(o)
Make a location mark of the stop fitting (14).
(p)
Remove the stop fitting (14) if it is necessary.
(q)
Remove the locknut (19), the washer (18), and the sprocket (16) from the torque tube sleeve (15), if it is necessary.
TASK 52-11-11-004-049
4. DOOR 5; Sprocket Removal (Fig. 402)
________________
A. References
(1)
AMM 25-59-01/401, Main Deck Compartment Cargo Lining Panels
(2)
52-11-14/401, Main Entry Door Hinge Flaps
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MAINTENANCE MANUAL
(3)
AIPC 52-11-07, Fig. 7, AIPC 52-11-09, Fig. 4, AIPC 52-11-17, Fig. 1,
B.
Access
(1)
Location Zone
271 Main Deck, Sta 2040 to Sta 2360, LH
(2)
Access Panel
271AL Panel, Access - Door Maintenance (Door 5, LH)
835L Door - No. 5 Main Entry, LH
C.
Procedure
S 014-009
(1)
Remove the maintenance access panel (1) from the outer side of the airplane, forward of the door.
S 014-010
(2)
Remove the hinge flaps forward of the hinge links (Ref
52-11-14/401).
S 014-062
(3)
Remove the lining from the side of the doorway (AMM 25-59-01/401).
S 024-012
(4)
Remove the sprocket (16).
(a)
Remove the bolt (35) from the telescopic sleeve (23).
(b)
Disconnect the chain (17) from the door actuator rod (43).
1) Turn the door actuator rod (43) to disconnect the rod end (44).
(c)
Remove the bolt (39) that connects the snubber arm (21) to the structure link (38).
(d)
Disconnect the snubber (21) from the torque tube sleeve (15). 1) Move the snubber (21) down the telescopic sleeve (23).
(e)
Remove the snubber fitting (20) and the shims (40).
(f)
Make a location mark of the shims (40) on the structure.
NOTE: Keep the shims for installation.
____
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(g)
Remove the locknut (19) and the washer (18).
(h)
Remove the sprocket (16).
(i)
If you cannot remove the sprocket, do these steps: 1) Remove the bolt (33) from the telescopic sleeve (23). 2) Disconnect the telescopic sleeve (23) from the lower link
(27). 3) Remove the snubber (21) and the telescopic sleeve (23). 4) Remove the sprocket (16).
TASK 52-11-11-404-057
5. DOOR 1; Body Hinge Torque Tube Installation (Fig. 401)___________________________________
A. Consumable Materials
(1)
D00013 - Grease, MIL-G-23827
(2)
D00015 Grease - Corrosion Preventive, BMS 3-24
(3)
A00247 - Sealant, BMS 5-95
B.
Parts
(1)
This table is for the main entry door no. 1.
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~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 |Bolt | 53-43-55 | 01 | 35 | | | 2 |Nut | | | 235 | | | 3 |Bearing Plate | | | 50 | | | 4 |Shim | 52-11-11 | 09 | 15 | | | 5 |Spacer | | | 10 | | | 6 |Nut | | | 55 | | | 7 |Washer | | | 50 | | | 8 |Bolt | | | 45 | | | 9 |Chain | 52-11-05 | 03 | 70 | | | 10 |Nut | 52-11-11 | 09 | 165 | | | 11 |Washer | | | 170 | | | 12 |Lower Link (Door 1L) | | | 215 | | | 13 |Nut | 53-43-55 | 01 | 43 | | | 15 |Camplate (Door 1L) | | | 455 | | | 16 |Camplate (Door 1L) | | | 360 | | | 17 |Bolt | | | 440 | | | 18 |Nut | | | 340 | | | 19 |Bearing Plate (Door 1L) | | | 310 | | | 20 |Bolt | | | 325 | | | 21 |Bolt | 52-11-11 | 09 | 25 | | | 22 |Washer | | | 30 | | | 23 |Nut | | | 35 | | | 25 |Cotterpin | 52-11-05 | 03 | 45 | | | 26 |Washer | | | 60 | | | 28 |Rod End | | | 65 | | | 29 |Rod End Attachment Pin | | | 40 | | | 30 |Release Handle (Door 1L) | | | 90 | | | 31 |Spring | | | 65 | | | 32 |Anchor Plate (Door 1L) | 53-43-55 | 01 | 260 | 2.....….........…...................................…..........…......…........1 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 艙門 DOORS 1(86)
