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时间:2011-04-10 10:19来源:蓝天飞行翻译 作者:航空
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TRACK NO. 2 AND 7
4.38 |0.03 INCHES  D
(111.3 |0.8 mm)
0.06 INCH
(1.5 mm) MAXIMUM
AFT ROLLER SUPPORT
E-E
Outboard Aftflap Drive Mechanism Installation Figure 401 (Sheet 4)
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 27-51-40
 ALL  ú ú 01 Page 406 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

CARRIAGE48. WASHER
H  58. NUT
51. WASHERS
56. LUBE
54.
 NUT

55.
 WASHER


53. BUSHING
0.002 INCH 0.002 INCH
(0.05 mm) MINIMUM MINIMUMCLEARANCE CLEARANCE
35. GENEVA
SUPPORT
F-F
PIN BOLT
SPECIAL NUT
34. UPSTOP
NUT
WASHER 59. BOLT
BOLT/WASHER
60.
 WASHER

61.
 LUBE

62.
 ROLLER

63.
 SPACER


G-G H-H

1
WASHERS (57) ARE THINNER THAN WASHERS (51).
MOVE WASHERS AS IT IS NECESSARY TO GET
THE CLEARANCE

CARRIAGE
AFT BOGIE

66. WASHER
65.
64.
60.
49.
 WASHER

50.
 BOLT


UPSTOP
SUPPORT
FITTING

52. BOLT
35. GENEVA CAM
1. PUSHROD
69. WASHER
34.
1
H  57. WASHERS
PUSHROD
34.
 UPSTOP

35.
 GENEVA CAM HOOK


SUPPORT
(RELEASED (RELEASED 51. WASHERFITTNGFITTINGPOSITION) POSITION)
E
(0.05 mm) CAM 67. BOLT
SUPPORT
FITTING

68. WASHER
72. BUSHING FITTING
70.
 WASHER

71.
 NUT


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-40
Outboard Aftflap Drive Mechanism Installation
Figure 401 (Sheet 5)

ALL  ú ú 01 Page 407 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

COTTER PIN
FILL CAVITY
WITH GREASE

88. WASHER
(4 LOCATIONS) (2 LOCATIONS)


F

3
INSTALL A SUFFICIENT NUMBER OF WASHERS
TO GET THE NECESSARY TORQUE


Outboard Aftflap Drive Mechanism Installation
Figure 401 (Sheet 6)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


OUTBOARD FITTING
OUTBOARD FLAP INBOARD FITTING


0.000-0.007 INCH 0.000-0.007 INCH (0.00-0.18 mm) (0.00-0.18 mm)

J-J  CRANK ATTACH FITTING  K-K  CRANK ATTACH 4. MIDFLAP 
FITTING 
0.000-0.007 INCH  0.000-0.007 INCH 
(0.00-0.18 mm)  (0.00-0.18 mm) 


L-L  CRANK ATTACH FITTING 4. MIDFLAP  M-M  CRANK ATTACH FITTING 4. MIDFLAP 
Outboard Aftflap Drive Mechanism Installation Figure 401 (Sheet 7) 

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 ALL  ú ú 01 Page 409 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (c)  Remove the washer (8) and the bushing (9) from the crank.
 S 034-008
 (7)  
Disconnect the actuator rod (3) from the midflap crank:

 (a)  
Remove the bolt (21), washer (16 and 20), and nut (17).

 (b)  
Remove the actuator rod from the crank.

 (c)  
Remove the washer (19) and the bushing (18) from the crank.


 S 934-009
 (8) Install a tag on the midflap crank with the track number.
 
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