52-41-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 494-006-B00
(5)
Put the wood block in a position to hold the weight of the door.
S 034-007-B00
(6)
Disconnect the door from the fuselage at the top hinge.
(a)
Remove the bolt (2, Fig. 401) that holds the hinge arm (5) to the hinge link (1).
(b)
Remove the four bolts that hold the attach fitting (6) to the hinge support (7).
S 034-008-B00
(7)
Disconnect the door from the fuselage at the bottom hinge.
(a)
Remove the bolt (12) that holds the hinge arm (15) to the hinge link (11).
(b)
If it is necessary, remove the snubber (18): 1) Remove the bolts (23) and washers (24) that attach the attach fitting (16) to the hinge support (17). 2) Remove the nut (19), washer (20) and snubber bolt (22) that
attach the snubber (18) to the stop link (21). 3) Remove the snubber (18).
(c)
If the snubber (18) is installed, remove the bolts (23) and washers (24) that attach the attach fitting (16) to the hinge support (17).
S 024-009-B00
(8) Remove the door from the airplane.
NOTE: The door weighs approximately 136 pounds.
____ The door can be lifted from above with a strap attached through the top middle lightening holes of the door inner skin.
S 494-010-B00
(9)
Put the safety barrier across the door opening.
S 034-011-B00
(10)
If you will not install the door again, remove and keep these parts:
(a)
The covers on the hinge arms
(b)
The stop pins with the lock springs
(c)
The door seal (AMM 52-09-13/401).
TASK 52-41-00-404-012-B00
3. Galley Service Door Installation
________________________________
A. Special Tools and Equipment
(1) Safety Barrier, Entry and Galley Doors - 4PRE50-7945
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
B.
C.
D.
E.
F.
A
737-300/400/500MAINTENANCE MANUAL
Standard Tools and Equipment
(1)
Maintenance Stand
(2)
A wood block satisfactory to hold the weight of the door (136
pounds)Consumable Materials
(1)
C00174 Compound - Corrosion Preventive, MIL-C-16713, Class II, Grade 2 (Ref 20-30-21)
(2)
C00259 Primer - BMS 10-11, Type 1References
(1)
AMM 25-61-35/201, Escape Slide Assembly (Door-Mounted)
(2)
SRM 51-20-01, Corrosion Inhibiting Compound
(3)
AMM 52-09-13/401, Bulb-Type Mechanical Seals
(4)
AMM 52-41-00/501, Galley Service Doors
(5)
AMM 52-41-31/401, Galley Service Door Lining and InsulationAccess
(1)
Location Zone 106 Forward Galley Service Door 112 Aft Galley Service Service Door
(2)
Access Panel 4701R Forward Galley Door 4301R Aft Galley Door
Procedure
S 624-013-B00
(1)
Apply the Corrosion Preventive Compound (BMS 3-23) to these areas (SRM 51-20-01):
(a)
The hinges
(b)
Below the scuff plates
(c)
The bottom 3 to 4 inches of the door.
(2)
Remove the door safety barrier, if it is installed.
S 944-015-B00
(3)
Move the door to a position adjacent to the door opening.
(a)
Use the wood block to hold the door.
(b)
Move the door until it is approximately 60 degrees from its open position.
S 094-014-B00
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52-41-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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本文链接地址：737-300 400 500 AMM 飞机维护手册 舱门 DOORS 1(122)
