52-13-00
ALL ú ú B01 Page 804 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
STOP FITTING
SEE A
FWD
BEARING PLATE
CRACK
45`
45`
PARTING LINE
STOP FITTING
A
Aft Entry Door Approved Repair Figure 802
F57283
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52-13-00
ALL ú ú B01 Page 805 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(b)
Make a spotface in the stop fitting to give a 0.002 to 0.012 inch clearance with the bearing plate.
(c)
Prepare the surfaces (Method III) and apply Alodine (AMM 51-21-41/701 and AMM 51-21-21/701).
(d)
Apply the primer (AMM 51-21-99/701).
S 428-017-B00
(5) Bond the bearing plate to the stop fitting with the BMS 5-95 sealant.
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52-13-00
ALL ú ú B01 Page 806 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
AFT ENTRY DOOR HINGE ARMS - REMOVAL/INSTALLATION
________________________________________________
1. General
_______
A. This procedure contains two tasks:
(1)
The removal of the hinge arms from the aft entry door
(2)
The installation of the hinge arms on the aft entry door.
TASK 52-13-11-004-001-B00
2. Aft Entry Door Hinge Arm Removal (Fig. 401)
________________________________
A. References
(1)
25-61-35/201, Escape Slide Assembly (Door-Mounted)
(2)
52-13-00/401, Aft Entry Door
(3)
52-13-31/401, Aft Entry Door Lining and Insulation
B.
Access
(1)
Location Zone
110 Aft Entry Door
C.
Procedure
S 014-002-B00
(1)
Remove the escape slide assembly from the door (Ref 25-61-35/201).
S 014-003-B00
(2)
Remove the lining from the door (Ref 52-13-31/401).
S 014-004-B00
(3)
Remove the door from the airplane (Ref 52-13-00/401).
S 034-005-B00
(4)
Remove the external handle from the door.
(a)
Remove the cam plate (10).
(b)
Remove the bolts in the recess for the external handle.
(c)
Remove the external handle (6).
S 034-006-B00
(5)
Remove the hinge arm cover from each hinge arm (18).
S 034-007-B00
(6)
Remove the access panel (2) from the door.
S 034-008-B00
(7)
Disconnect the torque tube from the hinge pins (Fig. 402).
(a)
Remove the bolts in the torque tube (3, Fig. 402) and the hinge pins (1).
(b)
Move the sleeves along the torque tube.
S 034-009-B00
(8) Remove the twelve bolts (8, Fig. 401) that hold the housing for the handle mechanism.
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52-13-11
ALL ú ú B02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500
MAINTENANCE MANUAL
TOP GATE GATE CONTROL ROD LATCH ROD
1. CONTROL ROD
DOOR HANDLE
2.
ACCESS PANEL
3.
CONTROL ROD
LATCH ROD GATE CONTROL ROD BOTTOM GATE
TOP HINGE SEE B
SLEEVE
5. TORQUE TUBE
4. HOUSING
SEE ASLEEVE
BOTTOM HINGE SEE C
FWD
SNUBBER
Aft Entry Door Hinge Arm Installation
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