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时间:2011-04-16 10:00来源:蓝天飞行翻译 作者:航空
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 423 and 424 Fan Cowl Panel - Engine 2
 433 and 434 Fan Cowl Panel - Engine 3
 443 and 444 Fan Cowl Panel - Engine 4
 417 and 418 Core Cowl Panel - Engine 1
 427 and 428 Core Cowl Panel - Engine 2
 437 and 438 Core Cowl Panel - Engine 3
 447 and 448 Core Cowl Panel - Engine 4


 D.
Do the Test of the Latches on the Pressure Relief Doors (Fig. 501).


 S 045-002-N00
 WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  Do this procedure: Thrust Reverser Deactivation for Ground Maintenance (AMM 78-31-00/201).
 NOTE: This is only necessary if you will use this procedure for the
____ pressure relief doors on the core cowl panels.
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 ALL  ú ú N01 Page 501 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////

FAN COWL PANEL
LATCH TOOL SLOT SEE

PRESSURE RELIEF DOOR FOR THE CORE COWL PANEL 
(4 LOCATIONS)
1  0.06 |0.03 INCH (1.5 |0.76 MM)  Cowl Panel Pressure Relief Doors B 
Figure 501 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
WASHER TO ADJUST 
UPPER/LOWER SIDE  TAPERED 
GAP  SPACER 
SHIM 
DOOR 
DOOR  NUT 
(2 LOCATIONS) 
SHIM TO ADJUST STEP-HEIGHT  (2 LOCATIONS) BOLT  PINS ROLL 
WASHER 
(2 LOCATIONS) 
WASHER 

|0.03 INCH 
(|0.76 MM)
BUSHING 
HINGE FITTING 
OUTSIDE 
COWL PANEL 
INSIDE 
HINGE ASSEMBLY CROSS SECTION 
HINGE ASSEMBLY  A-A 

COWL PANEL DOOR
INSIDE (REF)
3. BOLTS  WASHERS NUTS
LATCH 
2  SKIN GAP TOLERANCE INSTALL AS NECESSARY FOR  D 

Cowl Panel Pressure Relief Door Details
Figure 501 (Sheet 2)

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 ALL  ú ú N01 Page 503 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
5. PIVOT SUPPORT ASSEMBLY

B71044-10 LOAD TEST TOOL INSTALLATION
Cowl Panel Pressure Relief Door Latch Test Figure 501 (Sheet 3)
G83438
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 015-017-N00
 (2)  Open the latches on the pressure relief door.
 (a)  
Put the blade of a straight-slot screwdriver into the latch slot (1).

 (b)  
Move the screwdriver handle to the side to turn the latch (1) to the open position.


 S 485-018-N00
 (3)  Install the load-test-adapter-tool for the latch on the pressure relief door.
 (a)  
Remove the two latch mounting bolts (3) that are nearest to the edge of the pressure relief door.

 (b)  
Temporarily fasten the adapter assembly (2) to the door with the bolts (4) that are supplied with the adapter assembly. 1) Put the adapter bolts (4) into the bolt holes that the
 
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