747-400
MAINTENANCE MANUAL

5. IGNITER PLUG 
4. ONE-PIECE  (2 LOCATIONS) 
QUICK-RELEASE 
CLAMP 
(7 LOCATIONS) 
SEE  C 

6. TWO-PIECE QUICK-RELEASE CLAMP (2 LOCATIONS)
SEE D
FWD
B
LOCKSCREW LOCKSCREW
QUICK-RELEASE CLAMP ONE-PIECE  C  TWO-PIECE QUICK-RELEASE CLAMP  D 
Figure 401 (Sheet 2) Ignition Cable Installation 

L76417
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 49-41-05
 ALL  ú ú 04 Page 404 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (d)  
Loosen the coupling nut on the ignition cable (1) until you can disconnect the ignition cable from the igniter plug (5).

 (e)  
Open the three or four one-piece quick-release clamps (4) and two two-piece quick-release clamps (6) that attach the ignition cable (1) to the APU.

 NOTE: There are four one-piece quick-release clamps (4) that
____ attach the ignition cable (1) to the igniter plug (5) at the 5 o'clock position. There are three one-piece quick-release clamps (4) that attach the ignition cable (1) to the igniter plug (5) at the 7 o'clock position.
 (f)  
Remove the ignition cable (1).

 (g)  
Make sure you install all necessary protection covers.

 TASK 49-41-05-404-009
 3. Ignition Cable Installation (Fig. 401)
___________________________
 A. Consumable Materials
 (1)
D50029 Lubricant, Fluorocarbon Release Agent (Spray) - PWC06-005

 B.
Parts ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Ignition Cable Assembly | 49-41-05 | 01 | 30 | 2.......….......…...................................…...........…......….......1

 C.
Access

 (1)  
Location Zones
 221 Control Cabin - Left
 222 Control Cabin - Right
 310 Fuselage - Station 2360 to Station 2792

 (2)  
Access Panels
 317AL APU Access Door - Left
 318AR APU Access Door - Right

 D.
Procedure

 S 424-025
 CAUTION: REMOVE THE PROTECTION COVERS FROM THE OPENINGS AS NECESSARY.
_______ IF YOU DO NOT REMOVE THE PROTECTION COVERS, DAMAGE TO THE APU CAN OCCUR.
 (1)  Do these steps to install the ignition cable (1):
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 49-41-05
 ALL  ú ú 04 Page 405 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 CAUTION:_______ DO NOT LET THE LUBRICANT TOUCH THE CONDUCTORS IN THE
 IGNITION CABLE.  A HIGH RESISTANCE BETWEEN THE IGNITER
 PLUG AND IGNITION EXCITER WILL RESULT IN DAMAGE TO THE

 IGNITION CABLE.
 (a)  
Lightly apply the spray lubricant to the seal seat area at the ends of the ignition cable (1).

 (b)  
Connect but do not tighten the ignition cable (1) to the ignition exciter (2).

 (c)  
Connect but do not tighten the ignition cable (1) to the igniter plug (5).

 CAUTION: DO NOT LET THE BRAID OR FERRULE OF THE IGNITION CABLE MOVE
_______ WHEN YOU TIGHTEN THE TWO COUPLING NUTS. DAMAGE TO THE IGNITION CABLE CAN OCCUR.
 (d)  
Tighten the two coupling nuts on the ignition cable (1) with your fingers plus 1/8 of a turn.

 (e)  
Put the ignition cable (1) in the three or four one-piece quick-release clamps (4) and two two-piece quick-release clamps (6) and close the clamps with the lockscrews.

 NOTE: There are four one-piece quick-release clamps (4) that
____ attach the ignition cable (1) to the igniter plug (5) at the 5 o'clock position. There are three one-piece quick-release clamps (4) that attach the ignition cable (1) to the igniter plug (5) at the 7 o'clock position.
　
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 機載輔助動力 2(71)