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Continuous pump operation can result in overheating and shutdown of the pump.
• IF LANDING GEAR HANDLE IS UP
1. Landing Gear UNLOCK light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
 IF UNLOCK LIGHT ILLUMINATED
2. AIRSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BELOW 140 KIAS
3. Rudder Input . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMIZE
4. LDG GEAR CONTROL Circuit Breaker (L circuit breaker panel) . . . . . . . . . CHECK
5. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE DOWN then UP
O IF LANDING GEAR DOES NOT RETRACT
6. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
7. Landing Gear Downlock Lights . . . . . . . . . . . . . . . VERIFY ALL ILLUMINATED
8. HYD PUMP ON message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY OFF
9. Land as soon as practical.
PROCEDURE COMPLETED
O IF LANDING GEAR RETRACTS (UNLOCK LIGHT OUT)
6. HYD PUMP ON message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY OFF
PROCEDURE COMPLETED
 IF UNLOCK LIGHT NOT ILLUMINATED
2. HYD PUMP circuit breaker (L Circuit Breaker panel) . . . . . . . . . . . . . . . . . . . . . PULL
3. Reset HYD PUMP Circuit Breaker prior to landing.
PROCEDURE COMPLETED
• IF LANDING GEAR HANDLE IS DOWN
ON GROUND
1. BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY
2. PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
3. HYD PUMP Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . . . . . . . PULL
4. Wheels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHOCK
5. Correct prior to flight.
PROCEDURE COMPLETED
IN FLIGHT
1. HYD PUMP Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . . . . . . . PULL
2. Reset HYD PUMP Circuit Breaker prior to landing.
PROCEDURE COMPLETED
3-116 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 WOW MISCOMPARE (WEIGHT-ON-WHEELS MISCOMPARE)
Indicates the weight-on-wheels switches do not indicate the same condition – either on-ground or
in-air. The following systems or equipment may not operate normally:
• Engine will default to Flight Idle (Ground Idle not available).
• Antiskid touchdown protection is not available.
• Landing gear will not retract.
• ON GROUND
1. Correct prior to flight.
PROCEDURE COMPLETED
• IN FLIGHT
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
CAUTION
The touchdown protection feature of the antiskid system is inoperative when
either squat switch indicates the airplane is on the ground. Normal antiskid and
power braking will be available once the aircraft is back on the ground even if
only one squat switch indicates on the ground.
PROCEDURE COMPLETED
510FM-07 AA 3-117/3-118

MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
ABNORMAL LANDING
 SINGLE-ENGINE APPROACH AND LANDING
APPROACH
1. Landing Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE the following landing data:
a. Airspeed:
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 and STALL
WARNING-NORMAL performance and procedures can be used.
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
　
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本文鏈接地址：Citation Mustang airplane flight manual 1(80)