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时间:2011-04-14 10:11来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Remove the cross bolt (8) and remove the latch roller cranks (14) and spacers (11) .


 NOTE: Write the position and number of the spacers (11) at
____ each latch roller crank (14) for installation.
 (c)  
Remove the bearings (10) from the bearing housing (9) at each end of the torque tube (6).

 (d)  
Remove the cam (17) and the cam saddle (16) (on the lower torque tubes only).


 NOTE: Identify the position of the cam (17) for the
____
 installation.

 (e)  
Remove the cross bolt (23) on the torque tube crank (2).

 (f)  
Put the torque tube (6) through the bearing housing (9) and remove it from the door assembly.


 TASK 52-11-19-404-008
 3. Latch Torque Tube Installation (Fig. 401)
______________________________
 A. Special Tools and Equipment
 (1)  
BACP18AM6B28H Pin, Mode Selector Lockout

 (2)  
DJ65B04957 Drill Jig, Latch Torque Tube Crank

 (3)  
TME65B04308 Dolly, Cargo/Main Entry Door

 B.
Consumable Materials

 (1)  
D00013 Grease, MIL-G-23827

 (2)  
C00308 Compound, Corrosion Preventive


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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (3)
A00952 Sealant, BMS 5-19

 (4)
C00259 Primer, BMS 10-11, Type I

 C.
Parts

 (1)
This table is for the Main Entry Door No. 1 (Upper Torque Tube).


 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 |Upper Control Rod | 52-11-13| 01 | 80 | | | 2 |Torque Tube Crank (Door 1L) | 52-11-19| 05 | 185 | | | 3 |Nut | | | 50 | | | 4 |Washer | | | 45 | | | 5 |Bushing | | | 175 | | | 6 |Torque Tube | | | 435 | | | 8 |Crossbolt | | | 20 | | | 10 |Bearing | | | 80 | | | 11 |Spacers | | | 75 | | | 12 |Nut | | | 30 | | | 13 |Washer | | | 25 | | | 14 |Latch Roller Crank | | | 70 | | | 19 |Bolt | 52-11-13| 01 | 65 | | | 20 |Lower Control Rod | | | 85 | | | 21 |Washer | | | 75 | | | 22 |Nut | | | 80 | | | 23 |Crossbolt | 52-11-19| 05 | 35 | 2.....….........…...................................…..........…......…........1
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 |Upper Control Rod | 52-11-13| 01 | 90 | | | 2 |Torque Tube Crank | 52-11-19| 05 | 205 | | | 3 |Nut | | | 50 | | | 4 |Washer | | | 45 | | | 5 |Bushing | | | 200 | | | 6 |Torque Tube | | | 135 | | | 7 |Nut | | | 270 | | | 8 |Crossbolt | | | 20 | | | 10 |Bearing | | | 80 | | | 11 |Spacers | | | 75 | | | 12 |Nut | | | 30 | | | 13 |Washer | | | 25 | | | 14 |Latch Roller Crank | | | 70 | | | 15 |Washer | | | 265 | | | 16 |Cam Saddle | | | 275 | | | 17 |Lockout Cam | | | 280 | | | 18 |Bolt | | | 260 | | | 19 |Bolt | 52-11-13| 01 | 70 | | | 20 |Lower Control Rod | | | 120 | | | 21 |Washer | | | 75 | | | 22 |Nut | | | 80 | | | 23 |Crossbolt | | | 35 | 2.....….........…...................................…..........…......…........1
 (2) This table is for the main entry door No. 5 (upper torque tube).
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