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1. Land as soon as practical.
2. LANDING GEAR Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - -DOWN
3. CABIN DUMP Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DUMP
(if Cabin Differential Pressure not zero)
4. Make sure brakes are not applied during touchdown.
5. Brakes- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - APPLY NORMALLY
after touchdown
PROCEDURE COMPLETED
1  WOW MISCOMPARE (WEIGHT-ON-WHEELS MISCOMPARE)
80 AA 510CLEAP-07
AB
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
APPROACH
1. Landing Data - Use the following landing data:
a. Airspeed:
VREF (KIAS)
b. Landing Distance:
2. Seats and Seat Belts - - - - - - - - - - - - - - - - - - ADJUST AND SECURE
3. Avionics and Flight Instruments - - - - - - - - - - - - - - - - - - - - - - - CHECK
4. Minimums - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - SET
5. Passenger Seats - - - - - - - - - - - - - - - - - - - - - CHECK FULL UPRIGHT
6. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - - - - - - PAX SAFETY
7. FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
8. Anti-Ice/Deice Systems- - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED
9. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - TO/APR (as required)
10. ANTISKID Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ON
11. LANDING Light Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ON
12. CAS Messages - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
13. Crew Briefing - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPLETE
(Include SINGLE-ENGINE GO-AROUND; Tab AC1.)
BEFORE LANDING
14. LANDING GEAR Handle- - - - - - - - - - - - - - - - - -DOWN AND LOCKED
15. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TO/APR
16. Pressurization - - - - - - - - - - - - - - - - - - CHECK ZERO DIFFERENTIAL
17. Autopilot and Yaw Damper - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
18. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VREF
19. Speed Brakes - - - - - - - - - - - - - - RETRACT PRIOR TO 50 FEET AGL
20. Refer to SINGLE-ENGINE GO AROUND; Tab AC1, if required.
C A U T I O NCAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
2  SINGLE-ENGINE APPROACH AND LANDING
FLAPS STALL
WARNING
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
TO/APR NORMAL
HIGH
87
98
91
102
95
105
98
109
101
112
105
117
* Use in an emergency which requires landing at weights in excess of 8000 pounds.
STALL WARNING - NORMAL Multiply normal Flap LAND landing distance by 1.12.
STALL WARNING - HIGH Use normal Flap TO/APR landing distance.
510CLEAP-07 AA 81
AB
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
1. Throttle (operating engine) - - - - - - - - - - - - - - - - - - - - - - - - - - TO DETENT
(Thrust Mode Indicator - green T/O)
2. Go-Around Button (either throttle) - - - - - - - - - - - - - - - - - - - - - - - - PRESS
3. Airplane Pitch Attitude - - - - - - - - - - - - - - - - - - - - - - - - - - - - 8° INITIALLY
(go-around pitch command) then AS REQUIRED
4. AP/TRIM DISC Button - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - PRESS
(if required to turn off Yaw Damper)
5. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TO/APR
6. Climb Speed- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VAPP MINIMUM
7. LANDING GEAR Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -UP
(when positive rate of climb is established)
8. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - UP AT VAPP +10 knots
(when clear of obstacles)
9. Airspeed - - - - - - - - - - - - - - - - - - - - -ACCELERATE TO VENR (118 KIAS)
10. Throttle (operating engine) - - - - - - - - - - - - - - CLB DETENT or as required
11. YD or AP Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -AS REQUIRED
12. Land as soon as possible. Refer to ENGINE FAILURE/ PRECAUTIONARY
SHUTDOWN; Tab B1, and/or SINGLE-ENGINE APPROACH AND
LANDING; Tab AB2.
PROCEDURE COMPLETED
APPROACH
1. Landing Data - Refer to the following tables:
VREF (KIAS)
LANDING DISTANCE
(Continued Next Page)
1  SINGLE-ENGINE GO-AROUND
2  FLAPS INOPERATIVE APPROACH AND LANDING (FLAPS
NOT IN LANDING POSITION)
　
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