73-11-05
ALL ú ú N01 Page 473 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 414-410-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 thrust reversers (AMM 78-31-00/201).
S 414-411-N00
(4)
Close the core cowl panels (AMM 71-11-06/201).
S 414-412-N00
(5)
Close the fan cowl panels (AMM 71-11-04/201).
S 444-413-N00
(6)
Do the activation procedure for the thrust reversers
(AMM 78-31-00/201).
S 714-456-N00
(7)
Do the test of the fuel injector and suuport as shown in the Power Plant Test Reference Table (AMM 71-00-00/501).
TASK 73-11-05-404-216-N00
14. Install the No. 13, 14, or 15 Fuel Injector and Support
_______________________________________________________
(Fig. 401, 402, and 404)
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)
D00045 Beeswax
(2)
D00250 Petrolatum White, VV-P-236
(3)
D00301 Petroleum Jelly, Vaseline
(4)
D00390 Oil - Engine
(5)
G00964 Compound - Antigalling, Fel-Pro C-200
(6)
G01505 Lockwire - MS20995
(7)
G02332 Ferrule - P05-292 (Optional)
(8)
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 |
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73-11-05
ALL ú ú N01 Page 474 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | | 19 | Gasket | | | 20 | | | 20 | Packing | 73-11-06 | 25 | 15 | 2.....….........…...................................…..........…......…........1
D. References
(1)
AMM 24-11-01/401 Integrated Drive Generator (IDG)
(2)
AMM 70-24-05/201, Electrical Harnesses
(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 78-31-00/201, Thrust Reverser System
E.
Access
(1)
Location Zone 412 Engine 1 - Diffuser and Combustor Case 7 o'clock 422 Engine 2 - Diffuser and Combustor Case 7 o'clock 432 Engine 3 - Diffuser and Combustor Case 7 o'clock 442 Engine 4 - Diffuser and Combustor Case 7 o'clock
(2)
Access Panel 415 and 416 Thrust Reverser Halves - Engine 1 425 and 426 Thrust Reverser Halves - Engine 2 435 and 436 Thrust Reverser Halves - Engine 3 445 and 446 Thrust Reverser Halves - Engine 4
F.
Prepare for the Installation of the No. 13, 14 or 15 Fuel Injector and Support
S 224-217-N00
(1)
Examine the clearance between the outer diameter of the support (5) and the inner diameter of the diffuser and combustor case boss.
(a)
Make sure the clearance is in the limits that are given in the table below:
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