end (18) to the support fitting (8) up and down easily.

 (d)  
If you can move the bolt easily, then there is no initial load on the the guide arm (2) and the guide arm length is correct.

 (e)  
If you can't move the bolt easily, do these steps: 1) Loosen the locknuts (19) and (21). 2) Turn the length adjustment fitting (20) to adjust the guide

 arm (2) length sufficiently. 3) Make sure the bolt (24) is free to move. 4) Tighten the larger locknut (21) to 650-700 pound-inches and
 the smaller locknut (19) to 350-400 pound-inches.
 (f)  
Install the washer (22) and nut (23) on the bolt (24).

 (g)  
Tighten the bolt (24) which connects the guide arm (2) to the support fitting (8).

 (8)  
Open the door to the cocked position with the external handles.

 S 824-014

 (9)  
Adjust the length of the cocking crank pushrod to let the external handles go in the door recess, if it is necessary.

 S 014-013
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A
747-400 MAINTENANCE MANUAL
 G. Restore the Airplane to Normal.
 S 414-016
 (1)  
Install the hinge covers (5).

 (a)  
DOOR 1; Do these steps: 1) Apply the sealant around the edge of the hinge cover if it

 is necessary (AMM 51-31-01/201). 2) Install the cover (5). 3) Install the bolts (3) and the washers (4) that hold the
 cover (5) on.
 (b)  DOOR 5; Do these steps: 1) Apply the sealant around the edge of the hinge cover if it
 is necessary (AMM 51-31-01/201). 2) Install the cover (5). 3) Install the bolts (3), (6), and (7) and the washers (4)
 that hold the cover (5) on.
 S 414-020
 (2)  Install the door lining (AMM 52-11-02/401).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 MAIN ENTRY DOOR ACTUATOR AND CHAIN - REMOVAL/INSTALLATION
_________________________________________________________
 1.  General_______
 A.  This procedure has two tasks. The first is the removal of the power actuator and the chain on the main entry door. The second is the installation of the power actuator and the chain on the main entry door.
 TASK 52-11-05-004-001
 2.  Entry Door Actuator and Chain Removal (Fig. 401)_____________________________________
 A.  Special Tools and Equipment
 (1)  
BACP18AM6B28H - Pin, Mode Selector Lockout

 (2)  
B52009-10 - Safety Pin Set, Emergency Power System, Entry Doors (PREFERRED)

 NOTE: The safety pin set contains 10 pin assemblies (P/N B52009-2).
____ Each pin assembly consists of 2 pins connected by a lanyard with a streamer attached. If a pin assembly is not available, you can use 2 bolts, 3/16-inch diameter by 1-1/4-inch grip. Install one bolt above and one below the reservoir knife plunger. Attach the bolts in position to prevent their loss. Attach a streamer as a reminder that you must remove the bolts to operate the reservoir.
 (3)  MIT65B04430-1 - Safety Pin, Power Reservoir, Main Entry Door (ALTERNATE IF PIN SET P/N B52009-10 IS NOT AVAILABLE)
 NOTE: The safety pin is a set of 2 pins connected by a lanyard with
____ a streamer attached. If a safety pin is not available, you can use 2 bolts, 3/16-inch diameter by 1-1/4-inch grip. Install one bolt above and one below the reservoir knife plunger. Attach the bolts in position to prevent their loss. Attach a streamer as a reminder that you must remove the bolts to operate the reservoir.
 B.  References
 (1)  
AMM 25-22-01/401, Main Passenger Cabin Ceiling Access Panel

 (2)  
DOOR 1;
 AIPC 52-11-01, Fig. 4, AIPC 52-11-05, Fig. 3

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