S 714-459-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 73-11-05-404-237-N00
15. Install the No. 16, 17, or 18 Fuel Injector and Support (Fig. 401)
_______________________________________________________
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)
G01505 Lockwire - MS20995
(6)
G02332 Ferrule - P05-292 (Optional)
(7)
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 N01 Page 480D ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D. References
(1)
AMM 71-00-00/501, Power Plant
(2)
AMM 71-11-04/201, Fan Cowl Panels
(3)
AMM 71-11-06/201, Core Cowl Panels
(4)
AMM 78-31-00/201, Thrust Reverser System
(5)
AMM 79-11-01/401, Oil Tank
E.
Access
(1)
Location Zone 412 Engine 1 - Diffuser and Combustor Case 8 o'clock 422 Engine 2 - Diffuser and Combustor Case 8 o'clock 432 Engine 3 - Diffuser and Combustor Case 8 o'clock 442 Engine 4 - Diffuser and Combustor Case 8 o'clock
(2)
Access Panel
415 Left Thrust Reverser Half - Engine 1
425 Left Thrust Reverser Half - Engine 2
435 Left Thrust Reverser Half - Engine 3
445 Left Thrust Reverser Half - Engine 4
F.
Prepare for the Installation of the No. 16, 17 or 18 Fuel Injector and Support
S 224-238-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:
~............................................................. | | | NEW PART REFERENCE | CLEARANCE | | | | DIMENSIONS | LIMITS | | PART | | INCHES | INCHES | | NAME | DIA | (MM) | (MM) | | | ............................................... | | | MIN | MAX | MIN | MAX | ............................................................... | SUPPORT | OD | 1.821 | 1.823 | | | | | | (46.254) | (46.304) | 0.001 | 0.005 | ......................................... (0.026) | (0.127) | | CASE | ID | 1.824 | 1.826 | | | | BOSS | | (46.330) | (46.380) | | | 2.........….....…...........…...........…..........…..........1
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73-11-05
ALL ú ú N01 Page 480E ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
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