0.010
(0.25)
0.005
2
(0.13)
0.005 3
(0.13)
(0.13)
0.005
4
0.005
5
(0.13)
0.005
6
(0.13)
0.005
7
(0.13)
0.005
8
(0.13)
0.005
9
(0.13)
Inboard Aftflap Drive Mechanism Wear Limits
Figure 601 (Sheet 6)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-39
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ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
DESIGN LIMITS WEAR LIMITS
PERMITTED MAXIMUMDIAMETER
INDEX
WEAR DIAMETER
PART NAME DIM.
NO.
MINIMUM MAXIMUM DIMENSION CLEARANCE INCHES INCHES INCHES INCHES (mm) (mm) (mm) (mm)
BUSHING
ID
(26.97)
1.0620
(27.01)
1.0635
(27.14)
1.0685
BUSHING
SHAFT
ID
OD
(36.51)
1.4375
(26.92)
1.0600
(36.55)
1.4390
(26.96)
1.0615
(36.73)
1.4460
(26.80)
1.0550
BUSHING
FLANGED
SHAFT
ID
OD
(14.27)
0.5620
(36.46)
1.4355
(14.40)
0.5670
(36.50)
1.4370
(14.39)
0.5665
(36.28)
1.4285
BUSHING
FLANGED
SCREW
ID
OD
(14.27)
0.5620
(14.24)
0.5605
(14.30)
0.5630
(14.26)
0.5615
(14.39)
0.5665
(14.15)
0.5570
BUSHING
FLANGED
SCREW
ID
OD
(14.27)
0.5620
0.5605
(14.24)
(14.30)
0.5630
(14.26)
0.5615
(14.39)
0.5665
0.5570
(14.15)
BUSHING
FLANGED
SCREW
ID
OD
(14.27)
0.5620
0.5605
(14.24)
(14.40)
0.5670
(14.26)
0.5615
(14.39)
0.5665
0.5570
(14.15)
BUSHING
FLANGED
SCREW
ID
OD
(11.11)
0.4375
0.5605
(14.24)
(11.14)
0.4385
(14.26)
0.5615
(11.23)
0.4420
0.5570
(14.15)
BOLT
BUSHING
ID
OD
(11.07)
0.4360
(15.86)
0.6245
(11.10)
0.4370
(15.89)
0.6255
(10.99)
0.4325
(15.98)
0.6290
BUSHING
BUSHING
ID
OD
0.4375
(11.11)
(15.82)
0.6230
0.4385
(11.14)
(15.85)
0.6240
0.4420
(11.23)
(15.74)
0.6195
BUSHING
FLANGED
BOLT
ID
OD
(20.64)
0.8125
0.4360
(11.07)
(20.66)
0.8135
0.4370
(11.10)
(20.75)
0.8170
0.4325
(10.99)
0.8100
0.8120
0.8075
BOLT
OD
(20.57)
(20.62)
(20.51)
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