(a)
If the forward edge of the door is not in the limits, adjust the door as follows: 1) Remove the door. 2) Add or remove shims between the fillers and hinges to make
the door smooth with the cowl panel outer surface. 3) Apply primer to all shims that do not have primer on them. 4) Install the door.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-11-05
ALL ú ú C01 Page 208 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 222-039-C00
(5) Make sure there is no free play of the door when the latch is fully locked.
(a) If there is free play, adjust the latch as follows:
1) Open the door.
2) Look for a missing rubber pad on the latch.
a) If the rubber pad is missing, do these steps to replace
the rubber pad: b) Remove the screw and washer from the latch. c) Remove any parts of the old rubber pad from the screw. d) Put a new rubber pad in the latch and install the
washer and screw. 3) Add or remove shims between the latch plate and doubler to remove the free play.
4) If it is necessary to install shims, install the shims as follows: a) Apply primer to all shims that do not have primer on
them. b) Put the shim in the correct position. c) Apply a layer of sealant (BMS 5-95) on the bottom of
the screwheads. d) Install the screws. e) Install and tighten the collar. f) Clean the unwanted sealant from the screwhead. g) Apply fillet seal to the collar with DC 93-006 sealant.
5) Close the door.
S 222-040-C00
(6) Make sure the door aft edge is smooth with the outer surface of the fan cowl panel |0.03 inch (|0.76 mm).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-11-05
ALL ú ú C02 Page 209 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
VORTEX CONTROL DEVICE - REMOVAL/INSTALLATION
____________________________________________
1. General
_______
A. This procedure has two tasks. The first task removes the vortex control device (VCD). The second task installs the vortex control device (VCD). The VCD is installed on the inboard fan cowl panel of each engine.
B. If the inboard fan cowl panel is replaced, the VCD must be removed and installed on the replacement panel. The VCD is not interchangeable between left and right fan cowl panels. The VCD must be installed on the inboard fan cowl panel only.
TASK 71-11-08-004-001-C00
2. Remove the Vortex Control Device (Fig. 401)
________________________________
A. References
(1)
71-11-02/201, Fan Cowl Panels
B.
Access
(1)
Location Zones
506 Engine No. 1 - Inboard Fan Cowl Panel
606 Engine No. 2 - Inboard Fan Cowl Panel
(2)
Access Panels
5737 Engine No. 1 - Fan Cowl Panel
5846 Engine No. 2 - Fan Cowl Panel
C.
Procedure
S 014-002-C00
(1)
Open the applicable fan cowl panel (Ref 71-11-02/201).
S 034-003-C00
(2)
Remove the 16 screws, washers, and collars that attach the VCD to the inboard fan cowl panel.
S 014-004-C00
(3)
Carefully remove the VCD and gasket from the panel.
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 動力裝置 POWER PLANT 2(145)
