S 024-010

 (10)
 Carefully move the detector out from below the tubes and the brackets.

 (11)
 Remove the grommets from the element.

 S 034-011
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-17-02
 ALL  ú ú 01 Page 403 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 TASK 26-17-02-404-012
 3.  Install the Detector (Fig. 401)____________________
 A. Standard Tools and Equipment
 (1)  
Bonding Meter (Ref 20-22-01/601)

 B.
References

 (1)  
20-22-01/601, Electrical Bonding

 (2)  
26-17-00/501, Wheel Well Fire Detection System

 (3)  
32-00-00/201, Landing Gear

 (4)  
32-00-30/201, Landing Gear Door Locks

 (5)  
IPC 26-17-02 Fig.02

 (6)  
WDM 26-17-11, Wheel Well Fire Detection

 (7)  
SSM 26-17-01

 C.
Access

 (1)  
Location Zone
 135 Wing Landing Gear Well L.H.
 136 Wing Landing Gear Well R.H.
 137 Body Landing Gear Well L.H.
 138 Body Landing Gear Well L.H.

 (2)  
Access Panel 731 Wing Landing Gear - Center Section Inboard Left 732 Wing Landing Gear - Center Section Outboard Left 741 Wing Landing Gear - Center Section Inboard Right 742 Wing Landing Gear - Center Section Outboard Right

 751 Landing Gear - Aft Inboard Left 752 Landing Gear - Aft Outboard Left 753 Landing Gear - Forw ard Inboard Left 754 Landing Gear - Forward Outboard Left
 761 Landing Gear - Aft Inboard Right 762 Landing Gear - Aft Outboard Right 763 Landing Gear - Forward Inboard Right 764 Landing Gear - Forward Outboard Right
 D. Procedure
 S 414-013
 CAUTION:_______DO NOT TWIST OR PULL THE DETECTOR. DO NOT PUT TENSION ON THE DETECTOR. DO NOT ATTACH THE DETECTOR WITH A CLAMP. IF YOU TRY TO MAKE THE PERMITTED BENDS OR DENTS STRAIGHT, YOU CAN CAUSE A DETECTOR FAILURE.
 (1)  
Put the detector in the approximate position.

 S 434-014

 (2)  
Remove the end caps from the electrical connectors DM691, DM692, DM693, and DM694.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-17-02
 ALL  ú ú 01 Page 404 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 434-026
 (3)  Remove the end fittings from the detector.
 S 434-027
 (4)  Loosely install the detector in the applicable flange fittings.
 S 434-015
 (5)  Install the grommets on the element to make sure each grommet is in
 the center of its related clamp.
 NOTE:____ The clamps and the grommets must attach the element tightly.

 S 034-016
 (6)  
Loosen the clamps and adjust the grommets and the element to install correctly.

 S 434-017

 (7)  
Tighten the clamps.

 S 024-018

 (8)  
Remove the used detector element if one is there.

 S 824-019

 (9)  
Install the new detector element with the most clearance from the units that shake or are moved by torque.

 S 214-020

 (10)
 Make a check of all bends and clearances after you tighten the element into the correct position.

 S 434-021

 (11)
 Tighten the two end fitting connectors to 50 to 60 pound-inches.

 S 434-028

 (12)
 Install the lockwires through the connectors to the flange fittings.

 S 764-022

 (13)
 Make a check of the electrical bond between the connector and the primary structure (Ref 20-22-01/601).

 NOTE: The resistance must not be more than 0.0025 ohms.
____
 S 864-023
 (14) Remove the DO-NOT-CLOSE tag and close this circuit breaker on the main power distibution panel, P6:
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 防火 FIRE PROTECTION 2(17)