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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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REAR SEGMENT OF
FRONT SEGMENT OF
THE INLET CONE
THE INLET CONE

L-A0035
Inlet Cone Installation
Figure 401 (Sheet 1)

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 72-31-01
 ALL  ú ú N01 Page 402 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

L-A3302 (0697)
Inlet Cone Installation Figure 401 (Sheet 2)
H08838
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 72-31-01
 ALL  ú ú N01 Page 403 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 024-014-N00
 (4)  
Remove the front segment of the inlet cone:

 (a)  
Remove six bolts and washers that hold the front segment of the inlet cone to the rear segment.

 (b)  
Remove the front segment.


 S 024-006-N00
 CAUTION: DO NOT LET THE INLET CONE FALL WHEN YOU RELEASE IT FROM THE
_______ COMPRESSOR HUB. THIS CAN CAUSE DAMAGE TO THE INLET CONE.
 CAUTION:_______DO NOT INSTALL THE PULLER INCORRECTLY. YOU CAN CAUSE DAMAGE TO THE NUT PLATES AND THE INLET CONE IF YOU DO NOT INSTALL THE PULLER CORRECTLY.
 (5)  
Remove the rear segment of the inlet cone:

 (a)  
Remove 19 bolts and washers that hold the rear segment to the front LPC hub.

 (b)  
Install the puller to the nut plates of the inlet cone on the inner side and remove the rear segment (Fig. 402).


 TASK 72-31-01-404-007-N00
 3. Inlet Cone Installation (Fig. 401)
_______________________
 A. Standard Tools and Equipment
 (1)  
Mat - Protective, Rubber Manufacturer's Association, Grade SC43, neoprene sponge, 1 inch thick, 5 x 6 feet with warning streamers attached (three required)

 B.
Consumable Materials

 (1)  
D00390 Oil - Engine

 C.
References

 (1)  
IPC 72-31-01 Fig. 5

 D.
Access

 (1)  
Location Zone
 412 Engine 1 - Front LPC Hub
 422 Engine 2 - Front LPC Hub
 432 Engine 3 - Front LPC Hub
 442 Engine 4 - Front LPC Hub

 

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 72-31-01
 ALL  ú ú N01 Page 404 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

Inlet Cone Puller Installation
Figure 402

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 72-31-01
 ALL  ú ú N01 Page 405 ú Feb 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
E. Procedure
 S 224-008-N00
 (1)  Refer to the table that follows for the clearance between the rear segment of the inlet cone and the hub of the low pressure compressor (LPC) and the clearance for the compressor blade lock (Fig. 401):
 NOTE: The clearances are only for reference.
____
 ~................................................................. | TABLE 401 | ................................................................... | | | NEW PART REFERENCE | CLEARANCE | | | | DIMENSIONS | LIMITS | | PART | | INCHES | INCHES | | NAME | DIA | (MM) | (MM) | | | ............................................... | | | MIN | MAX | MIN | MAX | ................................................................... | LPC HUB | OD | 27.378 | 27.382 | | | | | | (695.402) | (695.502) | 0.028L | 0.006T | ............................................. (0.71L) | (0.15T) | | INLET CONE | ID | 27.376 | 27.384 | *[1] | *[1] | | REAR SEGMENT| | (695.350) | (695.554) | | | ................................................................... | Compressor | OD | ------| ------| 0.010 | 0.060 | | Blade Lock | | | | (0.245) | (1.524) | 2.............….....…...........…...........…..........…..........1
 
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