曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

 B.  In the second part you make sure that the fasteners which attach the failsafe link to the fitting are correctly tightened.
 C.  In the third part you make sure the the main carriage retainer nut is correctly tightened.
 TASK 27-51-28-206-001
 2.  Outboard Flap Carriage Inspection_________________________________
 A.  Standard Tools and Equipment
 (1)  
Micrometer - 1 to 2 inch (2 to 5 cm), To measure inner and outer dimensions

 (2)  
Micrometer - 3 to 4 inch (7 to 10 cm), To measure inner and outer dimensions

 (3)  
Vernier Caliper

 B.  
References

 (1)  
27-51-28/401 - Outboard Flap Carriage

 (2)  
29-11-00/201, Main Hydraulic Supply System

 C.  
Access

 (1)  
Location Zone 567 Outboard Flap Track Fairing, Outboard Flap, LH (Track No. 1) 565 Inboard Flap Track Fairing, Outboard Flap, LH (Track No. 2) 665 Inboard Flap Track Fairing, Outboard Flap, RH (Track No. 7)

 667  Outboard Flap Track Fairing, Outboard Flap, RH (Track No. 8)
 D.  Examine The Dimensions Of The Carriage Bearings.
 S 026-002
 (1)  
Remove an outboard flap carriage (Ref 27-51-28/401).

 S 226-003

 (2)  
Measure the carriage bearings:

 (a)  
Remove the parts.

 (b)  
Use a micrometer or a vernier caliper to measure the parts.

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

 (d)  
Repair or replace all parts which are not in the tolerance, as shown in Fig. 601.

 (e)  
Install the parts.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-28
 ALL  ú ú 01 Page 601 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 426-004
 (3)  
Install the outboard flap carriage (Ref 27-51-28/401).

 E.
Examine The Torque Of The Failsafe Link Fasteners

 S 866-005
 (1)  
Pressurize hydraulic systems No. 1 and 4 (Ref 29-11-00/201).

 S 866-006

 (2)  
Put the flap control lever in the 30 unit detent to extend the flaps.

 S 226-007

 (3)  
Do a check of the torque of the failsafe link fasteners:

 (a)  
Tighten the nut to 230-250 pound-inches (26-28 N-m).

 (b)  
Loosen the nut one quarter turn.

 S 866-008
 (4)
Put the flap control lever in the UP detent to retract the flaps.

 S 866-009

 (5)  
Release the pressure in hydraulic systems No. 1 and 4
 (Ref 29-11-00/201).

 F.
Examine The Torque Of The Main Carriage Retainer Nut

 S 866-010
 (1)  
Pressurize hydraulic systems No. 1 and 4 (Ref 29-11-00/201).

 S 866-011

 (2)  
Put the flap control lever in the 30 unit detent to extend the flaps.

 (3)  
Remove the lockbolt from the retainer nut.

 (4)  
Remove the locknut and retainer from the retainer nut.

 (5)
Make sure the retainer nut is tightened to 300 pound-feet (407 N-m).

 S 026-015
 S 026-016
 S 226-012
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-28
 ALL  ú ú 01 Page 602 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (6)  S 426-017Install the locknut and retainer on the retainer nut.
 (7)  S 426-018Install the lockbolt on the retainer nut.
 (8)  S 426-019Install lockwire.
 (9)  S 866-013Put the flap control lever in the UP detent to retract the flaps.
 S 866-014

 (10) Release the pressure in hydraulic systems No. 1 and 4 (Ref 29-11-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 www.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(44)