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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 024-098
(3)
Remove the terminal connector from the jumper wire.
S 024-099
(4)
Remove the jumper wire from the terminal block on the lower outboard edge of the windshield.
S 034-101
(5)
Carefully remove the aerodynamic smoother from the clearance at inboard upper corner of the windshield (Fig. 402).
S 034-102
(6)
Pull the outboard end of the nylon cord out of the clearance.
S 034-103
(7)
Fold the nylon cord and slowly remove it from around the window.
TASK 56-11-01-404-016
3. Install the Windshield (Fig. 401)______________________
A. Special Tools and Equipment
(1) 2OHME65B07630, Windshield Handling Sling
B. Standard Tools and Equipment
(1)
Crane equipped with 40-foot boom and capable of lifting 500 pounds
(2)
Mobile mechanical lift (capable of extending to a height of 35 feet) or overhead crane capable of lifting 500 pounds
(3)
Spatula or flow gun
C. Consumable Materials
(1)
G00139 Tape - Protective, Gizard Protex 20V
(2)
G00294 Tape - Masking, Permacel No. 76
(3)
G02186 Tape - silicone foam insulation seal, Form III, Grade B
(4)
C00308 Compound - Corrosion Preventive, MIL-C-11796, Class 3
(5)
B00083 Solvent - Aliphatic Naphtha, TT-N-95
(6)
G00039 Cord - Nylon, MIL-C-5040, Type 1A or
(7)
G00040 Cord (optional) - Nylon, V-T-295, Type 1, Class 2, Size No. 9
(8)
A00055 Primer - Silicone, RTV 1200, S-2260, Dow Corning
(9)
A00247 Sealant - BMS 5-95, (aerodynamic smoother) or
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(10)
A00474 Sealant - Rubber Silicone, DC 93006,
(aerodynamic smoother)(optional)
(11)
A00707(Alternative) PR 1826, Class B-1/2 and Class B-1/4 (with primer) (dark grey).
(12)
A00707 (Alternative) PR1828, Class B-1/2 and B-1/4 (white).
(13)
A00955 Sealant - BMS 5-26, class B (used to fill hole of missing bolt)
D. Parts
~............................................................................... | AMM | | AIPC | ................. ........................... | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................. | 401 | 1 |Windshield Assembly (Pilot, Left) | 56-11-01 | 01 | 150 | | | 1 |Windshield Assembly (Co-pilot, Right)| | | 155 | | | 2 |Bolt | | | 160 | 2......…........….....................................…..........….....…........1
E. References
(1)
25-13-01/401, Pilots' Lightshield Assembly
(2)
30-41-00/501, Flight Compartment Window Anti-Icing System
(3)
30-42-00/501, Windshield Wiper System
(4)
WDM 30-41-11
(5)
SSM 30-41-01
F. Access
(1) Location Zone
221 Flight Deck, Left
222 Flight Deck, Right
G. Prepare for the Installation of the Windshield .
S 024-089
(1)
Remove the pilot assist handle.
S 424-091
(2)
Install washers as required to replace material thickness of the handle support bracket.
(3)
Install collars on the hi-loks.
(4)
Put the window heat switches in the OFF position.
S 864-018
(5)
Open these circuit breakers and attach DO-NOT-CLOSE tags:
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本文链接地址：747-400 AMM 飞机维护手册 WINDOWS 窗户/风挡(9)
