25-24-36
ALL ú ú 02 Page 207 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 022-041
(8) Remove the latch assembly.
TASK 25-24-36-402-042
9. Latch Assembly Installation (Fig. 201)___________________________
A. Access
(1) Location Zones 100 Upper Half of Fuselage
B. Procedure
S 422-043
(1)
Install the latch assembly.
S 422-071
(2)
Install the bracket on each end of the torque tube.
S 422-045
(3)
Install the screws to attach the latch handle.
S 422-072
(4)
Install the horizontal trim strip.
S 422-073
(5)
Install the screws that connect the latch covers to the bullnose support.
S 422-074
(6)
Install the bullnose.
S 422-076
(7)
Lift the PSU.
S 712-077
(8)
Make sure the door latched correctly.
TASK 25-24-36-822-051
10. Stowage Bin Door Does Not Open (Fig. 201)
______________________________
A. Access
(1) Location Zones
100 Upper Half of Fuselage
B. Procedure
S 822-052
(1)
Put a small diameter rod (less than 0.11 inch) into the manual-release hole and push to release the latch.
S 822-053
(2)
Replace or adjust the latch (AMM 25-24-36/201), if it is necessary.
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25-24-36
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A
737-300/400/500MAINTENANCE MANUAL
TASK 25-24-36-822-054
11. Latch Adjustment (Fig. 201)
________________
A. Access
(1) Location Zones
100 Upper Half of Fuselage
B. Procedure
S 822-062
(1)
Adjust the clearance between the door and the latch pawl covers, if it is necessary
(a)
Adjust the door horizontally in the center of the stowage compartment.
(b)
Lightly close the door and adjust the strikers on the door.
1) The latch pawls must fully engage with the striker rollers on the door.
(c)
When the two latch pawls are fully engaged with the door striker rollers, 1) The latch actuator handle will come out of the latch
housing to the dimension shown on detail C.
(d)
The door is not fully engaged and latched if the dimension is less than the minimum dimension shown on detail C.
(2)
The door must latch at the ends when closed with a light force.
S 712-079
NOTE: A light force must be applied on the latch striker at one
____
of the two ends of the door.
S 422-078
(3) Tighten the fasteners on the striker plate after you complete the latch adjustment.
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25-24-36
ALL ú ú 02 Page 209 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CLASS DIVIDER PARTITION - REMOVAL/INSTALLATION
______________________________________________
TASK 25-24-41-004-070
1. Class Divider Removal (Fig. 401)_____________________
A. Access
(1) Location Zones
107 Forward Half of Cabin
B. Remove the Class Divider
S 024-067
CAUTION:_______BE CAREFUL WITH THE DECORATIVE SURFACES. THE SURFACES CAN BE DAMAGED IF YOU HIT THEM OR GET THEM DIRTY.
(1)
Remove the pin and the hook from the PSU extrusion support.
S 034-007
(2)
Remove the curtain, if installed.
S 024-008
(3)
Remove the screws to remove each support clamp assembly from the A/C extrusion.
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本文链接地址：737-300 400 500 AMM 飞机维护手册 EQUIPMENT/FURNISHINGS(74)
