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时间:2011-04-15 08:41来源:蓝天飞行翻译 作者:航空
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 (a)  P414 Power Distribution Center - Left
 1) 414D17 CH SELECT GND TEST ENG 1
 2) 414D18 CH SELECT GND TEST ENG 2
 3) 414D19 CH SELECT GND TEST ENG 3
 4) 414D20 CH SELECT GND TEST ENG 4
 5) 414D21 EEC GND TEST ENG 1
 6) 414D22 EEC GND TEST ENG 2
 7) 414D23 EEC GND TEST ENG 3
 8) 414D24 EEC GND TEST ENG 4

 TASK 76-11-03-862-115-N00
 40. Energize the Fuel Control Toggle Switches (Fig. 201)
_________________________________________
 A. Access
 (1)  Location Zone
 221 Control Cabin, LH
 222 Control Cabin, RH

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 76-11-03
 ALL  ú ú N02 Page 259 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
B. Procedure
 S 862-116-N00
 WARNING: MAKE SURE YOU KEEP THE CIRCUIT BREAKERS FOR THE ENGINE IGNITION
_______ OPEN WHILE THE CIRCUIT BREAKERS FOR THE FUEL CONTROL VALVE ARE OPEN. THE IGNITER PLUGS WILL AUTOMATICALLY FIRE IF YOU ARE OUT OF ZERO DETENT, NACELLE ANTI-ICE IS ON, CON IGNITION SWITCH IS SET TO "ON", OR ENGINE START SWITCH IS PULLED TO "ON". IF THE COMBUSTION CHAMBER HAS FUEL IN IT, AN INTERNAL ENGINE OR A TAILPIPE FIRE CAN OCCUR. THE FIRE CAN CAUSE INJURY TO PERSONS OR DAMAGE TO THE ENGINE.
 (1)  Close these circuit breakers and remove the DO-NOT-CLOSE tags:
 (a)  P6 Main Power Distribution Panel
 1) 6F1 IGN 1 ENG 1
 2) 6F2 IGN 1 ENG 2
 3) 6F3 IGN 1 ENG 3
 4) 6F4 IGN 1 ENG 4
 5) 6G1 FUEL SHUTOFF VALVE ENG 1
 6) 6G2 FUEL SHUTOFF VALVE ENG 2
 7) 6G3 FUEL SHUTOFF VALVE ENG 3
 8) 6G4 FUEL SHUTOFF VALVE ENG 4
 9) 6G19 IGN 1 ENG 1
 10) 6G20 IGN 2 ENG 2
 11) 6G21 IGN 2 ENG 3
 12) 6G22 IGN 2 ENG 4
 13) 6K19 STBY IGN ENG 1
 14) 6K20 STBY IGN ENG 2
 15) 6K21 STBY IGN ENG 3
 16) 6K22 STBY IGN ENG 4
 17) 6L10 FUEL CONT VALVE ENG 1
 18) 6L11 FUEL CONT VALVE ENG 2
 19) 6L12 FUEL CONT VALVE ENG 3
 20) 6L13 FUEL CONT VALVE ENG 4

 TASK 76-11-03-442-117-N00
 41. Activation Procedure for the Autothrottle Servomotor (Fig. 201)____________________________________________________
 A. Access
 (1)  
Location Zone
 221 Control Cabin, LH
 222 Control Cabin, RH


 B.
Procedure


 S 862-118-N00
 (1)  Close these circuit breakers and remove the DO-NOT-CLOSE tags:
 (a)  P7 Overhead Circuit Breaker Panel
 1) 7C4 FMCS A/T SERVO L
 2) 7C25 FMCS A/T SERVO EXC

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 76-11-03
 ALL  ú ú N02 Page 260 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
3) 7C26 FMCS A/T SERVO R
 TASK 76-11-03-862-119-N00
 42. Energize the Reverse Thrust Lever Interlock Actuators (Fig. 201)
_____________________________________________________
 A. Access
 (1)  Location Zone
 221 Control Cabin, LH
 222 Control Cabin, RH

 B. Procedure
 S 862-120-N00
 (1)  Close these circuit breakers and remove the DO-NOT-CLOSE tags:
 (a)  P6 Main Power Distribution Panel 1) 6F12 T/R IND ENG 1 2) 6E12 T/R IND ENG 2 3) 6D12 T/R IND ENG 3 4) 6C12 T/R IND ENG 4
 TASK 76-11-03-862-121-N00
 43. Energize the Thrust Lever Switches (Fig. 201)
__________________________________
 A. Access
 (1)  Location Zone
 221 Control Cabin, LH
 222 Control Cabin, RH

 B. Procedure
 S 862-122-N00
 (1)  To energize the control switches for the thrust reverser, close these circuit breakers and remove the DO-NOT-CLOSE tags:
 (a)  P6 Main Power Distribution Panel 1) 6F13 T/R CONT ENG 1 2) 6E13 T/R CONT ENG 2 3) 6D13 T/R CONT ENG 3 4) 6C13 T/R CONT ENG 4
 TASK 76-11-03-862-123-N00
 
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本文链接地址:747-400 AMM 飞机维护手册 发动机控制 ENGINE CONTROLS(44)