S 864-040-N00
 (1)  Make sure the FUEL CONTROL switch for the applicable engine is in the CUTOFF position.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-11-04
 ALL  ú ú N01 Page 401 ú Jun 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE A
MAIN FUEL SUPPLY HOSE (REF)
IGNITION EXCITERS (REF)
(REF) MAIN GEARBOX  DISTRIBUTION VALVE STRAINER HOUSING ON FUEL BSEE  TRANSMITTER FUEL FLOW 
A  FWD 
Fuel Distribution Valve Strainer Installation Figure 401 (Sheet 1)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-11-04
 ALL  ú ú N02 Page 402 ú Feb 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
PWA 86459 PULLER FUEL FLOW
4. WASHER TRANSMITTER(4 LOCATIONS)
5. BOLT (4 LOCATIONS)
3. STRAINER COVER 6. TRANSFER HOSE FOR MAIN TUBEFUEL SUPPLY 2. PACKING 24. STRAINER (REF)
1. PACKING
8.
 PACKING

9.
 PACKING

7. GASKET
10.
 BOLT

11.
 CLAMP

23. BOLT (4 LOCATIONS) 16. BRACKET
12. NUT
22. WASHER (4 LOCATIONS) 13. CLAMP
21. ADAPTER FOR 
FUEL FLOW  14. BOLT 
TRANSMITTER  (2 LOCATIONS) 
FUEL 
DISTRIBUTION VALVE  12. NUT  1  15. BOLT 
20. CLAMP 
17. CLAMP 
19. CLAMP 

18. CLAMP
10. BOLT
16. BRACKET 2B
1
ENGINES PRE-PW-SB 73-164
2
ENGINES POST-PW-SB 73-164
Fuel Distribution Valve Strainer Installation Figure 401 (Sheet 2)
G21358
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-11-04
 ALL  ú ú N01 Page 403 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 864-054-N00
 WARNING: MAKE SURE YOU OPEN THE APPLICABLE CIRCUIT BREAKERS FOR THE
_______ ENGINE IGNITION BEFORE YOU OPEN THE ENGINE CIRCUIT BREAKER FOR THE FUEL CONT VALVE. THE IGNITER PLUGS CAN START THE IGNITION AUTOMATICALLY IF YOU DO NOT OPEN THE CIRCUIT BREAKERS. IF THE COMBUSTION CHAMBER HAS FUEL IN IT, AN INTERNAL ENGINE FIRE OR A TAILPIPE FIRE CAN OCCUR. THE FIRE CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE ENGINE.
 (2)  
For the applicable engine, open these circuit breakers and attach the DO-NOT-CLOSE tags:

 (a)  
P6 Main Power Distribution Panel
 1) 6F01, IGN 1 ENG 1
 2) 6G19, STBY IGN ENG 1
 3) 6K19, IGN 2 ENG 1
 4) 6F02, IGN 1 ENG 2
 5) 6G20, STBY IGN ENG 2
 6) 6K20, IGN 2 ENG 2
 7) 6F03, IGN 1 ENG 3
 8) 6G21, STBY IGN ENG 3
 9) 6K21, IGN 2 ENG 3
 10) 6F04, IGN 1 ENG 4
 11) 6G22, STBY IGN ENG 4
 12) 6K22, IGN 2 ENG 4

 S 864-053-N00
 (3)  
For the applicable engine, open this circuit breaker and install the DO-NOT-CLOSE tag:

 (a)  
P6 Main Power Distribution Panel
 1) 6L10, FUEL CONT VALVE ENG 1
 2) 6L11, FUEL CONT VALVE ENG 2
 3) 6L12, FUEL CONT VALVE ENG 3
 4) 6L13, FUEL CONT VALVE ENG 4

 (4)  
Open the right fan cowl panel (AMM 71-11-04/201).

 S 014-045-N00
 S 044-047-N00
 WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
 (5)  Do this procedure: Thrust Reverser Deactivation for Ground Maintenance (AMM 78-31-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 發動機燃油和控制 1(38)