S 422-059
(2)
Connect the actuator to the hinge quadrant.
S 822-060
(3)
Align the holes in the door with the slots in the hinge quadrant and install the screws.
S 822-024
(4)
Close the door.
(a) Make sure the door aligned correctly with the latches.
S 822-025
(5)
Open the door to examine the door clearances.
S 422-026
(6)
Tighten the screws after the door is aligned correctly.
TASK 25-24-36-002-027
6. Door Removal (Fig. 201)____________
A. Access
(1) Location Zones
100 Upper Half of Fuselage
B. Procedure
S 022-028
(1) Do this task: Hinge Quadrant Removal (AMM 25-24-36/201).
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S 932-061
(2) Make a mark on the edges of the hinges on the door.
NOTE: These marks are necessary to install the door.
____
S 022-056
(3)
Remove the screws and the washers (4 locations) and remove the door from the stowage compartment.
S 932-057
(4)
Make a mark on the edges of the striker plates on the removed door.
NOTE: These marks are necessay for installation of the door.
____
S 022-062
(5)
Remove and keep the striker plate assemblies.
S 022-029
(6)
Remove the door.
TASK 25-24-36-402-030
7. Door Installation (Fig. 201)
_________________
A. Access
(1) Location Zones
100 Upper Half of Fuselage
B. Procedure
S 932-063
(1)
Measure the marks on the removed door.
S 932-064
(2)
Lightly make the location marks for the hinge and striker plate on the new door.
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A 737-300/400/500MAINTENANCE MANUAL
S 422-065
(3) Use the aligned mark to install the striker plates with the screws (4 locations).
(a) Do not fully tighten the screws.
S 422-066
(4) Install the new door assembly on the hinge brackets with the screws and washers (4 locations).
(a)
Use the aligned marks from the Door Removal Procedure (AMM 25-24-36/201) to align the brackets.
(b)
Do not fully tighten the screws.
S 422-032
(5) Do this task: Hinge Quadrant Installation (AMM 25-24-36/201).
TASK 25-24-36-002-033
8. Latch Assembly Removal (Fig. 201)
______________________
A. References
(1) AMM 25-23-61/201, Passenger Cabin Pasenger Service Units (PSU's)
B. Access
(1) Location Zones
100 Upper Half of Fuselage
C. Procedure
S 012-034
(1)
Open the overhead bin door.
S 012-035
(2)
Lower the PSU below the overhead bin (AMM 25-23-61/201).
S 022-067
(3)
Remove the bullnose.
S 022-068
(4)
To remove the horizontal trim strip, push up and pull out the bottom first.
(5)
Remove the two screws which attach the latch handle.
S 022-069
(6)
Remove the screws that attach the latch cover to the bullnose support.
(7)
Remove the bracket on each end of the torque tube.
S 022-038
S 022-070
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