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
16. ENG ANTI-ICE and AIR COND Switches - - - - - - - -AS REQUIRED
17. AIR SOURCE SELECT Knob- - - - - - - - - - - - - - - - - - - - - - - BOTH
PROCEDURE COMPLETED
(Continued Next Page)
2 INFLIGHT RESTART – ONE ENGINE
B
510CLEAP-07 AA 19
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
INFLIGHT RESTART - ONE ENGINE (Continued)
• WINDMILLING AIRSTART (AIRSPEED 225 KIAS MINIMUM, ALTITUDE
15,000 FEET OR LOWER, 4% N2 MINIMUM, RAT -10°C OR WARMER)
9. FUEL BOOST Switch (affected side) - - - - - - - - - - - - - - - - - - - - - - ON
10. Throttle (affected engine)- - - - - - - - - - - - - - - IDLE at 4% N2 (minimum)
11. Engine Instruments- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR
a. Abort Start if no ITT rise within 10 seconds or ITT limit exceeded.
b. Abort Start if stabilized flight idle is not achieved within 90 seconds.
C A U T I O NCAUTION
• The FADEC will cycle fuel flow and ignition to accelerate N2 to 20% while
maintaining ITT within limits. ITT and N2 will increase in a stair-step manner
and ITT may briefly exceed 830°C. Once N2 reaches 20%, the cycling
should stop and the ITT should smoothly increase until peaking. If ITT
exceeds a start limit during this portion of the start sequence, the start must
be manually terminated.
• If the airspeed decreases below 225 KIAS during the windmill start
sequence, the start attempt should be terminated.
IF ENGINE DOES NOT START
12. Throttle (affected engine) - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF
13. FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - -AS REQUIRED
14. Refer to the WITH STARTER ASSIST bullet in this procedure; Tab
B2, or ENGINE FAILURE/PRECAUTIONARY SHUTDOWN; Tab B1,
or SINGLE-ENGINE APPROACH AND LANDING; Tab AB2.
PROCEDURE COMPLETED
IF ENGINE DOES START
12. GEN Switch (affected side) - - - - - - - - - - - - - - - - - - - - - - - - - GEN
13. FUEL BOOST Switch (affected side)- - - - - - - - - - - - - - - - - - NORM
(after engine stabilizes)
14. Engine Instruments/CAS Messages - - - - - - - - - -CHECK NORMAL
15. ENGINE ANTI-ICE and AIR COND Switches - - - - - -AS REQUIRED
16. AIR SOURCE SELECT Knob - - - - - - - - - - - - - - - - - - - - - - - BOTH
PROCEDURE COMPLETED
B
20 AA 510CLEAP-07
Configuration
MODEL 510 EMERGENCY/ABNORMAL PROCEDURES
1. Throttle (affected engine)- - - - - - - - - - - - - - - - - - - - - - - - - - - - - -CUTOFF
2. ENGINE START DISENG Button - - - - - - - - PRESS 15 SECONDS AFTER
THROTTLE CUTOFF
• IF UNABLE TO ATTEMPT ANOTHER START
ON GROUND
PROCEDURE COMPLETED
IN FLIGHT
3. Land as soon as practical. Refer to ENGINE FAILURE/
PRECAUTIONARY SHUTDOWN; Tab B1.
PROCEDURE COMPLETED
• IF ABLE TO ATTEMPT ANOTHER START
ON GROUND
3. Refer to DRY MOTORING, Tab B4, prior to making another start
attempt.
PROCEDURE COMPLETED
IN FLIGHT
3. Refer to INFLIGHT RESTART – ONE ENGINE; Tab B2.
PROCEDURE COMPLETED
1. Throttle (affected engine)- - - - - - - - - - - - - - - - - - - - - - - - - - - - - -CUTOFF
2. IGNITION Switch (affected side)- - - - - - - - - - - - - - - - - - - - - - - - - - NORM
3. ENGINE START Button (affected side) - - - - - - - - - - - PRESS momentarily
Motor engine for desired duration (observe starter limits; refer to Operating
Limitations, START CYCLE LIMITATIONS in the AFM).
4. ENGINE START DISENG Button - - - - - - - - - - - - - - - - - - - - - - - - -PRESS
PROCEDURE COMPLETED
3 ENGINE START MALFUNCTION (ENGINE DOES NOT START)
4 DRY MOTORING
B
510CLEAP-07 AA 21
Configuration
EMERGENCY/ABNORMAL PROCEDURES MODEL 510
1. ENGINE START DISENG Button - - - - - - - - - - - - - - - - - - - - - - - - PRESS
• IF STARTER DOES NOT DISENGAGE AND ENGINE START SWITCH
LIGHT REMAINS ILLUMINATED (START RELAY STUCK)
ON GROUND
2. L and R GEN Switches - - - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
3. BATTERY DISCONNECT Switch - - - - - - - - - - - - - - - LIFT GUARD
AND DISCONNECT
4. Ground Power Unit (if connected) - - - - - - - - - - - - - - DISCONNECT
5. Throttle(s) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF
6. Battery (in tailcone) - - - - - - - - - - - - - - - - - - - - - - - - DISCONNECT
7. BATT Switch- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
8. STBY INST Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF
9. Ground Power Unit - - - - - - - - - - - - - - - - - - DO NOT RECONNECT
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Citation Mustang checklist EMERGENCY/ABNORMAL PROCEDURES(14)
