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EMERGENCY PROCEDURES
FAA APPROVED
U.S. Configuration
 MAXIMUM GLIDE - EMERGENCY LANDING (Continued)
WARNING
Wing and tail deice systems will be inoperative. Avoid entering or exit
icing conditions as required. STALL WARNING-HIGH landing data is
provided and must be used in the event any ice remains on the wings
and/or tail during approach and landing.
NOTE
• With no generator online and the BATT switch in EMER, the battery will supply DC
power to the emergency bus equipment for approximately 30 minutes, provided
EMER is selected within 1 minute after failure of the second generator.
• The battery switch must be moved from BATT to EMER within 1 second to
maintain adequate avionics power. If the switch is moved slowly, the PFD, AHRS,
ADC, and other devices may need to re-initialize.
• ENG CTRL SYS L-R message will display due to loss of normal aircraft DC power
to the FADEC’s. Engine operation will not be degraded and no pilot action is
required.
• Flap system will be inoperative. Plan to land with the flap position set when EMER
selected.
• Normal gear extend will be inoperative. Plan to use emergency extension and
blow-down.
• Power brakes and antiskid will be inoperative. Plan to use emergency brake
system for landing.
• The exterior lighting and transponder will be inoperative. Advise Air Traffic
Control.
• Windshield anti-ice and defog will be inoperative.
• Master Warning and Master Caution lights will be inoperative. However, the pressto-
reset function will still work to acknowledge flashing EICAS messages.
• Avionics audio warnings including Altitude Alert, Decision Height (BARO only),
Marker Beacon, TAWS, and Vertical Track will be functional. Aircraft generated
tones including Overspeed, Landing Gear, and Stall Warning will be inoperative.
• The AP button on the autopilot control panel may be pressed two times to cancel
the autopilot disconnect tone if required.
(Continued Next Page)
3-16.1 AE 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
EMERGENCY PROCEDURES
FAA APPROVED
Configuration U.S.
 MAXIMUM GLIDE - EMERGENCY LANDING (Continued)
BEFORE LANDING
1. Landing Data. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
a. Airspeed
VREF (KIAS)
b. Landing Distance:
CAUTION
• Avoid landing with a tailwind.
• Landing above 8000 feet MSL with flaps up may exceed brake energy
limits.
2. Crew Briefing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
3. Seats and Seat Belts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST and SECURE
4. Avionics and Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
5. PAX SAFETY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PAX SAFETY
6. Passenger Briefing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
7. Passenger Seats. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FULL UPRIGHT
8. LANDING GEAR. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMERGENCY EXTEND
a. LDG GEAR CONT Circuit Breaker (left circuit breaker panel) . . . . . . . . . . . . PULL
b. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
c. EMERGENCY GEAR RELEASE Cover . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE
d. EMERGENCY GEAR RELEASE T-Handle . . . . . . PULL AND ROTATE TO LOCK
e. EMERGENCY GEAR RELEASE Knob. . . . . . . . . . . . . . . PULL TO BLOW DOWN
(for positive lock)
f. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK DOWN and LOCKED
(3 green lights)
(Continued Next Page)
FLAPS STALL
WARNING
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
UP or
UNKNOWN
NORMAL
HIGH
98
110
102
114
106
118
109
122
113
126
117
131
TO/APR NORMAL
HIGH
87
98
91
102
95
105
98
109
101
112
105
117
LAND NORMAL 82 85 88 91 94 98
*Use in an emergency which requires landing at weights in excess of 8000 lbs
Flaps UP or UNKNOWN MULTIPLY appropriate STALL WARNING-NORMAL or HIGH
landing distance by 2.31.
Flaps TO/APR MULTIPLY appropriate STALL WARNING-NORMAL or HIGH
landing distance by 2.10.
Flaps LAND MULTIPLY appropriate landing distance by 1.83.
　
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本文鏈接地址：Citation Mustang airplane flight manual 1(32)