BS
255
FWD
AFTER THE TABLE IS FILLED OUT, MEASURE THE SKIN AT
WL 230 AT POSITION 1. ENTER THE MEASUREMENT HERE:_________
G18981
737 Skin Waviness Analysis Worksheet Figure 604 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
51-10-00
ALL ú ú B01 Page 612 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
BS
255
AIRPLANE:DATE
FLIGHT CYCLES:LEFT SIDE FLIGHT HOURS:
230.0WL
226.0WL
224.0WL
218.0WL
214.0WL
210.0WL
206.0WL
204.0WL
198.0WL
193.0WL
189.7WL
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
POSITION
BS
228
FWD
AFTER THE TABLE IS FILLED OUT, MEASURE THE SKIN AT
WL 230 AT POSITION 1. ENTER THE MEASUREMENT HERE:_________
G18983
737 Skin Waviness Analysis Worksheet Figure 604 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
51-10-00
ALL ú ú B01 Page 613 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
AND FUSELAGE
WINDOW NO. 2 VACUUM BLANKET
____ THE VACUUM BLANKET COVERS THE ENTIRE WINDOW AND
NOTE:
THE GAP BETWEEN THE WINDOW AND THE FUSELAGE.
Window No. 2 Vacuum Blanket Check
Figure 601
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
51-11-00
ALL ú ú B01 Page 601 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E85429
A 737-300/400/500MAINTENANCE MANUAL
____ THE VACUUM BLANKET COVERS THE ENTIRE DOOR AND
NOTE: THE GAP BETWEEN THE DOOR AND THE FUSELAGE.
1
THIS PROCEDURE IS THE SAME FOR THE GALLEY
ENTRY DOORS AND THE ESCAPE HATCHES.
Passenger Entry Door Vacuum Blanket Check Figure 602
E85554
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
51-11-00
ALL ú ú B01 Page 602 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
WINDOW, DOOR AND HATCH LEAK CHECK - INSPECTION/CHECK
____________________________________________________
1. General_______
A. This procedure has these tasks:
(1)
Leak Check of the No. 2 Openable Window
(2)
Leak Check of the Doors and Hatches
TASK 51-11-00-286-001-B00
2. Leak Check of the No. 2 Window______________________________
A. General
(1) This procedure is for the right and left No. 2 Openable Windows.
B. Equipment
(1)
FT1W2130-2, No. 2 Window Vacuum Blanket
(2)
ST6760A-1, Ultrasonic Leak Probe Tool
(3)
ST9999-VBA-201, Vacuum Generator (No. 2 window, door and hatch)
(4)
ST9999-VBA-301, Vacuum Generator (No. 2 window only)
C. References
(1)
AMM 30-41-00/501, Control Cabin Window Anti-Ice System
(2)
AMM 56-12-11/501, No. 2 Window
D. Access
(1) Location Zone
101 Control Cabin, Left
102 Control Cabin, Right
E. Procedure
S 866-002-B00
WARNING:_______DISARM THE WINDOW HEAT SYSTEM BEFORE YOU CHECK THE WINDOWS. IF THE WINDOW POWER IS ON, YOU CAN GET AN ELECTRICAL SHOCK WHEN YOU TOUCH THE WINDOW. THE SHOCK CAN CAUSE INJURY TO PERSONS.
(1) Make sure the power is OFF for the window heat system.
(a)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 结构 STRUCTURES(7)
