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时间:2011-04-16 10:02来源:蓝天飞行翻译 作者:航空
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2  AREA A  1 

EDGE LEADING  AREA A 2  TRAILING 1 EDGE  EDGE LEADING  AREA A 2  TRAILING 1 EDGE 

3  3 

A  1 
NOTE: INSPECTION IS NOT NECESSARY IN AREA A.____ 3. 2. 1. 6.300 INCHES (16.020 cm) 0.500 INCH (12.700 mm) 0.500 INCH (12.700 mm) ALL AROUND  2 1  A ENGINES POST-PHASE III ENGINES PRE-PHASE III  2  L-A0970 

1st-Stage Blade Fluorescent Penetrant Inspection Areas
Figure 608

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 72-31-02
 ALL  ú ú N01 Page 632 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
1ST-STAGE (FAN) BLADE - REPAIRS
_______________________________
 1.  General_______
 A. This procedure gives the data for the tasks that follow:
 (1)  
The repair of the 1st-stage fan blades.

 (2)  
The replacement of the platform rubber seals.

 (3)  
The repair of the leading edge contour of the 1st-stage fan blades.

 B.
You must go into the inlet cowl to get access to the 1st-stage fan blade.


 TASK 72-31-02-308-001-N00
 2.  Blend Repair of the 1st-Stage Fan Blade_______________________________________
 A. General
 (1)  
You will blend the edges and the surfaces of the 1st-stage fan blades to do the repair.

 (a)  
You can blend the blades with a file or an abrasive stone.

 (b)  
If you must remove a large quantity of material, you can blend with a power tool.


 WARNING:_______ALWAYS WEAR GLOVES WHEN YOU TOUCH THE FAN BLADES. THESE BLADES HAVE SHARP EDGES THAT CAN CAUSE INJURY TO YOUR HANDS.
 CAUTION: BE VERY CAREFUL WHEN YOU REPAIR THE DAMAGE IN THE INNER HALF OF
_______ THE BLADE. THE NICKS IN THE LEADING AND TRAILING EDGES BECOME MORE IMPORTANT AS THEY GET NEARER TO THE ROOT OF THE BLADE.
 IF YOU USE A POWER TOOL TO REPAIR THE BLADE, MAKE SURE THE BLADE IS NOT TOO HOT. TOO MUCH HEAT CAN CAUSE THE BLADE TO BECOME WEAK AND CAUSE A FRACTURE. IF THE BLADE IS TOO HOT TO TOUCH WITH YOUR BARE HAND, LET THE SURFACE BECOME COOL BEFORE YOU CONTINUE.
 (2) Obey these procedures when you repair the 1st-stage fan blade:
 NOTE: Always use a sharp tool or a clean abrasive cloth to
____ prevent too much heat. Examine the tools frequently and replace them when it is necessary.
 For the location of the blade areas, refer to the procedure (AMM 72-31-02/601).
 (a) All the repairs on the blade surface must be smooth.
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 ALL  ú ú N01 Page 801 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////

D-D
L-A8005
1st-Stage (Fan) Blade Leading and Trailing Edge Minimum Thickness Limits Figure 801 (Sheet 1)
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 72-31-02
 ALL  ú ú N01 Page 802 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.


0.032 INCH
(0.813 mm)
0.025 INCH
(0.635 mm)

E-E
0.086 INCH
(2.184 mm)
0.041 INCH
(1.041 mm)

F-F

0.040 INCH
(1.016 mm)
0.031 INCH
(0.787 mm)
G-G
0.020 INCH
(0.508 mm) FOR THE FULL
LENGTH OF THE BLADE
7.812-8.062 INCHES
(198.4-204.8 mm) 0.040 INCH

(1.016 mm)
(P/N 53A321, 56A511 AND 56A821) H-H

B
L-A8007
1st-Stage (Fan) Blade Leading and Trailing Edge Minimum Thickness Limits Figure 801 (Sheet 2)
A80001
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