S 486-007
(2)
Place the track setting fixture over the seat tracks.
S 426-008
(3)
Apply a slight downward pressure. The locating pins of the fixture should fully engage in the holes in the top surface of each track.
S 426-022
(4)
Tighten all the mounting bolts accessible through and around the edge of the fixture.
(5)
Remove the fixture.
(6)
Tighten all the remaining bolts.
S 086-008
S 426-023
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
FLIGHT COMPARTMENT LINING AND INSULATION - MAINTENANCE PRACTICES
________________________________________________________________
1. General
A. This procedure has nine tasks:
(1)
The removal of the Flight Compartment Lining
(2)
The installation of the Flight Compartment Lining
(3)
The removal of the Flight Compartment Insulation
(4)
The installation of the Flight Compartment Insulation
(5)
The approved repair of the Flight Compartment Insulation
(6)
The removal of the Flight Compartment Drip Pan
(7)
The installation of the Flight Compartment Drip Pan
(8)
The removal of the Flight Compartment Pad
(9)
The Installation of the Flight Compartment Pad
TASK 25-11-21-002-001
2. Flight Compartment Lining Removal (Fig. 201)_________________________________
A. Access
(1) Location Zone
101 Control Cabin - Left
102 Control Cabin - Right
B. Procedure
S 012-002
(1) Remove the equipment to get access to the panel, if it is necessary.
CONTROL STAND PANEL
AFT BULKHEAD
LINING PANELS LINING PANELS WITH CRASH PADDING
AFT BULKHEAD
Control Cabin Lining Panels Installation Figure 201
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 012-003
(2)
Remove or loosen the adjacent fitting and panel to release the panel, if it is necessary.
S 022-004
(3)
Remove the fasteners and remove the panel.
TASK 25-11-21-402-005
3. Flight Compartment Lining Installation (Fig. 201)______________________________________
A. Access
(1) Location Zone
101 Control Cabin - Left
102 Control Cabin - Right
B. Procedure
S 422-006
(1)
Put the panel into its position and install it with the mounting screws.
S 412-007
(2)
Tighten the adjacent loose fittings or panels.
S 412-008
(3)
Install the equipment removed for access.
TASK 25-11-21-002-009
4. Flight Compartment Insulation Removal (Fig. 202)_____________________________________
A. Access
(1) Location Zone
101 Control Cabin - Left
102 Control Cabin - Right
B. Procedure
S 012-010
(1)
Remove the lining panels (Refer to par. 1).
(2)
Remove the wire and the tubing clips.
(3)
Disconnect and remove the wire or the tubing where it is necessary.
S 012-011
S 032-012
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本文链接地址：737-300 400 500 AMM 飞机维护手册 EQUIPMENT/FURNISHINGS(39)
