(7)
Remove material from the chain guard on the access panel to prevent any interference.
S 414-019
(8)
Install the entry door (Ref 52-11-01/401).
S 424-050
(9)
To attach the door actuator rod (27) to the chain (9), do these steps:
(a)
Close and latch the door.
CAUTION: DO NOT LET THE CHAIN (9) TWIST WHEN YOU INSTALL THE
_______ ACTUATOR ROD (27) TO THE ROD END (28). THIS CAN CAUSE DAMAGE TO THE CHAIN.
(b) Connect the door actuator rod (27) to the rod end (28).
NOTE: The rod end (28) is attached to the chain (9).
____
TASK 52-11-11-404-021
6. DOOR 5; Body Hinge Torque Tube Installation (Fig. 402)
___________________________________
A. Consumable Materials
(1) D00013 - Grease, MIL-G-23827
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-11-11
ALL ú ú 03 Page 415 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(2)
D00015 Grease - Corrosion Preventive, BMS 3-24
B.
Parts
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 402 | 3 |Washer | 52-11-09 | 02 | 375 | | | 4 |Nut | | | 380 | | | 5 |Camplate (Door 5L) | | | 465 | | | 6 |Upper Link (Door 5L) | 52-11-09 | 04 | 24 | | | 7 |Camplate (Door 5L) | 52-11-09 | 02 | 470 | | | 8 |Nut | 52-11-01 | 20 | 210 | | | 9 |Shims | 52-11-09 | 02 | 500 | | | 10 |Bearing Plate | | | 485 | | | 11 |Washer | 52-11-09 | 04 | 51 | | | 12 |Washer | | | 54 | | | 13 |Locknut | | | 57 | | | 14 |Door Open Stop Fitting | | | 129 | | | 15 |Torque Tube Sleeve (Door 5L) | | | 69 | | | 16 |Sprocket | 52-11-07 | 07 | 160 | | | 17 |Chain | 52-11-05 | 04 | 190 | | | 18 |Washer | 52-11-17 | 01 | 10 | | | 19 |Locknut | | | 15 | | | 20 |Snubber Fitting (Door 5L) | | | 20 | | | 21 |Snubber | | | 100 | | | 22 |Nut | 52-11-09 | 04 | 159 | | | 23 |Telescopic Sleeve (Door 5L) | | | 162 | | | 24 |Bolt | 52-11-09 | 02 | 655 | | | 25 |Bearing Plate | 52-11-09 | 04 | 195 | | | 26 |Shim | 53-43-70 | 01 | 315 | | | 27 |Lower Link | 52-11-09 | 04 | 198 | | | 28 |Nut | 52-11-04 | 05 | 175 | | | 29 |Washer | 52-11-09 | 02 | 695 | | | 30 |Bearing Plate | | | 740 | | | 31 |Shim | 52-11-09 | 04 | 204 | | | 32 |Spacer | | | 201 | 2.....….........…...................................…..........…......…........1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-11-11
ALL ú ú 03 Page 416 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 402 | 33 |Bolt | 52-11-09 | 04 | 156 | | | 34 |Nut | | | 159 | | | 35 |Bolt | | | 151 | | | 36 |Nut | 52-11-17 | 01 | 90 | | | 37 |Washer | | | 85 | | | 38 |Structure Link | | | 110 | | | 39 |Bolt | | | 80 | | | 40 |Shim | | | 40 | | | 41 |Cotterpin | 52-11-05 | 04 | 185 | | | 42 |Washer | | | 50 | | | 44 |Rod End | | | 225 | | | 45 |Rod End Attachment Pin | | | 175 | | | 46 |Nut | 52-11-09 | 04 | 66 | | | 47 |Washer | | | 63 | | | 48 |Bolt | | | 60 | | | 49 |Bolt | 52-11-01 | 20 | 200 | | | 50 |Bolt | 52-11-09 | 02 | 370 | 2.....….........…...................................…..........…......…........1
C. References
(1)
52-11-09/401, Main Entry Door No. 5
D.
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
E.
Procedure
S 414-022
(1)
Install the sprocket (16), if you removed it.
(a)
Do these steps to lubricate the assembly: 1) Clean the torque tube sleeve (15) and the sprocket (16).
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 艙門 DOORS 1(89)
