(b)
A00225 Compound - Sealing, BMS 5-16
(c)
A00141 Compound - Sealing, BMS 5-19, Class BReferences
(1)
AMM 20-30-31/201, Cleaners and Polishes
(2)
AMM 20-30-51/201, Miscellaneous Materials
(3)
AMM 51-31-00/201, Seals and SealingAccess
(1)
Location Zones 208 Forward Cargo Compartment 218 Aft Cargo Compartment
Procedure
S 434-011
(1) Replace the tape on the support structure.
(a) If you use 0.75 inch tape, overlap the tape adhesive side to adhesive side.
NOTE: The optional tape is double back tape.
____ If you use 1.0 inch wide Permacel No. 55 (double back tape) do not overlap the tape.
(b) If you use 2.0 inch wide tape, fold it to be doubled
lengthwise.
NOTE: The optional tape is double back tape.
____ If you use 1.0 inch wide Permacel No. 55 (double back tape) do not fold the tape.
S 434-012
(2)
Put the deck panel in the correct position on the support structure.
(3)
Install the screws for the deck panel.
(4)
Apply sealant to the area for the scuff plate.
(5)
Install the scuff plate.
(6)
Install the cap strips.
S 434-013
S 394-014
S 424-015
S 424-016
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-52-51
ALL ú ú 02 Page 402 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(7) S 424-017Install the splice plates.
(8) S 394-023Seal the gaps and holes (AMM 51-31-00/201).
NOTE:____ Gaps around tiedown track bosses and at the end of splice straps and any other gaps or holes that would allow air leakage must be sealed. The compartment must be virtually airtight to meet the requirements of a Class D cargo compartment. Edges of the cap strips and scuff plates need not be sealed.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-52-51
ALL ú ú 02 Page 403 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
TIEDOWN CAP STRIP DOORWAY
AFT CAP STRIP
FWD
A-A
B-B
OUTBOARD
Forward Cargo Compartment Deck Panel
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-52-51
ALL ú ú 01 Page 404 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A51488
A
737-300/400/500MAINTENANCE MANUAL
CARGO COMPARTMENT LINING AND INSULATION - DESCRIPTION AND OPERATION
___________________________________________________________________
1. General_______
A. The cargo compartment bulkheads, ceilings and sidewalls are lined with fiberglass or aluminum alloy panels and the compartments are furnished with thermal insulation (Fig. 1).
2. Lining______
A. The compartment ceilings and sidewalls are lined with fiberglass panels which are held in place by depressor and cap strips. The cap strips are fastened to the supporting structure by screws. The space between the panel edges and the depressor strips or between the panel edges and the airplane structure is sealed with rubber strips which are cemented to the depressor strips or to the structure. Small cork pads are cemented to the structure where screws pass through panels and cap strips at places that are not at panel edges.
B. The forward cargo compartment forward bulkhead is lined with aluminum alloy panels. Two of the panels are riveted in place and three are held by quarter-turn fasteners, which are spaced around the panel edges. A plastic or sheet metal grille covers the blowout panel opening.
LINING
CARGO COMPARTMENT SECTION
Cargo Compartment Lining and Insulation Location
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 EQUIPMENT/FURNISHINGS(131)
