747-400
MAINTENANCE MANUAL
DOOR LINING
AA
REVEAL
REVEAL
ACOUSTIC
SEAL
SEAL
FASTENER
0.05 |0.05 INCH
DOOR LINING
DOOR UNLATCHED DOOR LATCHED
A-A
Lining Installation Figure 403
B41116
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52-13-01
ALL ú ú 02 Page 410 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
S 034-006
(5)
Release the carriage latch to unlatch the door latch pin.
S 034-007
(6)
Remove the door from the airplane.
S 494-008
(7)
Install the safety barrier.
TASK 52-13-01-404-009
3. Upper Deck Crew Service Door Installation (Fig. 401)
_________________________________________
A. Special Tools and Equipment
(1)
Rig pin - 5/16-inch diameter, 2.031-inch length
B.
Consumable Materials
(1)
Clear Alodine 1000. Refer to 20-30-02, Finishing Material.
C.
Access
(1)
Location Zone
224 Fwd Upper Deck, RH
(2)
Access Panel
847R Upper Deck Emergency Door, RH
D.
Procedure
S 024-010
(1)
If you install a new door, remove these parts from the old door:
(a)
the door lining, cover, and reveals
(b)
the door seal
(c)
The bottom hinge pin
(d)
The cam follower and the fitting that adjusts the follower to the programming cam
(e)
The door stop pins
S 094-011
(2)
Remove the safety barrier.
S 324-012
(3)
On a new door, do these steps:
(a)
Turn the door handle to the open position.
(b)
Place the door in the door opening with the stop pins centered on the bearing plates within 0.15 inch.
(c)
Remove material from the edge of the door if it is necessary to achieve these dimensions: 1) from 0.06 to 0.12 inch at the forward, aft and top sides of
the door 2) from 0.09 to 0.15 inch at the bottom of the door.
(d)
Remove the door from the opening.
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52-13-01
ALL ú ú 02 Page 411 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 824-013
(4)
Adjust the door stops and latches as follows:
(a)
Retract the stop pins until they are between 0.20 and 0.30 inch 0.20-0.30 inch beyond the face of the pad.
NOTE: Keep the stop pin retainers for subsequent installation.
____
(b)
Loosen the fasteners on the latch fitting to allow vertical and horizontal adjustment.
(c)
Place the door in the opening with the stop pins centered on the bearing plates within 0.15 inch.
(d)
Turn the door handle in the closed direction to engage the latches and support the door.
(e)
Do these steps to adjust the door stops: 1) Turn the stop pins until they touch the bearing plates. 2) Turn the stop pins back one-half turn. 3) Install the retainers in the stop pins.
(f)
Adjust the latch cams to get these dimensions: 1) The door aligns with the fuselage as shown in Figure 402. 2) The clearance between the latch rollers and the latch
fittings is from 0.10 to 0.16 inch. 3) The latch roller touches the latch fitting as shown in Figure 401.
(g)
Tighten the fasteners in the latch fittings to hold them when the door opens.
S 414-014
(5)
Connect the upper and the lower hinges.
(a)
Disconnect the upper control rod from the upper hinge fitting.
(b)
Disconnect the lower control rod at the crank.
(c) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：747-400 AMM 飞机维护手册 舱门 DOORS 1(129)
