(2)  
Access Panels
 8203, 8703 Outboard Midflap Access Panel
 8204, 8704 Outboard Midflap Access Panel
 8205, 8705 Outboard Midflap Access Panel
 8206, 8706 Outboard Midflap Access Panel

 D.  
Procedure

 S 026-002
 (1)  
Remove the outboard aftflap (Ref 27-51-39/401).

 S 226-003

 (2)  
Examine the bolt and bushing that attach the bottom flight rollers (Fig. 601):

 (a)  
Remove the bolt, washer, nut and bushing from the aftflap support fitting.

 (b)  
Use a micrometer to measure the diameters of the bolt and bushing.

 (c)  
Compare the dimensions you measured with the permitted dimensions shown in Fig. 601.

 (d)  
Replace the parts that are not in the tolerance.

 (e)  
Install the bushing, bolt, washers and nut.

 (3)  
Install the outboard aftflap (Ref 27-51-39/401).

 S 426-004
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-39
 ALL  ú ú 01 Page 601 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
TOP FLIGHT ROLLER  1. BUSHING/BOLT
AFTFLAP TRACK
AFTFLAP

A
A
FWD
INBD
BOTTOM
FLIGHT
ROLLER

(EXAMPLE, 2 PIECE BUSHING)
A-A
2. BUSHING/BOLT TOP FLIGHT ROLLER
AFTFLAP TRACK  AFTFLAP
B
B  FWD
INBD
BOTTOM
FLIGHT
ROLLER

(EXAMPLE, 1 PIECE BUSHING)  B-B
DESIGN LIMITS
WEAR LIMITS PER-
MAXDIAMETER REPLACE
REPAIR INDEX MITTED DIA WORN WORN REPAIRWEAR CLEAR-
NO.
PART NAME DIM.
MIN
MAX
PART PART INSTRDIM.
ANCE
BUSHING
ID 0.2490
0.2510
0.2545
1

X
BOLT

0.0050
OD
X X
0.2485
0.2495
0.2440
0.2490 2 0.2510 2
0.2545 2 0.0050
BUSHING
ID
0.3125 3

0.3145 3 0.3190 3 2 4
2

X
0.2485 4 0.2495 4
0.2440 4 0.0070
BOLT

OD
X
X 0.3110 5
35
0.3120 5 0.3055 5
1 MOST OUTBOARD FLAP TRACK 4  P/N 69-38849-2, P/N 69-38849-8
2 P/N 69-37234-9, P/N 69-37234-19 5  P/N 69-38849-10, P/N 69-38849-503,
P/N 69-38849-502

3 P/N 69-37234-26
Outboard Aftflap Wear Limits
Figure 601

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-39
 ALL  ú ú 01 Page 602 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 OUTBOARD MIDFLAP CARRIAGE - REMOVAL/INSTALLATION
________________________________________________
 1.  General
_______
 A.  There are two tasks in this procedure. There is a task for the removal and a task for the installation of the outboard midflap carriage. This procedure is applicable to the two carriages on an outboard midflap. It is necessary to remove the midflap to remove a carriage.
 TASK 27-51-44-004-001
 2.  Outboard Midflap Carriage Removal (Fig. 401)
_________________________________
 A.  References
 (1)  
27-51-34/401, Outboard Trailing Edge Flap

 B.  
Access

 (1)  
Location Zone 307, 407 Wing Trailing Edge Outboard Flap and Spoilers

 (2)  
Access Panels
 8207, 8707 Outboard TE Flap Access Panel
 8208, 8708 Outboard TE Flap Access Panel

 C.  
Procedure

 S 034-002
 (1)  
Do this task: "Outboard Trailing Edge Flap Removal" (Ref 27-51-34/401).

 S 014-003

 (2)
Remove the access panels from the top surface of the midflap.

 S 024-004

 (3)  
Remove a carriage from the outboard midflap:

 (a)  
Remove the bolt that attaches the safety link to the inboard side of the carriage.

 (b)  
Remove the special bolt that attaches the spherical bearing to the carriage.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 4(67)