(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 414-418-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 left thrust reverser (AMM 78-31-00/201).
(4)
Close the left core cowl panel (AMM 71-11-06/201).
(5)
Close the left fan cowl panel (AMM 71-11-04/201).
S 414-420-N00
S 414-419-N00
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73-11-05
ALL ú ú N01 Page 480H ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 444-421-N00
(6)
Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
S 714-461-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 73-11-05-404-256-N00
16. Install the No. 19, 20, or 21 Fuel Injector and Support (Fig. 401)
_______________________________________________________
A. Standard Tools and Equipment
(1) M303, M305, or M307 Bergen Mechanical Crimper
Bergen Cable Technologies Inc
170 Gregg St
P.O. Box 1300
Lodi, NJ 07644-9982
(2)
Bonding Meter (AMM 20-22-01/601)
B.
Consumable Materials
(1)
A00303 Adhesive - RTV 174 (optional to BMS 5-63 Sealant)
(2)
A00429 Sealant - Hydraulic, Fire Resistant, BMS 5-63
(3)
D00045 Beeswax
(4)
D00250 Petrolatum White, VV-P-236
(5)
D00301 Petroleum Jelly, Vaseline
(6)
D00390 Oil - Engine
(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 | ................................................................................ | 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 | 2.....….........…...................................…..........…......…........1
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73-11-05
ALL ú ú N02 Page 480I ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
D. References
(1)
AMM 20-11-15/401, Bonding Jumpers and Ground Leads
(2)
AMM 20-22-01/601, Electrical Bonding
(3)
AMM 71-00-00/501, Power Plant
(4)
AMM 71-11-04/201, Fan Cowl Panels
(5)
AMM 71-11-06/201, Core Cowl Panels
(6)
AMM 75-24-02/401, Turbine-Vane Cooling-Air Duct
(7)
AMM 78-31-00/201, Thrust Reverser System
E.
Access
(1)
Location Zone 412 Engine 1 - Diffuser and Combustor Case 10 o'clock 422 Engine 2 - Diffuser and Combustor Case 10 o'clock 432 Engine 3 - Diffuser and Combustor Case 10 o'clock 442 Engine 4 - Diffuser and Combustor Case 10 o'clock
(2)
Access Panel
415 Left Thrust Reverser Half - Engine 1
425 Left Thrust Reverser Half - Engine 2
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