52-34-12
ALL ú ú 04 Page 206 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 822-039
(2)
Adjust the trigger (Detail C).
(a)
Make sure the outside contour of the trigger aligns with the outside contour of the handle within 0.03 inch.
NOTE: This is the aerodynamic flushness tolerance.
____
(b) Add or remove washers between the lock pin and the handle if it is necessary to set this dimension.
S 822-040
(3)
Adjust the handle stop.
(a)
Make sure the distance between the pressure relief door and the cargo door shown is as shown in section A-A.
(b)
Make sure there is 0.06 inch between the lock sector and the latch cam (Detail D).
(c)
Change the rubber washers in the handle stop if it is necessary to get the dimensions above.
(d)
Tighten the nut only until there is no play in the stack of washers.
(e)
See that when the handle is open the lock sectors retract inside the bottom beam of the door.
S 822-041
(4)
Adjust the lock pin (Detail C).
(a)
Put marking ink on the end of the lock pin.
(b)
Operate the handle.
(c)
Look at the lock pin to know the dimension of the overlap between the lock pin and the housing (Detail C).
(d)
Change the washers between the housing and the door if it is necessary to set this dimension.
S 822-042
(5)
Do a test of the force that is necessary to close the handle.
(a)
Use a spring scale to push the handle to the closed position.
NOTE: Put the spring scale approximately 1.0 inch from the
____
top of the handle.
(b) Make sure the force is between 25 and 45 pounds.
S 822-043
(6)
Do a test of the door warning switch.
(a)
Open the handle.
(b)
Make sure the EICAS message FWD CARGO DOOR or AFT CARGO DOOR shows for the applicable door.
(c)
Close the handle.
(d)
Make sure the EICAS message FWD CARGO DOOR or AFT CARGO DOOR does not show for the applicable door.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-34-12
ALL ú ú 03 Page 207 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
TASK 52-34-12-302-026
5. Repairs - Master Latch Lock Handle (Fig. 201)
__________________________________
A. General
(1)
This task is a repair of the master latch lock handle. The repair replaces the rivet through the driver and the handle.
(2)
This task refers to the master latch lock handle as "the handle".
B.
Consumable Materials
(1)
BACR15BB5B-24 - Rivet (MS20470B5-24 optional)
C.
References
(1)
52-34-00/001, Forward/Aft Cargo Door
(2)
IPC 52-34-12
D.
Access
(1)
Location Zone 122 Forward Cargo Container Compartment, Forward Half 142 Aft Cargo Container Compartment
(2)
Access Panel
821R Door - Forward Cargo Compartment
822R Door - Aft Cargo Compartment
E.
Procedure
S 862-044
(1)
Close the door electrically (Ref 52-34-00/001).
S 862-045
(2)
Make sure the latch cams are fully engaged.
NOTE: Look at the latch alignment stripes to make sure the
____
latches are engaged.
S 012-028
(3)
Lift the handle approximately 30 degrees to get access to the rivet.
(4)
Remove the parts of the rivet from the handle and the driver.
S 212-029
(5)
Make sure the holes through the handle and the driver are clean and have no burrs.
S 032-046
S 422-030
CAUTION: USE ONLY THE RIVETS SPECIFIED IN THE LIST OF CONSUMABLE
_______ MATERIALS. IF YOU USE ALTERNATIVE RIVETS YOU CAN CAUSE DAMAGE TO THE HANDLE MECHANISM.
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 3(90)