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时间:2011-04-10 10:01来源:蓝天飞行翻译 作者:航空
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 B.  
References

 (1)  
27-51-05/401, Outboard Foreflap

 C.  
Access

 (1)  
Location Zone
 586 Outboard Flap Foreflap, LH
 686 Outboard Flap Foreflap, RH


 D.  
Procedure


 S 026-002
 (1)  
Remove the foreflap (Ref 27-51-05/401).

 S 226-003

 (2)
Examine the parts, which connect the foreflap, for worn areas:

 (a)  
Remove the parts.

 (b)  
Measure the parts.


 NOTE: Use a micrometer or a vernier caliper.
____
 (c)  
Compare the dimensions you measured, with the permitted dimensions shown in Fig. 601.

 (d)  
Replace the parts that are out of the tolerance.

 (e)  
Install the parts.

 (3)  
Install the foreflap (Ref 27-51-05/401).


 S 426-004
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 27-51-05
 ALL  ú ú 01 Page 601 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

747-400 
MAINTENANCE MANUAL 
FOREFLAP 
MIDFLAP 
FWD 
LEVER  CARRIAGE 
SEE  B  SEE  A 
CARRIAGE 
FOREFLAP 
SEQUENCE 
CARRIAGE 
FOREFLAP  A 
MIDFLAP TRACK 
FLAP  (4 LOCATIONS) 
TRACK 
MIDFLAP 


LEVER 

BOLT/NUT 


Outboard Foreflap Wear Limits 
Figure 601 (Sheet 1) 

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 27-51-05
 ALL  ú ú 01 Page 602 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

1. BEARING/BOLT  2. BEARING BOLT

FOREFLAP FITTING

FOREFLAP FITTING
SEQUENCE CARRIAGE
SEQUENCE
CARRIAGE

INBOARD FLAP TRACK OUTBOARD FLAP TRACK A-A
NO. 1 INDEX  PART NAME DIM. IDBEARING  INCHES MINIMUM MAXIMUM INCHES DESIGN LIMITS DIAMETER (cm) (cm) 0.50000.4995 (1.269) (1.270)  0.5045 PERMITTED DIMENSION INCHES WEAR WEAR LIMITS (cm) (1.281)  0.0050 MAXIMUM DIAMETER CLEARANCE INCHES (cm)  PART WORN REPLACE X  REPAIR INSTRPART WORN REPAIR 
ODBOLT  0.49950.4990 (1.267) (1.269)  0.4950 (1.257)  (0.013)  X 
2  ID OD BEARING BOLT  0.3745 0.3750 0.3740 0.3745 (0.951) (0.953) (0.950) (0.951)  0.3700 0.3795 (0.964) (0.940)  0.0050 (0.013)  X 

Outboard Foreflap Wear Limits
Figure 601 (Sheet 2)

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 27-51-05
 ALL  ú ú 01 Page 603 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


OLD CONFIGURATION  NEW CONFIGURATION
B-B
Outboard Foreflap Wear Limits
Figure 601 (Sheet 3)

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 27-51-05
 ALL  ú ú 01 Page 604 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
H40477
A
747-400
MAINTENANCE MANUAL

2 1 NO. INDEX  PART NAME DIM. OD IDBUSHING BUSHING  (cm)(cm) DIAMETER DESIGN LIMITS INCHES MAXIMUMMINIMUM INCHES 0.5605 0.5630 0.5595 0.5615 (1.424)(1.421) (1.430)(1.426)  (cm) WEAR LIMITS WEAR INCHES DIMENSION PERMITTED 0.555 0.568 (1.410) (1.443)  (cm) INCHES CLEARANCE DIAMETER MAXIMUM 0.007 (0.018)  REPLACE WORN PART  REPAIR WORN INSTR REPAIR PART X X 
 
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