BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F. Install the Isolation Valve for the Thrust Reverser (Fig. 401)
 S 864-018-N00
 (1)
Make sure you release the pressure from the main hydraulic system.

 S 864-019-N00

 (2)  
Make sure the DO-NOT-CLOSE tags are on the thrust levers.

 S 864-020-N00

 (3)  
Make sure the isolation valve has the pressure switch and solenoid valve installed.

 S 434-021-N00

 (4)  
Install the reducer (9) and gasket (10) on the hydraulic port of the isolation valve with the mark "RETURN OUT".

 S 434-022-N00

 (5)  
Install the restrictor (11) and gasket (10) on the hydraulic port of the isolation valve with the mark "CONTROL IN".

 S 434-023-N00

 (6)  
Install the unions (7) and packings (8) on the hydraulic ports of the isolation valve with the marks, "PRESSURE IN" and "RETURN OUT".

 S 434-024-N00

 (7)  
If it is necessary, install the jumper wire (6) with the steps that follow:

 (a)  
Remove the screw (12) from the valve solenoid.

 (b)  
Install the jumper wire (6) between the two washers (3 and 4) on the valve solenoid with the screw (12).

 S 424-026-N00
 (8)  Install the isolation valve (1) with the steps that follow:
 (a)  
Align the isolation valve (1) on the bracket.

 (b)  
Install the two mounting bolts (2), washers (4), and nuts (5).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-34-05
 ALL  ú ú N01 Page 407 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(c)  Install the bolt (2), two washers (3 and 4), jumper wire (6), and nut (5), from the isolation valve (1).
 NOTE: The jumper wire (6) is installed between the washers (3
____
 and 4).

 S 764-027-N00
 (9)  
Make sure the maximum resistance across the bond of the mounting bolt and jumper wires with the structure is 0.0025 ohms.

 S 434-038-N00

 (10)
 Remove the protection caps from the hydraulic lines (13).

 S 434-028-N00

 (11)
 Connect the hydraulic lines (13) to the isolation valve (1).

 S 434-039-N00

 (12)
 Remove the protection caps from the electrical connectors (12).

 S 434-040-N00

 (13)
 Connect the electrical connectors (12).

 S 614-041-N00
 CAUTION: BE PREPARED TO CATCH THE HYDRAULIC FLUID IN THE APPLICABLE
_______ CONTAINERS. IF THE HYDRAULIC FLUID FALLS INTO THE ENGINE, QUICKLY CLEAN THE ENGINE. IF YOU DO NOT QUICKLY CLEAN THE HYDRAULIC FLUID, THE HYDRAULIC FLUID CAN CAUSE DAMAGE TO THE ENGINE.
 (14)
 Fill the applicable hydraulic system reservoir with the hydraulic fluid (Ref 12-12-01/301).

 S 864-031-N00

 (15)
 Remove the DO-NOT-CLOSE tags and close these circuit breakers.

 (a)  P6 Main Power Distribution Panel
 1) 6F12 T/R IND ENG 1
 2) 6E12 T/R IND ENG 2
 3) 6D12 T/R IND ENG 3
 4) 6C12 T/R IND ENG 4
 5) 6F13 T/R CONT ENG 1
 6) 6E13 T/R CONT ENG 2
 7) 6D13 T/R CONT ENG 3
 8) 6C13 T/R CONT ENG 4

 (16)
 Supply the pressure to the main hydraulic system (Ref 29-11-00/201).

 S 864-032-N00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 78-34-05
 ALL  ú ú N01 Page 408 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 864-033-N00
 (17)
 Remove the DO-NOT-OPERATE tags from the thrust levers.

 S 714-034-N00

 (18)
 Do an operational test of the thrust reverser (Ref 78-31-00/501).

 S 794-035-N00

 (19)
 Look for hydraulic leaks.

 S 414-036-N00

 (20)
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 EXHAUST 2(78)