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2. Refer to Abnormal Procedures, INFLIGHT RESTART - ONE ENGINE or ENGINE
FAILURE/PRECAUTIONARY SHUTDOWN.
PROCEDURE COMPLETED
ENGINE FAILURE DURING APPROACH
(POSSIBLE ENGINE FAIL L-R CAS MESSAGE)
4. RUDDER TRIM . . . . . . . . . . . . . . . . . . . . . . . TRIM toward operating engine (as required)
5. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
6. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN and LOCKED
NOTE
It is recommended to land with flaps in the TO/APR position when single engine. Use
of flaps in the LAND position (and corresponding normal speed and distance data) is
permitted only if shorter landing performance is required when landing and STALL
WARNING-NORMAL performance data is being used.
7. Landing Distance:
WHEN LANDING ASSURED
8. Pressurization. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK ZERO DIFFERENTIAL
9. Autopilot and Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (at or above minimums)
10. Speed brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT PRIOR TO 50 FEET AGL
11. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VAPP
CAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
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.
3-8 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
ENGINE FIRE L OR R
(ENGINE FIRE WARNING LIGHT ILLUMINATED)
NOTE
The red ENGINE FAIL CAS message for the affected engine will be displayed when
the engine is shut down using the ENGINE FIRE switch while the throttle is at or
above the idle position. This message will clear when the throttle is moved to
CUTOFF.
3. Throttle (affected engine). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
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 Abnormal Procedures, SINGLE-ENGINE APPROACH AND
LANDING.
PROCEDURE COMPLETED
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 Abnormal Procedures, ENGINE FAILURE / PRECAUTIONARY
SHUTDOWN.
PROCEDURE COMPLETED
(Continued Next Page)
1. Throttle (affected engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
• IF LIGHT REMAINS ON (15 SECONDS)
2. Illuminated ENGINE FIRE Switch . . . . . . . . . . . . . . . . . . . . . LIFT COVER and PUSH
510FM-07 AA 3-9
SECTION III - OPERATING PROCEDURES MODEL 510
EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
ENGINE FIRE L OR R
(ENGINE FIRE WARNING LIGHT ILLUMINATED) (Continued)
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 Abnormal Procedures, ENGINE FAILURE / PRECAUTIONARY
SHUTDOWN.
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
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Citation Mustang airplane flight manual 1(28)
