C.
Standard Tools and Equipment
(1)
Modeling Clay
(2)
Rigging Simulator - Escape Slide, C52006-1
(3)
Spring scale, 0-100 pound range
(4)
Vaseline
D.
References
(1)
25-61-35/201, Escape Slide Assembly (Door-Mounted)
(2)
52-09-13/401, Bulb-Type Mechanical Seals
(3)
52-11-31/401, Forward Entry Door Lining and Insulation
(4)
52-61-53/401, Forward Airstair Door Lock Mechanism
E.
Access
(1)
Location Zone
105 Forward Entry Door
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52-11-00
ALL ú ú B03 Page 503 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
TOP GATE
1. DOOR STOP PIN GATE STOP RODS
SEE A
STOP ROD
BEARING
PLATE
GATE CONTROL ROD STOP FITTING (EXAMPLE)
2. LATCH CAM FITTING
SEE B
TOP HINGE
SEE D
4. ACCESS
PANEL
HANDLE MECHANISM
SEE G3. GUIDE TRACK
SEE F
BOTTOM HINGE
SEE E
2. LATCH CAM FITTING
BOTTOM GATE
FORWARD ENTRY DOOR
____ DOOR GATE LINING AND DOOR
NOTE: INTERIOR TRIM PANELS REMOVED.
Forward Entry Door Adjustment Figure 501 (Sheet 1)
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52-11-00
ALL ú ú B02 Page 504 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
1. DOOR
STOP PIN C/L OF STOP FITTINGS
6. DOOR STOP FITTING
THREADED BUSHING
0.20 INCH5. LOCK FWD(5.08 mm)
SPRING A DIAMETER
0.10 INCH
STOP
(2.54 mm)
AFT STOPS FORWARD STOPS
A 0.75 INCH (19.05 mm) DOOR STOP PIN DIAMETER STOP FITTINGS A-A
A
0.09 -0.03/+0.09 INCH ROLLER CLEARANCE
(2.29 -0.76/+2.29
SEE C
8. DOOR SKIN SKIN
7. FUSELAGE
LATCH CAM SHIMS TUBE
LATCH TORQUE FITTING
0.25 INCH
MORE THAN
(6.35 mm) 0.005 INCH
MINIMUM
(0.127 mm)
LATCH ROLLER FITTING WASHERS SHIMS
LATCH
9. LATCH ROLLER ROLLER2. LATCH CAM 0.03 -0.15 INCH FWD
1
FITTING (0.76 -3.81 mm)
INBD LATCH CAM FITTING
ROLLER CLEARANCE
B
C
NOTE:THE CENTERLINE OF THE STOP PINS MUST ALIGN WITH THE CENTERLINE OF THE STOP BUTTONS
WITHIN 0.10 INCH (2.54 mm) AS SHOWN.
1
AT ONE OF THE LATCH FITTINGS (NOT THE TOP FORWARD LATCH FITTING) THE ROLLER CLEARANCE CAN BE FROM 0.03 TO 0.21 INCH (0.76 TO 5.33 mm).
Forward Entry Door Adjustment
Figure 501 (Sheet 2)
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52-11-00
ALL ú ú B07 Page 505 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
HINGE PIN
12. ROD END BEARING
14. GUIDE ARM HINGE ARM
ATTACH BOLT COVER
SHIM
13. HINGE
SUPPORT
TOP SPIGOT
11. ROD END BEARING HINGE
CHECKNUT ARM
10. GUIDE ROLLER
ARM GUIDE
PLATE
11A. KEEPER TORQUE TRIGGER
TUBE 2 FUSELAGE
STRUCTURE
LATCH LEVER
TOP HINGE
D GUIDE ARM
ROLLER BUSHING
TORQUE TUBE
19. HINGE
SUPPORT
HINGE ARM
COVER
HINGE
PIN
18. ATTACH BOTTOM SPIGOT
FITTING
17. ROD END STOP PIN
BEARING HINGE
ARM
STOP PLATE
16. ROD END BEARING 15. DOOR
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