REMAINS ON OR SECONDARY FIRE
INDICATIONS ARE PRESENT
6. Land as soon as possible.
7. Accomplish SINGLE-ENGINE APPROACH AND LANDING; Tab
AB2.
PROCEDURE COMPLETED
(Continued Next Page)
2  ENGINE FAILURE DURING APPROACH (POSSIBLE ENGINE
FAIL L-R CAS MESSAGE)
1. Throttle (operating engine)- - - - - - - - - - - - - - - - - - - - - - - - - - INCREASE
as required
2. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VAPP
3. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -TO/APR
STALL WARNING - NORMAL Multiply normal FLAP LAND landing distance by 1.12.
STALL WARNING - HIGH Use normal FLAP TO/APR landing distance.
3  ENGINE FIRE L OR R (ENGINE FIRE WARNING LIGHT
ILLUMINATED)
1. Throttle (affected engine)- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE
• IF LIGHT REMAINS ON (15 SECONDS)
2. Illuminated ENGINE FIRE Switch- - - - - - - - - LIFT COVER AND PUSH
A
510CLEAP-07 AA 11
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
 ENGINE FIRE L OR R (ENGINE FIRE WARNING LIGHT
ILLUMINATED) (Continued)
O IF ENGINE FIRE LIGHT GOES OUT AND SECONDARY FIRE
INDICATIONS ARE NOT PRESENT
6. Rotary Test - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FIRE WARN
(ENG FIRE LIGHTS should both illuminate)
7. Land as soon as practical.
8. Refer to ENGINE FAILURE/PRECAUTIONARY SHUTDOWN;
Tab B1.
PROCEDURE COMPLETED
 IF ENGINE FIRE LIGHT GOES OUT AND SECONDARY FIRE
INDICATIONS ARE NOT PRESENT
5. Rotary Test - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FIRE WARN
(ENG FIRE LIGHTS should both illuminate).
O IF BOTH ENGINE FIRE LIGHTS ILLUMINATE
6. Land as soon as practical.
7. Refer to ENGINE FAILURE / PRECAUTIONARY SHUTDOWN;
Tab B1.
PROCEDURE COMPLETED
O IF ENGINE FIRE LIGHT ON AFFECTED SIDE DOES NOT
ILLUMINATE (POSSIBLE DAMAGE TO FIRE SENSOR)
6. Refer to ENGINE FIRE LIGHT REMAINS ON (30 SECONDS),
this procedure.
PROCEDURE COMPLETED
• IF ENGINE FIRE LIGHT GOES OUT - ENGINE AT IDLE - (PROBABLE
BLEED AIR LEAK)
2. Rotary Test - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FIRE WARN
(ENG FIRE LIGHTS should both illuminate)
 IF BOTH ENGINE FIRE LIGHTS ILLUMINATE
3. Throttle (affected engine) - - - - - - - - - - - - - - - - - - - -AS REQUIRED
4. Land as soon as practical.
PROCEDURE COMPLETED
 IF ENGINE FIRE LIGHT ON AFFECTED SIDE DOES NOT
ILLUMINATE (POSSIBLE DAMAGE TO FIRE SENSOR)
3. Illuminated ENGINE FIRE Switch - - - - - - - LIFT COVER and PUSH
4. Illuminated BOTTLE ARMED Switch- - - - - - - - - - - - - - - - - - PUSH
5. Throttle (affected side)- - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF
6. FUEL BOOST Switch (affected side)- - - - - - - - - - -OFF then NORM
O IF SECONDARY FIRE INDICATIONS ARE PRESENT
7. Land as soon as possible.
8. Accomplish SINGLE-ENGINE APPROACH AND LANDING; Tab
AB2.
O IF SECONDARY FIRE INDICATIONS ARE NOT PRESENT
7. Land as soon as practicle.
8. Refer to ENGINE FAILURE/PRECAUTIONARY SHUTDOWN;
Tab B1.
PROCEDURE COMPLETED
A
12 AA 510CLEAP-07
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
(Refer to Tab A5 for Airstart Envelope)
• EMERGENCY RESTART - STARTER ASSIST (ALTITUDE 20,000 FEET
OR LOWER)
5. ENGINE ANTI-ICE Switches - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
6. AIR COND Switch- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
7. Opposite Engine (after first start complete or aborted) - - - - - - - - - - START
(repeat steps 4-5)
WARNING
• Emergency Battery 30-minute duration is based on a maximum of two
starter-assist start attempts. Additional starter-assist start attempts
will cause battery power to be depleted prematurely.
• The battery switch may remain in the BATT position for a maximum of
2 minutes while attempting restarts. Exceeding 2 minutes will reduce
the battery capacity available to power the Emergency Bus items.
 IF NEITHER ENGINE STARTS
8. BATT Switch - - - - - - - - - - - - - - - - - - - - RAPIDLY SELECT EMER
9. Refer to Emergency Procedures, MAXIMUM GLIDE - EMERGENCY
LANDING; Tab A6.
PROCEDURE COMPLETED
　
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