BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
DESIGN LIMITS WEAR LIMITS
REPLACE WORN PART REPAIRREPAIR WORN PART INSTR
4
X
4
X
PERMITTED MAXIMUMDIAMETER
INDEX
WEAR DIAMETER
PART NAME DIM.
NO.
MINIMUM MAXIMUM DIMENSION CLEARANCE INCHES INCHES INCHES INCHES (mm) (mm) (mm) (mm)
FLANGED
BUSHING
ID
(11.11)
0.4375
(11.14)
0.4385
0.4420
(11.23)
BUSHING
BOLT
ID
OD
0.5620
(14.27)
(11.07)
0.4360
0.5630
(14.30)
(11.10)
0.4370
0.5665
(14.39)
(10.99)
0.4325
0.5605
0.5615
0.5575
BUSHING
OD
(14.24)
(14.26)
(14.16)
0.005
20
(0.13)
(0.13)
0.005
21
THE REPLACEMENT BUSHING CAN HAVE AN OVERSIZE OD TO +0.03 INCH (+0.76 mm). BORE A HOLE IN THE FITTING TO GET A 0.0003 TO 0.0018 INCH (0.008 TO 0.046 mm) INTERFERENCE FIT
THE REPLACEMENT BUSHING CAN HAVE AN OVERSIZE OD TO +0.03 INCH (+0.76 mm). BORE A HOLE IN THE FITTING TO GET A 0.0003 TO 0.0022 INCH (0.008 TO 0.056 mm) INTERFERENCE FIT
THE REPLACEMENT BUSHING CAN HAVE AN OVERSIZE OD TO +0.03 INCH (+0.76 mm). BORE A HOLE IN THE FITTING TO GET A 0.0002 TO 0.0013 INCH (0.005 TO 0.033 mm) INTERFERENCE FIT
THE REPLACEMENT BUSHING CAN HAVE AN OVERSIZE OD TO +0.03 INCH (+0.76 mm). BORE A HOLE IN THE FITTING TO GET A 0.0003 TO 0.0016 INCH (0.008 TO 0.041 mm) INTERFERENCE FIT
THE REPLACEMENT BUSHING CAN HAVE AN OVERSIZE OD TO +0.03 INCH (+0.76 mm). BORE A HOLE IN THE FITTING TO GET A 0.0004 TO 0.0023 INCH (0.010 TO 0.058 mm) INTERFERENCE FIT
THE REPLACEMENT BUSHING CAN HAVE AN OVERSIZE OD TO +0.03 INCH (+0.76 mm). BORE A HOLE IN THE FITTING TO GET A 0.0007 TO 0.0020 INCH (0.018 TO 0.051 mm) INTERFERENCE FIT
THE REPLACEMENT BUSHING CAN HAVE AN OVERSIZE OD TO +0.03 INCH (+0.76 mm). BORE A HOLE IN THE FITTING TO GET A 0.0006 TO 0.0018 INCH (0.016 TO 0.046 mm) INTERFERENCE FIT
THE REPLACEMENT BUSHING CAN HAVE AN OVERSIZE OD TO +0.03 INCH (+0.76 mm). BORE A HOLE IN THE FITTING TO GET A 0.0003 TO 0.0020 INCH (0.008 TO 0.051 mm) INTERFERENCE FIT
FAIRINGS NO. 1 AND 8 ONLY
Outboard Movable Flap Track Fairing Wear Limits
Figure 601 (Sheet 6)
L58293
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27-51-31
ALL ú
ú 01 Page 607
ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
____SHOWN WITH THE DOORS IN
NOTE:
THE CLOSED POSITION.
Fairing No. 1 and 8 Doors Wear Limits
Figure 602 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-31
ALL ú ú 01 Page 608 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
BOLT
FLANGED BUSHING/BUSHING
19. FLANGED BUSHING/BOLT
BUSHING/BOLT
C-C
Fairing No. 1 and 8 Doors Wear Limits
Figure 602 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-31
ALL ú ú 01 Page 609 ú Oct 18/00
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)
1
FLANGED
ID
0.2500
0.2510
0.2545
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