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时间:2011-04-16 10:04来源:蓝天飞行翻译 作者:航空
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 72-33-02
 ALL  ú ú N01 Page 609 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
~............................................................................... | TABLE 602 | | INSPECTION OF THE FAN EXIT VANES | ................................................................................. | Examine | Damage Limits | Necessary Procedure (AMM 72-33-02/801) | .................................................................................
 |  Vanes  |  3 vanes maximum  |  Install a replacement vane during the|
 |  that are  |  |  subsequent removal of the engine.  |
 |  missing  |  |  |
 |  |  4-5 vanes can be  |  Immediately remove broken pieces.  |
 |  |  missing if no more  |  Install replacement vanes in less  |
 |  |  than 3 are adjacent  |  than 50 hours.  If there are more  |
 |  |  and there is not less |  vanes missing than the limit, install|
 |  |  than 5 vanes between  |  replacement vanes immediately.  |
 |  |  each area of vanes  |  |
 |  |  that are missing  |  |

 2.............…........................…........................................1
 S 216-024-N00
 (4) Visually compare the damage you find on the vane platforms with the
 limits in Table 603 (Fig. 603). ~............................................................................... | TABLE 603 | | INSPECTION OF THE VANE PLATFORMS | ................................................................................. | Examine | Damage Limits | Necessary Procedure (AMM 72-33-02/801) | ................................................................................. | Cracks in | The base section on | No procedure is necessary. | | the inner | one side of a crack | | | diameter or | in Area A makes a | | | outer | continuous surface | | | diameter | with the section on | | | vane bases | the other side of the | | | | crack. | | | | | |
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 72-33-02
 ALL  ú ú N01 Page 610 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
SEE  A  CASE INTERMEDIATE 
(12.70 mm) AREA A 0.500 INCH  AXIAL LENGTH OUTER DIAMETER  FAN EXIT INNER CASE  VANE FAN EXIT BSEE
EDGE TRAILING 

RADIAL LENGTH
AREA B  AREA D 
AREA C 
LEADING 
EDGE 
AREA A 
INNER DIAMETER 
0.500 INCH  B 
(12.70 mm) 
L-A0965(0593) 
Fan Exit and Vane Inspection 
Figure 602 

D20329
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 72-33-02
 ALL  ú ú N01 Page 611 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE B
OUTER BASE
SEE A
AA
DIMENSION 0.75 INCH (19.050 mm) INITIAL  (EXAMPLE) CRACK  A 
B  B 
MOLD  BASE INNER 
VANE  AREA A 
VANE AND BASE ASSEMBLY 
ON THE OTHER SIDE OF THE BASE STRUCTURAL SECTION  B 
A-A  1 
DIMENSION INITIAL 1.380 INCH (35.052 mm)  B-B  1 

B-B 2
A-A 2
1  ENGINES WITHOUT PW SB 72-262
2  ENGINES WITH PW SB 72-262  L-A7587 
Fan Exit Vane Base Inspection Figure 603 

D20340
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