Citation Mustang airplane flight manual 1(65)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

are inoperative.
1. Electrical Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE AS REQUIRED
(300A maximum <FL300 / 280A >FL300)
2. AIR COND Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. GEN Switch (affected side). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESET, THEN OFF
4. Generator Volts. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
• IF VOLTAGE IS APPROXIMATELY 28 VOLTS
5. GEN Switch (affected side). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
6. Generator Amps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY GENERATOR ON LINE
 IF GENERATOR DOES NOT COME ON LINE
7. GEN Switch (affected side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
8. Electrical Load . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR, REDUCE as required
(300A maximum FL300 / 280A > FL300)
CAUTION
To avoid the possibility of ice shedding from the inoperative windshield and
entering the engine, avoid entering or exit icing conditions as required.
NOTE
With one generator inoperative, the air-conditioner compressor and one windshield
controller will automatically turn off. Refer to Normal Procedures, WINDSHIELD
ANTI-ICE for additional information on single controller operation.
PROCEDURE COMPLETED
 IF GENERATOR COMES ON LINE
7. AIR COND Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
PROCEDURE COMPLETED
• IF VOLTAGE IS ABOVE 29 VOLTS OR LESS THAN 26 VOLTS
5. GEN Switch (affected side). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAVE OFF
6. Electrical Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR, REDUCE as required
(300A maximum FL300 / 280A > FL300)
PROCEDURE COMPLETED
510FM-07 AA 3-77/3-78

MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
FLIGHT CONTROLS
 ELECTRIC ELEVATOR TRIM INOPERATIVE
NOTE
This condition may be accompanied by a red AFCS or PTRM on the PFDs.
1. Move both halves of pilot and copilot trim switches to check for stuck switch.
2. AFCS Circuit Breaker (L circuit breaker panel). . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESET
• IF STILL INOPERATIVE
3. Manual Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
4. If unable to trim using manual trim wheel, refer to JAMMED ELEVATOR TRIM TAB
procedure.
NOTE
Autopilot and yaw damper may also be inoperative.
PROCEDURE COMPLETED
• IF OPERATIVE
PROCEDURE COMPLETED
 JAMMED ELEVATOR TRIM TAB
• DURING CRUISE
1. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN trim airspeed as long as practical
2. Land as soon as practical.
3. Descent. . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN a continuous descent to landing,
if possible, to minimize elevator force
4. Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
5. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
PROCEDURE COMPLETED
• TAKEOFF OR GO-AROUND
1. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE at safe altitude
2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 150 KIAS OR LESS
(Continued Next Page)
510FM-07 AA 3-79
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 JAMMED ELEVATOR TRIM TAB (Continued)
BEFORE LANDING
3. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
4. FLAP Handle . . . . . . . . . . . . . . . . . . . . LAND (TO/APR if STALL WARN HI displayed)
5. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VREF+10
6. Landing Distance / Weight:
CAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
 AILERON TRIM INOPERATIVE
1. AP/TRIM DISC Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
2. Either Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY opposite roll input
　
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