EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-12-07
ALL ú ú 01 Page 601 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
SEE F
SEE G
WING GEAR SHOCK STRUT SEE A OUTBOARD SEE D DOOR
SEE E
WING GEAR
SHOCK STRUT SHOCK STRUT
DOOR FAIRING INBOARD DOOR
FWD
WING GEAR SHOCK STRUT
WING GEAR SHOCK STRUT OUTBOARD DOOR LINKAGE ROD
SEE B
SEE C
WING GEAR SHOCK STRUT OUTBOARD DOOR
INBD FWD
A
Wing Gear Shock Strut Outboard Door Wear Limits
Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-12-07
ALL ú ú 01 Page 602 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
Wing Gear Shock Strut Outboard Door Wear Limits
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-12-07
ALL ú ú 01 Page 603 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
8. BUSHING/BUSHING (2 LOCATIONS)
7.
CLEVIS
10.
WING LANDING GEAR INBOARD DOOR ASSEMBLY
WING LANDING GEAR OUTBOARD DOOR ASSEMBLY
INBOARD DOOR ASSEMBLY
OUTBOARD DOOR ASSEMBLY
FORWARD AND MID HINGE
Wing Gear Shock Strut Outboard Door Wear Limits
Figure 601 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-12-07
ALL ú ú 01 Page 604 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
HINGE SUPPORT FITTING ASSEMBLY
15. BUSHING/BOLT
HINGE FITTING
FORWARD HINGE F
18. BUSHING/BOLT
14. BEARING/BUSHING
13. BUSHING/BOLT (2 LOCATIONS)
17. BUSHING/BUSHING
16. BUSHING/BOLT WING LANDING GEAR OUTBOARD DOOR ASSEMBLY
HINGE SUPPORT FITTING ASSEMBLY
19.
BUSHING/BUSHING
20.
BUSHING/BOLT
HINGE FITTING
WING LANDING GEAR OUTBOARD DOOR ASSEMBLY
AFT HINGE
Wing Gear Shock Strut Inboard Door Wear Limits
Figure 601 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-12-07
ALL ú ú 01 Page 605 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR
DIAMETER MITTED PER-DIM. WEAR *[9] ANCE MAX CLEAR-DIAM
MIN MAX
1 BUSHING ID 0.5000 0.5005 0.5040 0.0050 *[1]
BOLT OD 0.4990 0.4995 0.4955 X
2 BEARING ID 0.4995 0.5000 0.5040 0.0050 X
BOLT OD 0.4990 0.4995 0.4950 X
3 BUSHING ID 0.7500 0.7515 0.7530 0.0050 *[2]
BUSHING OD 0.7480 0.7490 0.7455 X
4 BUSHING ID 0.5015 0.5030 0.5040 0.0050 X
BOLT OD 0.4990 0.4995 0.4980 X
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 起落架 LANDING GEAR 2(114)
