S 864-190-N00
(2) For the applicable engine, remove the DO-NOT-CLOSE tags and close these circuit breakers:
(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) 6K19 IGN 2 ENG 1
6) 6K20 IGN 2 ENG 2
7) 6K21 IGN 2 ENG 3
8) 6K22 IGN 2 ENG 4
9) 6G19 STBY IGN ENG 1
10) 6G20 STBY IGN ENG 2
11) 6G21 STBY IGN ENG 3
12) 6G22 STBY IGN ENG 4
S 414-406-N00
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(3) Close the right thrust reverser (AMM 78-31-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-11-05
ALL ú ú N02 Page 465 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 414-407-N00
(4)
Close the right core cowl panel (AMM 71-11-06/201).
S 414-408-N00
(5)
Clsoe the right fan cowl panel (AMM 71-11-04/201).
S 444-409-N00
(6)
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
S 714-454-N00
(7)
Do the test of the fuel injector and support as shown in the Power Plant Test Reference Table (AMM 71-00-00/501).
TASK 73-11-05-404-193-N00
13. Install the No. 10, 11, or 12 Fuel Injector and Support
_______________________________________________________
(Fig. 401, 402, and 403)
A. Equipment
(1) M303, M305, or M307 Bergen Mechanical Crimper
Bergen Cable Technologies Inc
170 Gregg St
P.O.
Box 1300
Lodi, NJ 07644-9982
B.
Consumable Materials
(1)
D00009 Compound - Antiseize, MIL-M-7866, Powdered Molykote Type Z
(2)
D00045 Beeswax
(3)
D00250 Petrolatum White, VV-P-236
(4)
D00301 Petroleum Jelly, Vaseline
(5)
D00390 Oil - Engine
(6)
G00767 Wax - Paraffin, PMC 9552
(7)
G01505 Lockwire - MS20995
(8)
G02332 Ferrule - P05-292 (Optional)
(9)
G02335 Cable - Safety - P05-291 (Optional)
C.
Parts
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-11-05
ALL ú ú N02 Page 466 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 3 | Packing | 73-11-06 | 30 | 65 | | | 5 | Fuel Injector and Support | 73-11-05 | 05 | 10 | | | 19 | Gasket | | | 20 | | | 20 | Packing | 73-11-06 | 25 | 15 | | 403 | 5 | Gasket | | | 50 | | | 15 | Gasket | | | 65 | | | 16 | Gasket | | | 80 | 2.....….........…...................................…..........…......…........1
D. References
(1)
AMM 71-00-00/501, Power Plant
(2)
AMM 71-11-04/201, Fan Cowl Panels
(3) 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(69)
