THE BUSHING FLANGE THICKNESS THE SPINDLE THICKNESS IF THE PLATING IS WORN TO THE BASE METAL THE PART HAS FAILED THE WORN PART IS REPAIRABLE. REFER TO THE OVERHAUL MANUAL FOR REPAIR INSTRUCTIONS BEARING AXIAL PLAY REPLACE A BOLT WHEN IT IS NOTCHED TO THE DIMENSION GIVEN. THE BOLT CAN BE TURNED TO REDUCE
THE CLEARANCE BETWEEN THE BOLT AND PIN IF THE TOTAL NOTCH IS NOT MORE THAN THE DIMENSION GIVEN
Inboard Aftflap Wear Limits
Figure 601 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 OUTBOARD FLAP - REMOVAL/INSTALLATION
____________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is one task for the removal and one task for the installation of an outboard flap.
 (1)
The outboard flap removal procedure has these parts:

 (a)
The removal of the outboard flap track fairing

 (b)
The removal of the outboard foreflap

 (c)
The installation of the support equipment

 (d)
The removal of the outboard flap.

 (2)
The outboard flap installation procedure has these parts:

 (a)
A check of the parts for worn areas

 (b)
The installation of the outboard flap

 (c)
The installation of the outboard foreflap

 (d)
The adjustment of the outboard flaps.

 B.  
The outboard flap has three parts, the foreflap, midflap and aftflap. The outboard flap cannot be removed from the airplane as an assembly. To remove the outboard flap, you must disconnect the foreflap from the midflap. The midflap and the aftflap can be removed from the airplane as an assembly. For procedures to remove and install the aftflap only, refer to (AMM 27-51-06/401). You must be careful when you move the flap sections, they are easily damaged.

 C.  
It is important, to save maintenance time, to measure the thickness of the shims that are removed from the midflap. When a replacement midflap is installed, you must examine the shim thickness, to make sure it did not change. If the shim thickness changes, the droop and symmetry will change. The adjustment procedure has steps to correct the thickness of the shims.

 D.  
A piece of all three outboard flap parts have an abrasion resistant teflon layer for protection. If a repair to the teflon layer is necessary, see 51-24-04, Abrasion Resistant Teflon Finish System.

 TASK 27-51-04-004-001
 2.  Remove The Outboard Flap________________________
 A.  Special Tools and Equipment
 (1)
10OHME65B00116, Trailing Edge Flap Spreader Bar

 (2)  
15ME65B00116, Outboard Midflap Strongback (Part of Outboard Trailing Edge Flap Strongback Kit 19ME65B00116)

 (3)
2MIT65B81117-1, Ball and Screw Support

 (4)
G27032, Outbd Spoiler Actuator Lock

 B.  
Standard Tools and Equipment

 (1)
Load Positioner (for 1300 pounds (590 kg)) 3734T52, McMaster-Carr

 P.O.
 Box 54960, Los Angeles, California 90054

 C.  
References

 (1)
AMM 24-22-00/201, Manual Control

 (2)
AMM 27-51-05/401, Outboard Foreflap

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747-400
MAINTENANCE MANUAL

 (3)  
AMM 27-51-28/401, Outboard Flap Carriage

 (4)  
AMM 27-51-31/401, Outboard Flap Track Fairings

 (5)  
AMM 27-51-45/401, Outboard Flap Track Fairing Support

 (6)  
AMM 29-11-00/201, Main Hydraulic Supply System

 (7)  
AIPC 27-51-04, Fig. 1

 (8)  
AIPC 27-51-04, Fig. 10

 (9)  
AIPC 27-51-28, Fig. 1

 (10)
 AIPC 27-51-33, Fig. 2

 (11)
 AIPC 27-51-40, Fig. 1

 (12)
 AIPC 27-51-33, Fig. 3
　
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