Wing Gear Shock Strut Outboard Door Wear Limits
Figure 601 (Sheet 5)
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A
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MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR
DIAMETER *[9] DIM. ALLOWED WEAR MAX ANCE CLEAR-DIAM
MIN MAX
11 BUSHING ID 0.5650 0.5660 0.5680 0.0050 *[5]
BUSHING OD 0.5630 0.5635 0.5610 X
12 BUSHING ID 0.3130 0.3140 0.3165 0.0050 X
BOLT OD 0.3115 0.3120 0.3090 X
13 BUSHING ID 0.4385 0.4390 0.4415 0.0050 *[6]
BOLT OD 0.4365 0.4370 0.4340 X
14 BEARING ID 0.7495 0.7500 0.7525 0.0150 X
BUSHING OD 0.7400 0.7450 0.7375 X
15 BUSHING ID 0.4385 0.4390 0.4415 0.0050 X
BOLT OD 0.4365 0.4370 0.4340 X
16 BUSHING ID 0.5630 0.5635 0.5660 0.0050 *[4]
BOLT OD 0.5610 0.5615 0.5550 X
17 BUSHING ID 0.8630 0.8640 0.8655 0.0050 *[7]
BUSHING OD 0.8605 0.8610 0.8590 X
18 BUSHING ID 0.5630 0.5635 0.5660 0.0050 X
BOLT OD 0.5610 0.5615 0.5580 X
19 BUSHING ID 0.9995 1.0005 1.0030 0.0050 *[8]
BUSHING OD 0.9980 0.9985 0.9955 X
20 BUSHING ID 0.5630 0.5635 0.5660 0.0050 X
BOLT OD 0.5610 0.5615 0.5585 X
Wing Gear Shock Strut Outboard Door Wear Limits
Figure 601 (Sheet 6)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-12-07
ALL ú ú 01 Page 607 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
*[1] INCH. OBTAIN BUSHING. INSTALL BUSHING PER AMM 20-11-01/401 WITH INTERFERENCE FIT OF 0.0003 TO 0.0018
*[2] INCH. OBTAIN BUSHING. INSTALL BUSHING PER AMM 20-11-01/401 WITH INTERFERENCE FIT OF 0.0004 TO 0.0023
*[3] INCH. LINE REAM TO DESIGN LIMITS. OBTAIN BUSHING. INSTALL BUSHING PER AMM 20-11-01/401 WITH INTERFERENCE FIT OF 0.0015 TO 0.0025
*[4] OBTAIN BUSHING. INCH. INSTALL BUSHING PER AMM 20-11-01/401 WITH INTERFERENCE FIT OF 0.0005 TO 0.0020
*[5] OBTAIN BUSHING. INCH. INSTALL BUSHING PER AMM 20-11-01/401 WITH INTERFERENCE FIT OF 0.0015 TO 0.0025
*[6] OBTAIN BUSHING. INCH. INSTALL BUSHING PER AMM 20-11-01/401 WITH INTERFERENCE FIT OF 0.0000 TO 0.0010
*[7] OBTAIN BUSHING. INCH. INSTALL BUSHING PER AMM 20-11-01/401 WITH INTERFERENCE FIT OF 0.0005 TO 0.0025
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