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

when not commanded.
• IF WING/STAB DEICE SWITCH AUTO OR MANUAL
1. Throttles - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - INCREASE POWER
(as required above 70% N2)
2. WING/STAB Deice Switch- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF
(Verify TAIL DE-ICE FAIL message clears)
3. WING/STAB Deice Switch- - - - - - - - - - - - - - - - - - - HOLD IN MANUAL
(SURFACE DE-ICE message should display within 6 seconds)
4. WING/STAB Deice Switch- - - - - - - - - - - - - AUTO for at least 2 minutes
 IF TAIL DE-ICE FAIL MESSAGE REMAINS DISPLAYED OR
DISPLAYS AGAIN
5. Exit icing environment.
o IF IT CANNOT BE VERIFIED THERE IS NO ICE ON THE
HORIZONTAL STABILIZER
ENROUTE / DESCENT
6. Minimum Airspeed (once out of icing conditions) - - - - 130 KIAS
APPROACH AND LANDING
7. Flaps - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TO/APR
8. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VREF + 10
9. Landing Distance/Weight:
a. MULTIPLY normal Flap TO/APR landing distance by 1.22.
b. REDUCE maximum landing weight by 40 lbs.
C A U T I O NCAUTION
Avoid landing with a tailwind.
PROCEDURE COMPLETED
o IF NO ICE ON THE HORIZONTAL STABILIZER
PROCEDURE COMPLETED
 IF TAIL DE-ICE FAIL MESSAGE REMAINS OFF
PROCEDURE COMPLETED
• IF WING/STAB DEICE SWITCH OFF
1. Do not fly into icing conditions.
PROCEDURE COMPLETED
4  TAIL DE-ICE FAIL
510CLEAP-07 AA 59
Q
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
Indicates the windshield has been overheated for more than 5 seconds. The white W/S
O’HEAT message turns amber if it is on for 5 seconds. If the windshield temperature
controller is working properly, it will shut off power to the windshield heater to allow the
windshield to cool then turn heat back on.
• IF MESSAGE IS ON STEADY
1. WINDSHIELD ANTI-ICE switch (affected side) - - - - - - - - - - - - - - -OFF
2. Exit icing environment.
3. Refer to WINDSHIELD A/I INOPERATIVE APPROACH AND LANDING;
Tab AE1.
PROCEDURE COMPLETED
• IF MESSAGE IS CYCLING ON AND OFF
1. W/S O’HEAT message - - - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR
PROCEDURE COMPLETED
Indicates that one or more segments of the wing deice boot system did not reach the
required pressure when commanded or that pressure is present when not
commanded.
• IF WING/STAB DEICE SWITCH AUTO OR MANUAL
1. Throttles - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - INCREASE POWER
(as required above 70% N2)
2. WING/STAB Deice Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
(Verify WING DE-ICE FAIL message clears)
3. WING/STAB Deice Switch - - - - - - - - - - - - - - - - - - -HOLD IN MANUAL
(SURFACE DE-ICE message should display within 6 seconds)
4. WING/STAB Deice Switch - - - - - - - - - - - - - AUTO for at least 2 minutes
 IF WING DE-ICE FAIL MESSAGE REMAINS DISPLAYED OR
DISPLAYS AGAIN
5. WING/STAB Deice Switch - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
6. Exit icing environment.
o IF IT CANNOT BE VERIFIED THERE IS NO ICE ON THE WING
7. Refer to LANDING WITH ICE ON WING LEADING EDGE; Tab
AD2.
PROCEDURE COMPLETED
o IF NO ICE ON THE WING
PROCEDURE COMPLETED
 IF WING DE-ICE FAIL MESSAGE REMAINS OFF
PROCEDURE COMPLETED
• IF WING/STAB DEICE SWITCH OFF
1. Do not fly into icing conditions.
2. WING/STAB Deice Switch - - - - - - - - - - - - - - - - - - - - - AUTO then OFF
(Verify white STALL WARN HI message is displayed).
3. Use STALL WARNING-HIGH performance data for landing.
PROCEDURE COMPLETED
1  W/S O’HEAT L-R – AMBER (WINDSHIELD OVERHEAT)
2  WING DE-ICE FAIL
60 AA 510CLEAP-07
R
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
In some icing encounters at high altitude, the heater on the engine T2 probe cannot
keep the probe clear of ice. This can cause a false high RAT temperature indication to
the FADEC. The result is the FADEC will command a lower N1 until the T2 probe is deiced,
or the Engine Anti-Ice is selected OFF. This may occur with only a trace of ice
accumulation visible on the airplane.
If both engine anti-ice circuit breakers are pulled, the engine inlets will both be heated,
but an amber ENG A/I COLD CAS message will display due to the loss of nacelle
temperature monitoring. No additional action is required to address the amber ENG
A/I COLD CAS message, and the message will clear when either circuit breaker is
reset.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang checklist EMERGENCY/ABNORMAL PROCEDURES(31)