NWS1A-4
NWS1B-4
NWS1A-2 LH
CABLE DRUMS  CABLE(INBOARD GROOVE) COMPENSATORNWS1B-2 RH ASSEMBLY(OUTBOARD GROOVE)
NWS1A-3 LH A NWS1B-3 RH
TRUNNION PIVOT LINK
NWS2A-1
(FORWARD
GROOVE) NWS2B-1 (AFT GROOVE)
FWDNWS2B-2 (SAME CABLE VIEW LOOKING DOWN AND AFT
NWS2A-2AS NWS2A-2)
B
FWD
A-A
Nose Wheel Steering System Control Cables Figure 7 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-00-40
 ALL  ú ú 01 Page 16 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

REF CABLE  REQ NO.  INCH) 2 (TO NEAREST TENTH LENGTH  2FITTINGS 
1  2 
NWS1A-1  1  249.8  MS21260L3RH  BACT14A3 
NWS1A-2  1  22.5  MS21260S3RH  BACT14A3 
NWS1A-3  1  40.5  MS21260S3LH  BACT14A3 
NWS1A-4  1  122.2  MS21260L3LH  BACT14A3 
NWS1B-1  1  341.7  MS21260L3LH  BACT14A3 
NWS1B-2  1  22.5  MS21260S3RH  BACT14A3 
NWS1B-3  1  114.7  MS21260S3LH  BACT14A3 
NWS1B-4  1  148.0  MS21260L3RH  BACT14A3 
NWS2A-1  1  28.0  MS21260S3RH  BACT14A3 
NWS2A-2  1  1122.7  MS21260S3LH  MS21260S3RH 
NWS2B-1  1  27.8  MS21260S3LH  BACT14A3 
NWS2B-2  1 

CABLE SIZE - 3/32 7 X 7
MS21260  BACT14A

BACC2C CABLE

MS21260S3LH  BACT14B3 BALL
MS21260S3RH

NWS2A-2 AND NWS2B-2 ARE ONE CONTINUOUS CABLE.
REFERENCE ONLY. FOR SPECIFIC PART NUMBER, LENGTH, MATERIAL, AND END FITTING, REFER TO CURRENT IPC.
Nose Wheel Steering System Control Cables
Figure 7 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-00-40
 ALL  ú ú 01 Page 17 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

DOUBLER
NOTE: LEFT HAND SHOWN RIGHT HAND OPPOSITE.

Brake Cable Air Pressure Seal Locations
Figure 8

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-00-40
 ALL  ú ú 01 Page 18 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

SEE A
SHIELD AND COVER
CABLE LGV1B  PULLEY 
STA 1372  AIR PRESSURE SEALS RISER BLOCK RISER BLOCK  CABLE LGV1A  FWD 
PRESSURE DECK RBL 120 
WL 186.3 
A 
Landing Gear Control Cable Air Pressure Seal Location Figure 9 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-00-40
 ALL  ú ú 01 Page 19 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 LANDING GEAR LUBRICATION RETAINER - REPAIR
__________________________________________
 1.  General_______
 A.  This procedure contains a task to repair the lubrication retainers for the landing gear.
 B.  The task gives steps to install the alternate lubrication fittings in the nylon lubrication retainers. The retainers are in the holes of the landing gear joints.
 TASK 32-00-50-308-001
 2.  Landing Gear Lubrication Retainer Repair (Fig. 801)________________________________________
 A.  Access
 (1)  
Location Zone
　
中國航空網(wǎng) 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 起落架 LANDING GEAR 1(39)