S 014-004-B00
(8)
Remove the glare shield (lightshield) brackets or clips, when it is necessary.
(a)
Support the lightshield.
(b)
Remove the four screws from each of the two lightshield brackets.
(c)
Lift the aft edge of the light shield.
(d)
Disconnect the antifogging ducts from the nozzles.
(e)
Remove the lightshield from the cockpit.
S 014-005-B00
(9) Remove the sunshade support rod above the window drain tube clamps at the window post on the airplane centerline.
NOTE: You must move the drain tubes to one side to permit the
____
removal of the window.
S 014-006-B00
(10)
Move the window heat switches on the P5-9 overhead panel to the OFF position.
(11)
Disconnect the power leads at the bus bar terminals on the window.
(12)
Remove the wiper arm (AMM 30-42-11/401).
S 034-008-B00
(13)
Remove the aerodynamic smoother from the free end of the nylon cord in the top aft corner of the window.
S 034-007-B00
S 024-088-B00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
56-11-11
ALL ú ú B02 Page 403 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 034-009-B00
(14) Pull the nylon cord from the window to remove the aerodynamic smoother.
NOTE:____Pull the cord parallel to the window frame. This will help stop the cord from braking before it is fully removed.
D. Remove the Window No. 1 (Fig. 401).
S 034-010-B00
(1) Remove the window fasteners, the wire clamps, the washers, the nuts, the seals and the O-rings.
NOTE: Make a note of all the parts and their locations to make the
____ installation easier. Refer to the IPC for new parts and their location.
There is a row of bolts that attach a retaining angle to the frame at the aft edge of the window. To get access to these bolts, open an adjacent sliding window (detail B).
S 034-011-B00
(2) Open an adjacent sliding window and remove the retaining angle bolts from the doubler, the retaining angle and the window frame post.
NOTE: Keep the retaining angle bolts and the retaining angle with
____
the doubler for installation.
The retaining angle cannot be removed until the windshield is out of the window frame.
S 034-012-B00
(3) Apply hand pressure to the outer side of the window to break the pressure seal.
NOTE: This procedure requires two persons, one on the inside and one on the outside of the airplane.
Always apply pressure to the largest area possible. You can tap the window with a rubber mallet and nonmetallic block if it is particularly difficult to remove. Do not permit the window to fall free when you break the pressure seal. Remove the spacers and the silicone rubber molded-in-position seal with the window assembly.
S 024-054-B00
(4) Remove the window.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
56-11-11
ALL ú ú B01 Page 404 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
TASK 56-11-11-404-013-B00
3. Window No. 1 Installation
_________________________
A. General
B. Standard Tools and Equipment
(1)
MIT5-89354 - High Voltage Tool
(2)
HYPOT Model 3500D - Dielectric Tester
Associated Research Inc., 13860 W Laurel Drive,
Lake Forest, IL 60045-4546
1-800-858-8378
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) WINDOWS(11)
