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until landing assured then slow to VREF
C A U T I O NCAUTION
Use of differential braking may be required for directional control upon landing.
PROCEDURE COMPLETED
1  LANDING WITH FAILED PRIMARY FLIGHT CONTROL
STALL
WARNING
FLAPS *MULTIPLY LANDING
DISTANCE BY
*REDUCE MAX LANDING
WEIGHT BY
NORMAL LAND 1.28 50 lbs.
HIGH TO/APR 1.22 40 lbs.
* Basic landing distance and maximum landing weight values must be obtained from the
appropriate landing performance charts based on the STALL WARNING and ANTI-ICE system
settings.
84 AA 510CLEAP-07
AD
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
This procedure should be used anytime there is an abnormal buildup of ice on the
leading edge of the wing. This may be caused by a failure of the de-ice boot system or
an unusually heavy accumulation of ice.
1. Landing Data - Use the following landing data (Landing Flaps limited to
TO/APR):
a. Airspeed:
VREF (KIAS) - STALL WARNING HIGH
b. Landing Distance/Weight:
(1) MULTIPLY STALL WARNING-HIGH landing distance by 1.22.
(2) REDUCE maximum landing weight by 40 lbs.
C A U T I O NCAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
2  LANDING WITH ICE ON WING LEADING EDGE
FLAPS WEIGHT - POUNDS
6000 6500 7000 7500 8000 8645
TO/APR 108 112 115 119 122 127
* Use in an emergency which requires landing at weights in excess of 8000 pounds.
510CLEAP-07 AA 85
AD
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
APPROACH
1. Select an airport with a straight-in ILS approach or a GPS/RNAV approach
with vertical guidance.
2. Landing Data - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CONFIRM
C A U T I O NCAUTION
Avoid landing with a tailwind.
3. Seats and Seat Belts - - - - - - - - - - - - - - - - - - - - - ADJUST AND SECURE
4. Avionics and Flight Instruments - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
5. Minimums - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -SET
6. Passenger Seats- - - - - - - - - - - - - - - - - - - - - - - -CHECK FULL UPRIGHT
7. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - PAX SAFETY
8 FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
9. Anti-Ice/Deice Systems - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
10. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - TO/APR (as required)
11. ANTISKID Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON
12. LANDING Light Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON
13. CAS Messages - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
14. Crew Briefing - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPLETE
(Include visibility call-outs, GO-AROUND,
and landing flap setting)
BEFORE LANDING
15. LANDING GEAR Handle - - - - - - - - - - - - - - - - - - - DOWN AND LOCKED
16. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TO/APR
17. Pressurization- - - - - - - - - - - - - - - - - - - - - CHECK ZERO DIFFERENTIAL
18. Autopilot/Yaw Damper - - - - - - - - - - - - - - - OFF (50 feet above minimums)
19. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VREF
20. Slip - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
to obtain and maintain runway visibility
21. Speed Brakes - - - - - - - - - - - - - - - - - RETRACT PRIOR TO 50 FEET AGL
PROCEDURE COMPLETED
1  WINDSHIELD A/I INOPERATIVE APPROACH AND LANDING
86 AA 510CLEAP-07
AE
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
Indicates that the tailcone baggage door is not locked.
• ON GROUND
1. Correct prior to flight. Secure baggage door if open, unlatched, or
unlocked.
PROCEDURE COMPLETED
• IN FLIGHT
1. Land as soon as practical.
PROCEDURE COMPLETED
Indicates the cabin door is not fully closed, latched and locked. Switches are located
on the inside handle, door pin mechanism, and the door frame.
• ON GROUND
1. Open the cabin door and close again.
2. Ensure inside handle is fully seated in the locked position.
3. Verify CAS message clears.
PROCEDURE COMPLETED
• IN FLIGHT
1. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - REDUCE
2. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - - - - - - PAX SAFETY
　
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