27-51-44
 ALL  ú ú 03 Page 414 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 6) Install the cotter pins in the nuts.
 (c)  Attach the drive rod to the fixed drive link (Section A-A): 1) Install the bushing in the fixed drive link. 2) Install the bolt, washers and nut. 3) Tighten the nut to 200-300 pound-inches (23-34 N-m).
 Continue to tighten the nut to align the subsequent cotter pin hole. 4) Install the cotter pin in the nut.
 S 644-045
 (2)  
Lubricate the pin on the attachment fitting.

 S 834-046

 (3)  
Do this task: "Inboard Flap Track Fairing Adjustment" (AMM 27-51-26/501).

 TASK 27-51-44-404-047
 11. Inboard Flap Track Fairing Drive Rod Installation
_________________________________________________
 A. References
 (1)  
AMM 27-51-26/501, Inboard Flap Track Fairings

 B.
Access

 (1)  
Location Zones 563 Outboard Flap Track Fairing, Inboard Flap, LH, (Track No. 3) 561 Inboard Flap Track Fairing, Inboard Flap, LH, (Track No. 4) 661 Inboard Flap Track Fairing, Inboard Flap, RH, (Track No. 5)

 663  Outboard Flap Track Fairing, Inboard Flap, RH, (Track No. 6)
 C. Procedure
 S 424-048
 (1)  Install the drive rod:
 NOTE:  You will attach the drive rod to the midflap fitting during
____ the inboard flap track fairing adjustment.
 (a)  
Adjust the drive rod to the correct length as shown in Fig. 401.

 (b)  
Connect the drive rod to the fixed drive link (Section A-A Fig. 401): 1) Install the bushing in the fixed drive link. 2) Install the bolt, washers and nut. 3) Tighten the nut to 200-300 pound-inches (23-34 N-m).

 Continue to tighten the nut to align the subsequent cotter pin hole. 4) Install the cotter pin.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-44
 ALL  ú ú 02 Page 415 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 834-049
 (2)  Do this task: "Inboard Flap Track Fairing Adjustment" (AMM 27-51-26/501).
 TASK 27-51-44-404-050
 12. Inboard Flap Track Fairing Midflap Fitting Installation
_______________________________________________________
 A. References
 (1)  
AMM 27-51-26/501, Inboard Flap Track Fairings

 B.
Access

 (1)  
Location Zones 563 Outboard Flap Track Fairing, Inboard Flap, LH, (Track No. 3) 561 Inboard Flap Track Fairing, Inboard Flap, LH, (Track No. 4) 661 Inboard Flap Track Fairing, Inboard Flap, RH, (Track No. 5)

 663  Outboard Flap Track Fairing, Inboard Flap, RH, (Track No. 6)
 C. Procedure
 S 424-051
 (1)  
Install the midflap fitting (Fig. 401):

 (a)  
Install the center bolt and washer through the midflap fitting (Section H-H).

 (b)  
Install the spacer and shim on the bolt.

 (c)  
Put the midflap fitting on the midflap and install the bolts and washers (Detail B).

 (d)  
Tighten the three bolts to 36-44 pound-inches (4-5 N-m).

 (e)  
If you did not replace the drive rod or change its length, connect the drive rod (Section F-F):

 NOTE:  Do not install the drive rod if you replaced it or
____ changed its length. You will install the drive rod during the flap track fairing adjustment.
 1) Install the bushing in the midflap fitting. 2) Put the drive rod on the midflap fitting. 3) Install the bolt, washers and nut. 4) Tighten the nut.
 S 834-052
 (2)  Do this task: "Inboard Flap Track Fairing Adjustment" (AMM 27-51-26/501).
 TASK 27-51-44-404-053
 13. Inboard Flap Track Fairing Attachment Fitting Installation
__________________________________________________________
 A. References
 (1)  AMM 27-51-26/501, Inboard Flap Track Fairings
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 5(147)