H30755
Window No. 2 (Pilot's Sliding Window) Installation 500
56-12-11 Figure 401 May 15/70
Page 402
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
3. Prepare Window No. 2 (Pilots' Sliding Window) for Installation
A. Check that power is off in window heating system.
CAUTION: OUTPUT VOLTAGE OF AUTOTRANSFORMER RANGES FROM 250 TO 350 VOLTS. BE CAREFUL WHEN WORKING ON SLIDING WINDOW.
B. Clean tracks, glides and surrounding areas with a rag moistened with solvent.
C. Apply a light film of oil, to tracks and to surfaces of glides and mechanism that contact tracks.
4. Install Window No. 2 (Pilots' Sliding Window)
A. Connect deicing electrical leads to terminal strip on clothing guard.
CAUTION: TO ENSURE SAFE AND SATISFACTORY OPERATION OF WINDOW HEATING SYSTEM, SEE THAT WINDOW LEAD TAPS TRANSFORMER AT A POINT WHERE CODE CONFORMS WITH THAT OF THE WINDOW RESISTANCE. REFER TO CONTROL CABIN WINDOW ANTI-ICING SYSTEM, CHAPTER 30.
NOTE: Window resistance code is usually etched in red near one of the bus bar terminals.
B. Hold window with front of clothing guard (4, figure 401) level with guide pin track (2) and insert lower aft glide (7), through cut out (5), into lower track. This can be accomplished by resting lower aft glide on top of track and sliding gently back and forth to locate cut out.
C. Lift lower front corner of window assembly so that upper glide (1) goes aft and can be slipped into its track.
D. Slide window aft, with lower forward glide (3), resting on top of track, until glide drops through cut out in track lip.
E. Test and adjust window if required. See Window No. 2 (Pilots' Sliding Window) -Adjustment/Test.
500
May 15/70 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 56-12-11 Page 403
WINDOW NO. 2 (PILOT'S SLIDING WINDOW) - ADJUSTMENT/TEST
1. Window No. 2 (Pilots' Sliding Window) Adjustment
A. Prepare for Adjustment
(1)
With the window in closed and lock position determine the adjustments required to obtain proper positioning of the window, as follows:
(a)
Determine adjustment required to center window in fore and aft position for a gap of
0.06 +0.03 inch between forward outer surface of window and outer skin.
(b)
Determining that window closing force does not exceed 45 +15 pounds.
(2)
Unlatch window and check for smooth operation.
(3)
Remove window No. 2 from track and place on a suitable support (Ref Window No. 2 [Pilots' Sliding Window] - Removal/Installation).
B. Adjust Window (Fig. 501)
(1) Adjust vertical position of window.
NOTE: Minor vertical adjustments can be made by varying number of shim washers between mechanism bellcranks and glide bearings as required to obtain smooth operation of window.
(a)
Remove special bolt from through glide track roller.
(b)
Remove or add shim washers as required.
NOTE: If shim washer is removed from lower glides, one will probably have to be installed at upper glide to maintain original dimensions between glide faces and to prevent window tilt. If adjustment is being made to correct a binding condition, removal of shims from upper glide only will be necessary.
(c)
Install special bolt.
NOTE: Make sure you tighten the lock screw (6) securely.
500
Oct 20/92 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 56-12-11 Page 501
H30762 A86910
Window No. 2 Adjustment 500
56-12-11 Figure 501 (Sheet 1) Nov 15/78
Page 502
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
500 Window No. 2 Adjustment
Oct 20/92 Figure 501 (Sheet 2) 56-12-11
Page 503
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
(2) Adjust fore and aft position of window.
(a) Adjust position of guide pin on serrated plate (Detail A).
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 AMM 飛機維護手冊 WINDOWS 風擋/窗戶(23)
