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

PROCEDURE COMPLETED
• IF MESSAGE CLEARS
PROCEDURE COMPLETED
Indicates that no current is flowing to the pitot probe or static port heaters.
• IN FLIGHT
1. Pitot-Static Switch- - - - - - - - - - - - - - - - - - - - - - - - - - - - PITOT-STATIC
2. Circuit Breaker - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
3. Airspeed/Altitude (affected system) - - - - - - - - - - - - - - - - - -COMPARE
with unaffected systems
 IF AIRSPEED AND ALTITUDE NOT NORMAL
4. SENSOR Softkey (affected side) - - - - - - - - - - - - - - - - - - - PRESS
5. ADC1/2 Softkey - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - PRESS
appropriate softkey
6. PFD ADI Displays - - - - - - - - - - - CONFIRM “BOTH ON ADC1 or 2"
is displayed on both PFDs.
7. Exit icing environment. Consider impact on RVSM capability.
PROCEDURE COMPLETED
 IF AIRSPEED AND ALTITUDE NORMAL
4. Continue to monitor.
PROCEDURE COMPLETED
• ON GROUND
1. PITOT STATIC Switch- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON;
verify message clears then OFF
C A U T I O NCAUTION
Pitot probes may be damaged if the pitot/static heat is operated for more than 2
minutes on the ground.
PROCEDURE COMPLETED
1  ENG A/I COLD L-R – AMBER (ENGINE ANTI-ICE COLD)
2  P/S HTR L-R (PITOT-STATIC HEATER)
56 AA 510CLEAP-07
P
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
IF SEVERE ICING IS PRESENT
1. Immediately report weather conditions and request priority handling from Air
Traffic Control to facilitate a route or altitude change to exit the severe icing
conditions.
2. Flaps - - - - - - - - - - - - - - - - - - - - - - - - - - LEAVE IN CURRENT POSITION
(Do not extend or retract until airframe is clear of ice)
3. Autopilot - - - - - - - - - - - - - - Hold control wheel firmly and DISENGAGE
C A U T I O NCAUTION
Exert control wheel force as required to maintain desired flight path.
4. Avoid abrupt and excessive maneuvering that may aggravate control
problems.
5. If unusual or uncommanded roll is encountered - - - - - - - REDUCE ANGLE
OF ATTACK
PROCEDURE COMPLETED
3  SEVERE ICING ENCOUNTER
510CLEAP-07 AA 57
P
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
Indicates that no power is being supplied to the stall warning vane.
1. PITOT STATIC Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - PITOT-STATIC
2. STALL WARN HEAT Circuit Breaker - - - - - - - - - - - - - - - - - - - - - - CHECK
(R circuit breaker panel)
• IF IN ICING CONDITIONS AND MESSAGE DOES NOT CLEAR
3. Exit icing environment.
4. Airspeed (except approach and landing) - - - - - - - - 160 KIAS MINIMUM
5. Airspeed (approach and landing) - - - - - - - - - - - - VAPP/VREF MINIMUM
from STALL WARNING-HIGH performance charts for approach and
landing.
WARNING
If the stall warning vane becomes iced, the following systems may
provide invalid data:
• Stall warning horn with automatic autopilot disconnect
• Low speed awareness range on airspeed indicator
• On-speed circle
PROCEDURE COMPLETED
• IF NOT IN ICING CONDITIONS OR MESSAGE CLEARS
PROCEDURE COMPLETED
Indicates that there is no current to the T2 heater on the affected side when ENGINE
ANTI-ICE Switch has been selected ON for that side.
• ON GROUND
1. Correct prior to flight.
PROCEDURE COMPLETED
• IN FLIGHT
1. Exit icing environment.
PROCEDURE COMPLETED
Indicates a loss of power to the windshield anti-ice system or insufficient heat is being
provided to the windshield.
1. WINDSHIELD ANTI-ICE Switch (affected side) - - - - - - - - - - OFF then ON
2. L or R WSHLD TEMP circuit breaker- - - - - - - - - - - - - - - - - - - - - - CHECK
• IF W/S A/I FAIL MESSAGE REMAINS DISPLAYED
3. Exit icing environment.
4. Windshield - - - - - - - - - - - - - - - CLEAR FOG MANUALLY (as required)
5. Refer to WINDSHIELD A/I INOPERATIVE APPROACH AND LANDING;
Tab AE1.
PROCEDURE COMPLETED
• IF W/S A/I FAIL MESSAGE EXTINGUISHED
PROCEDURE COMPLETED
1  STALL WARN HTR (STALL WARNING VANE HEATER
FAILURE)
2  T2 HTR FAIL (ENGINE T2 HEATER FAILURE)
3  W/S A/I FAIL L-R – AMBER (WINDSHIELD ANTI-ICE FAILURE)
58 AA 510CLEAP-07
Q
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
Indicates that one or more segments of the horizontal or vertical tail deice boot system
did not reach the required pressure when commanded or that pressure is present
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang checklist EMERGENCY/ABNORMAL PROCEDURES(30)