曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

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 Abnormal Procedures, SINGLE-ENGINE GO-AROUND)
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 Abnormal Procedures, SINGLE-ENGINE GO-AROUND if required.
CAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
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 lbs.
STALL WARNING-NORMAL MULTIPLY normal Flap LAND landing distance by 1.12.
STALL WARNING-HIGH Use normal Flap TO/APR landing distance.
510FM-07 AA 3-119
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 SINGLE-ENGINE GO-AROUND
1. Throttle (operating engine) . . . . . . . . . . . TO DETENT (Thrust Mode Indicator - green T/O)
2. Go-Around Button (either throttle) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
NOTE
The flight director go-around mode is recommended to establish the initial climb pitch
attitude reference. Pressing the throttle mounted go-around button disengages the
autopilot, and engages the flight director go-around mode (wings level, +8pitch).
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 (when positive rate of climb is established) . . . . . . . . . . . . . . . UP
NOTE
Reducing the throttle of the operating engine below approximately 70% N2 will trigger
the gear warning horn. If the STALL WARN HI message is displayed, this warning
cannot be cancelled until the landing gear is extended, the flaps are retracted, or the
throttle increased above approximately 85% N2.
8. FLAP Handle (when clear of obstacles) . . . . . . . . . . . . . . . . . . . . . . . UP at VAPP +10 knots
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 Abnormal Procedures, ENGINE FAILURE/
PRECAUTIONARY SHUTDOWN and/or SINGLE ENGINE APPROACH AND LANDING.
PROCEDURE COMPLETED
3-120 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 FLAPS INOPERATIVE APPROACH AND LANDING
(FLAPS NOT IN LANDING POSITION)
APPROACH
1. Landing Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refer to the following tables:
　
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