52-13-21
 ALL  ú ú B01 Page 405 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 AFT ENTRY DOOR GUIDE ARM AND ROLLER - REMOVAL/INSTALLATION
__________________________________________________________
 1.  General_______
 A. This procedure contains two tasks:
 (1)  
The removal of the guide arm from the aft entry door

 (2)  
The installation of the guide arm on the aft entry door.

 TASK 52-13-31-004-001-B00
 2.  Aft Entry Door Guide Arm Removal (Fig. 401)________________________________
 A. Access
 (1)  
Location Zone
 110 Aft Entry Door

 B.
Procedure

 S 034-002-B00
 (1)  
Disconnect the guide arm from the fuselage.

 (a)  
Remove the door release lever (3) and the shim (2).

 (b)  
Open the door sufficiently to get to the hinge link (7).

 (c)  
Remove the retainer ring (6).

 (d)  
Remove the pin (5).

 (e)  
Remove the roller (16) from the guide arm. 1) Open the door fully. 2) Put a punch in the bottom hole of the guide plate (1). 3) Hit the punch to push the roller through the hole in the

 top guide plate.
 NOTE: This removes the bushing also.
____
 S 024-003-B00
 (2)  Disconnect the guide arm from the door.
 CAUTION:_______BE CAREFUL IF YOU MOVE THE DOOR. WITH THE GUIDE ARM DISCONNECTED, YOU CAN CAUSE DAMAGE TO THE DOOR WHEN YOU MOVE IT.
 (a)  
Move the guide arm away from the hinge arm.

 (b)  
Remove the bolts that hold the attach fitting (10) to the hinge support (13).

 (c)  
Remove the guide arm from the door.

 NOTE: The attach fitting stays on the guide arm.
____
 (d)  Remove the attach fitting from the guide arm. 1) Remove the locknut (12), the washer (11), and the bolt (8).
 TASK 52-13-31-404-004-B00
 3.  Aft Entry Door Guide Arm Installation (Fig. 401)_____________________________________
 A. Access
 (1)  Location Zone
 110 Aft Entry Door

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 52-13-31
 ALL  ú ú B01 Page 401 ú Jul 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

LATCH ROLLER
(EXAMPLE)

TOP HINGE ASSEMBLY SEE A
FWD  2. SHIM
3. DOOR
 RELEASE 
LEVER 
5. PIN  6. RETAINER 
RING 
7. HINGE LINK 4. GUIDE
 ARM 
12. LOCKNUT 
11. WASHER 

9. HINGE ARM
16. ROLLER  1. GUIDE PLATES
TORQUE TUBE
18. KEEPER CHANNEL
17. ADJUSTMENT FITTING
10. ATTACH FITTING15. ROD END NUT
14. ROD END BEARING
8. BOLT
13. HINGE SUPPORT FWD(DOOR STRUCTURE)
TORQUE TUBE
INBD TOP HINGE ASSEMBLY
A
Aft Entry Door Guide Arm Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-13-31
 ALL  ú ú B01 Page 402 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 B. Consumable Materials
 (1)  
D00013 Grease - MIL-G-23827

 C.
Procedure

 S 644-005-B00
 (1)  
Put a layer of grease on the roller (16).

 S 424-006-B00

 (2)  
Connect the guide arm to the fuselage.

 (a)  
Align the holes in the guide arm with the holes in the guide plate.

 (b)  
Install the roller in the bushings in the guide arm.

 (c)  
Install the spring clip in the roller, if it is necessary.

 (d)  
Install the bushing in the top guide plate.

 (e)  
Install the door release lever (3) and the shim (2).

 S 434-007-B00
　
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