E.
Prepare to adjust the door.
(1)
Remove the escape slide from the door (25-61-35/201).
(2)
Remove the door lining (Ref 52-13-31/401).
(3)
Remove the access panel (1) from the door structure.
S 015-002-B00
S 015-003-B00
S 015-004-B00
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A
737-300/400/500
MAINTENANCE MANUAL
SEE F LATCH ROD SEE E (EXAMPLE) DOOR STOP
TOP GATE
GATE CONTROL ROD
LATCH ROD CONTROL ROD SEE E DOOR LATCH (EXAMPLE) (4 LOCATIONS)
WINDOW HANDLE SEE D TOP HINGE ASSIST HANDLE
ASEE DOOR CENTERING GUIDE ACCESS PANEL MECHANISM FORWARD SEE B HOUSING HANDLE MECHANISM
CONTROL ROD SEE B BOTTOM HINGE
LATCH ROD
BOTTOM GATE
GATE CONTROL ROD
FWD
Aft Entry Door Adjustment
Figure 501 (Sheet 1)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
PLATE CHANNEL AFT FRAME PLATE
2. ADJUSTABLEROLLER FITTING
FLAT WASHER
3.
HEX HEAD BOLT
4.
TRACK
5.
GUIDE
HINGE ARM
SELF-LOCKING NUT FLAT WASHER SPACER
FLAT WASHER (2 LOCATIONS)
3. HEX HEAD BOLT (2 LOCATIONS)
FWD DOOR CENTERING GUIDE
A
TORQUE TUBE
6. RADIUS LINK
HINGE LINK
ATTACH FITTING
HINGE SUPPORT (DOOR STRUCTURE) NUTPLATE (3 LOCATIONS)
10. SNUBBER BOLT
STOP PLATE
9. ROD END BEARING
8. ROD END NUT
WASHER
NUT
7. SNUBBER
TORQUE TUBE
FWD
INBD
LOWER HINGE B
Aft Entry Door Adjustment Figure 501 (Sheet 2)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
31. CONTROL ROD EXTERNAL HANDLE
HOUSING
33. LATCH CRANK
13. ADJUSTMENT NUT
CAM PLATE 14. BEARING
16. TORQUE TUBE
15. TORQUE TUBE CRANK
32. CONTROL 14. BEARING
ROD 12. PUSHROD
13. ADJUSTMENT NUT
11. DOOR CRANK
NOTE: THE MECHANISM IS CLOSED AND LATCHED. INBD FWD DOOR INNER HANDLE HANDLE MECHANISM
C
PIN HINGE LINK
TORQUE TUBE
HINGE ARM
21. GUIDE ARM
GUIDE PLATES
23. KEEPER
22. ADJUSTMENT FITTING 17. ATTACH FITTING
20. ROD END NUT BOLT
19. ROD END BEARING
18. HINGE SUPPORT (DOOR STRUCTURE) FWD
TORQUE TUBE INBD
TOP HINGE D
Aft Entry Door Adjustment
Figure 501 (Sheet 3)
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ALL ú ú B03 Page 506 ú Mar 15/97
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A 737-300/400/500MAINTENANCE MANUAL
CENTER OF STOP BUTTONS
STOP
A
BUTTONS
26. STOP PIN
0.30 INCH
27. LOCK22. STOP DIAMETER
A
SPRING FITTING
NOTE: THE CENTER OF THE STOP PINS MUST BE IN THE SHADED AREA.
1.00 INCH DIAMETER STOP BUTTON A-A
STOP ASSEMBLY
22. STOP FITTING
26. STOP PIN
DOOR FRAME
25. PLATES WITH SERRATIONS
24. LATCH FITTING
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本文链接地址：737-300 400 500 AMM 飞机维护手册 舱门 DOORS 1(69)
