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FLAPS STALL
WARNING
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
UP or
UNKNOWN
NORMAL
HIGH
98
110
102
114
106
118
109
122
113
126
117
131
TO/APR NORMAL
HIGH
87
98
91
102
95
105
98
109
101
112
105
117
LAND NORMAL 82 85 88 91 94 98
*Use in an emergency which requires landing at weights in excess of 8000 pounds.
Flaps UP or UNKNOWN MULTIPLY appropriate STALL WARNING-NORMAL or
HIGH landing distance by 2.31.
Flaps TO/APR MULTIPLY appropriate STALL WARNING-NORMAL or
HIGH landing distance by 2.10.
Flaps LAND MULTIPLY appropriate landing distance by 1.83.
510CLEAP-07 AA 15
A
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
 MAXIMUM GLIDE - EMERGENCY LANDING (Continued)
C A U T I O NCAUTION
• Avoid landing with a tailwind.
• Landing above 8000 feet MSL with flaps UP may exceed brake
energy limits.
2. Crew Briefing - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPLETE
3. Seats and Seat Belts- - - - - - - - - - - - - - - - - - - - ADJUST and SECURE
4. Avionics and Flight Instruments - - - - - - - - - - - - - - - - - - - - - - - CHECK
5. PAX SAFETY Switch- - - - - - - - - - - - - - - - - - - - - - - - - - - PAX SAFETY
6. Passenger Briefing - - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPLETE
7. Passenger Seats - - - - - - - - - - - - - - - - - - - - -CHECK FULL UPRIGHT
8. LANDING GEAR - - - - - - - - - - - - - - - - - - - - - EMERGENCY EXTEND
a. LDG GEAR CONT Circuit Breaker - - - - - - - - - - - - - - - - - - -PULL
(L circuit breaker panel)
b. LANDING GEAR Handle - - - - - - - - - - - - - - - - - - - - - - - - -DOWN
c. EMERGENCY GEAR RELEASE Cover - - - - - - - - - - - - REMOVE
d. EMERGENCY GEAR RELEASE T-Handle - - - - - - - - -PULL AND
ROTATE TO LOCK
e. EMERGENCY GEAR RELEASE Knob - - - - - - - -PULL TO BLOW
DOWN (for positive lock)
f. Landing Gear - - - - - - - - - - - - - - - CHECK DOWN AND LOCKED
(3 green lights)
C A U T I O NCAUTION
• Prior to using the emergency extension system, the landing gear handle
must be down and/or the gear control circuit breaker pulled to prevent
possible energizing of the gear hydraulic system to the retract position.
• Once the emergency gear extension system has been used, do not
attempt to retract the landing gear.
9. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VREF
10. Pressurization - - - - - - - - - - - - - - - ZERO DIFFERENTIAL PRESSURE
at touchdown (use CABIN DUMP switch if required)
LANDING
11. Brake Pedals - - - - - - - - - - - -REMOVE FEET FROM BRAKE PEDALS
12. EMERGENCY BRAKE Handle- - - - - - SMOOTH PULL AS REQUIRED
(Continued Next Page)
A
16 AA 510CLEAP-07
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
 MAXIMUM GLIDE - EMERGENCY LANDING (Continued)
C A U T I O NCAUTION
• Antiskid system does not function during emergency braking. Excessive
pressure on emergency brake handle can cause both wheel brakes to lock,
resulting in blowout of both tires.
• Repeated application and release of the emergency brake handle
may cause premature loss of pneumatic pressure.
• After landing, clear the runway and stop. Do not attempt to taxi onto
the ramp using emergency brakes.
13. Directional Control - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MAINTAIN
with nosewheel steering
PROCEDURE COMPLETED
3. Refer to ENGINE FAILURE / PRECAUTIONARY SHUTDOWN; Tab B1.
• IF ENGINE SURGING STOPS
2. Throttle (affected engine) - - - - - - - - - - - - - - INCREASE CAUTIOUSLY
3. Engine Instruments- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR
4. Throttles - - - - - - - - - - - - - - - - - - - - RESUME NORMAL OPERATION
PROCEDURE COMPLETED
1. Throttle (affected engine)- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE
• IF POINTER AND DIGITS CHANGE TO AMBER OR GREEN
2. Throttle (affected engine) - - - - - - - - - - - - - - - - -MAINTAIN REDUCED
POWER AS REQUIRED
3. Land as soon as practical.
PROCEDURE COMPLETED
• IF POINTER AND DIGITS RETURN TO RED OR REMAIN RED FOR
MORE THAN 15 SECONDS
2. Throttle (affected engine) - - - - - - - - - - - - - - - - - - - - - - - - - - -CUTOFF
3. Accomplish ENGINE FAILURE/PRECAUTIONARY SHUTDOWN; Tab
B1.
PROCEDURE COMPLETED
7  ENGINE SURGES OR UNSTABLE ENGINE OPERATION
1. Throttle (affected engine)- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE
　
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