(d)
Lubricate the threads of the fasteners with compound, BMS 3-28.
(e)
Install bolts with a fastener tool and an installation anti cam-out (ACR) driver bit.
NOTE: Use decreased lubricated fastener torques, (AMM 20-50-11/201).
NOTE: A combination removal/installation ACR bit is not recommended. The bit should have a hardness of 56-58 RC.
TASK 57-30-01-422-011-B00
4. Guidelines for Missing Fasteners
A. References
(1)
12-31-61/201 Wing Lower Surface Access Doors and Panels
(2)
20-50-11/201 Standard Torque Values
B. Access
(1) Location Zones
300 Left Wing
400 Right Wing
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
57-30-01
ALL ú ú B01 Page 204 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(2) Access Panels
6212L/6512R Slat Access Panel
6213L/6513R Slat Access Panel
6214L/6514R Slat Access Panel
6215L/6515R Slat Access Panel
6217L/6517R Slat Access Panel
6218L/6518R Slat Access Panel
6219L/6519R Slat Access Panel
6220L/6520R Slat Access Panel
6221L/6521R Slat Access Panel
6222L/6522R Slat Access Panel
6223L/6523R Slat Access Panel
6224L/6524R Slat Access Panel
6225L/6525R Slat Access Panel
6226L/6526R Slat Access Panel
6227L/6527R Slat Access Panel
6228L/6528R Slat Access Panel
6229L/6529R Slat Access Panel
6230L/6530R Slat Access Panel
6231L/6531R Slat Access Panel
6232L/6532R Slat Access Panel
6233L/6533R Slat Access Panel
6234L/6534R Slat Access Panel
6241L/6541R Slat Access Panel
C. Procedure
S 212-012-B00
(1) To help you find the applicable leading edge panel, see AMM
12-31-61/201.
S 422-023-B00
WARNING:_______MAKE SURE THAT EACH PANEL IS INSTALLED CORRECTLY. IF FASTENERS ARE NOT TIGHT ENOUGH OR IF TOO MANY ARE MISSING FROM THE ACCESS PANEL, PANEL LOSS MAY OCCUR. THIS MAY CAUSE DAMAGE TO PERSONS AND EQUIPMENT.
(2) Make sure that the leading edge access panels meet the following guidelines:
(a)
One fastener can be missing from a panel if the panel has six to twelve fasteners to keep the panel on the airplane.
(b)
Two fasteners can be missing from a panel if the panel has more than twelve fasteners to keep the panel on the airplane. 1) The two missing fasteners must not be adjacent to each
other.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
57-30-01
ALL ú ú B01 Page 205 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 912-014-B00
(3) To install the fasteners with the applicable torques, see AMM 20-50-11/201.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
57-30-01
ALL ú ú B01 Page 206 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
BOOST PUMP ACCESS DOOR - REMOVAL/INSTALLATION
_____________________________________________
1. General_______
A. This procedure contains two tasks. The first task is the removal of the access door for the boost pump. The second task is the installation of the access door for the boost pump.
B. The access doors for the boost pump lock with clamp latches. The latches have indicators with a groove to show that the latch is locked.
TASK 57-30-11-004-001-B00
2. Remove the Access Door for the Boost Pump (Fig. 401)____________________________________________________
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 机翼 WINGS(21)