757
MAINTENANCE MANUAL
ANCHOR PLATE (EXAMPLE)
SEE
A
(EXAMPLE)
CARGO NET TIEDOWN FITTING (EXAMPLE)
A
Lower Lobe Cargo Compartments
Figure 1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-50-00
ALL ú ú 01 Page 2 ú Jun 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
4. Operation - Zipper for the Station 1640 Bulkhead
________________________________________________
A. Procedure - Zipper Operation
(1)
Do the steps that follow to close the zipper:
(a)
Hold the access panel in the closed position with the top snap before you operate the zippers.
(b)
Pull the zipper tabs parallel to the line of the zipper, at an angle.
(2)
Do the steps that follow to open the zipper:
(a) Pull the zipper down the full length of the zipper travel to open the flap.
NOTE: Do not step on the flap when you access the bulkhead.
____
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-50-00
ALL ú ú 03 Page 3 ú Mar 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
CARGO COMPARTMENT - INSPECTION/CHECK
____________________________________
1. General
_______
ú A. This procedure gives instruction for the inspection of the fiberglass
ú liner on the vertical and sloping sidewalls, bulkhead, and ceiling in the
ú cargo compartment.
TASK 25-50-00-206-001
2. Compartment Lining - Inspection/Check
_____________________________________
A. References
(1)
AMM 25-00-00/801, Equipment/Furnishings, Approved Repairs
(2)
AMM 25-50-01/401, Cargo Compartment Ceiling Lining
(3)
AMM 25-50-02/401, Cargo Compartment Sidewall Lining
(4)
AMM 25-50-03/401, Bulkhead Lining
(5)
AMM 25-50-09/801, Cargo Compartment Lining (Fiberglass)
B. Access
(1) Location Zones
121/122 Forward Cargo Compartment
153/154 Aft Cargo Compartment
161/162 Bulk Cargo Compartment
C. Procedure
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-50-00
ALL ú ú 01.1 Page 601 ú Sep 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
S 416-025
CAUTION: DO NOT GET CORROSION-INHIBITING COMPOUNDS (CIC) ON THE
_______ INSULATION BLANKETS. APPLY CIC (BMS 3-23, BMS 3-26, BMS 3-29, OR EQUIVALENT) ONLY TO METALLIC AIRPLANE COMPONENTS. DO NOT ALLOW CIC TO CONTAMINATE NON-METALLIC MATERIALS. CIC WILL HAVE AN ADVERSE AFFECT ON THE FLAMMABILITY CHARACTERISTICS OF INSULATION BLANKETS.
(1) If Corrosion-inhibiting Compounds (CIC) contamination of insulation blankets occurs, adhere to the following steps: (a) Replace the insulation blanket if CIC contamination occurs along a seam. (b) For all areas except along seams, remove the CIC with Biogenic SE377C, Alphatic Naphtha, Citra-Safe, or equivalent.
NOTE:____ If the CIC can not be removed, replace the blanket.
S 016-026
(2) In order to prevent Corrosion-inhibiting compounds (CIC) contamination of insulaton blankets, obey the following steps prior to blanket installation:
NOTE: Adjust the following steps ventilation times upward to____ achieve satisfactory drying depending on the temperature, humidity, and quantity of CIC. (a) Ventilate areas, after application of CIC such as BMS 3-23, for a minimum of one hour.
(b) Ventilate areas treated with CIC such as BMS 3-26 or BMS 3-29 for a minimum of four hours.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 EQUIPMENT/FURNISHINGS 2(16)
