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时间:2011-04-17 09:13来源:蓝天飞行翻译 作者:航空
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
TURBINE VANE AND BLADE COOLING AIR VALVE AND IDG AIR/OIL HEAT EXCHANGER VALVE
_____________________________________________________________________________
 OVERRIDE SOLENOID - REMOVAL/INSTALLATION

________________________________________
 1.  General_______
 A.  This procedure is for engines with the Phase 3 changes. For engines
 without the Phase 3 changes, do this procedure: HPC Secondary Flow
 Control Valve and IDG Air/Oil Heat Exchanger Valve Override Solenoid
 Removal/Installation (AMM 75-33-04/401).

 B.  This procedure gives the instructions for the removal and installation of the solenoid for the Turbine Vane and Blade Cooling Air (TVBCA) Valve and the IDG air/oil heat exchanger valve override. The solenoid for the Turbine Vane and Blade Cooling Air (TVBCA) Valve and the IDG air/oil heat exchanger valve override will be referred to as the solenoid for this procedure.
 C.  The solenoid is installed on the aft face of the intermediate case at the 1 o'clock position.
 D.  You can get access to the solenoid through the right thrust reverser.
 TASK 75-24-15-004-042-N00
 2.  Remove the Turbine Vane and Blade Cooling Air Valve and IDG Air/Oil Heat________________________________________________________________________ Exchanger Valve Override Solenoid (Fig. 401)_________________________________
 A.  References
 (1)  
AMM 71-11-04/201, Fan Cowl Panels

 (2)  
AMM 71-11-06/201, Core Cowl Panels

 (3)  
AMM 72-34-03/401, Fan Exit Liner Segment

 (4)  
AMM 78-31-00/201, Thrust Reverser System

 B.  
Access

 (1)  
Location Zone
 412 Engine 1 - Intermediate Case Aft Face 1 o'clock
 422 Engine 2 - Intermediate Case Aft Face 1 o'clock
 432 Engine 3 - Intermediate Case Aft Face 1 o'clock
 442 Engine 4 - Intermediate Case Aft Face 1 o'clock


 (2)  
Access Panel
 416 Right Thrust Reverser Half - Engine 1
 426 Right Thrust Reverser Half - Engine 2
 436 Right Thrust Reverser Half - Engine 3
 446 Right Thrust Reverser Half - Engine 4


 C.  
Prepare to Remove the Solenoid


 S 864-043-N00
 (1)  For the applicable engine, open this circuit breaker and install the DO-NOT-CLOSE tag:
 (a)  P6 Main Power Distribution Panel
 1) 6F15, ENG 1 PERF SOL PWR A
 2) 6F16, ENG 1 PERF SOL PWR B
 3) 6E15, ENG 2 PERF SOL PWR A
 4) 6E16, ENG 2 PERF SOL PWR B
 5) 6D15, ENG 3 PERF SOL PWR A
 6) 6D16, ENG 3 PERF SOL PWR B

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITH PHASE 3 CHANGES ú

 75-24-15
 ú ú N01 Page 401 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
SOLENOID FOR THE TURBINE VANE AND BLADE COOLING AIR VALVE AND IDG AIR/OIL HEAT EXCHANGER VALVE
SEE B
INTERMEDIATE CASE
SEE A FAN EXIT LINER SEGMENT
BOLT
(2 LOCATIONS) PRESSURE SWITCH TUBE
CAP
ADAPTER

IDG AIR/OIL FWD ADAPTER HEAT EXCHANGER
GASKET VALVE OVERRIDEGASKET PRESSURE SWITCH
OVERRIDE PRESSURE A
BOLT SWITCH FOR THE
EEC IDG AIR/OIL HEATELECTRICAL
LOOP EXCHANGER VALVE
CONNECTOR CLAMP BRACKET
SOLENOID
BOLT

HOUSINGS
GASKET
PLUG SOLENOID FOR THE TURBINEGASKET
VANE AND BLADE COOLINGSUPPLY AIR VALVE AND IDG AIR/OIL TUBE HEAT EXCHANGER VALVE
GASKET EEC ELECTRICAL
ADAPTER CONNECTOR

ADAPTER
AIR SIGNAL TUBE B
Solenoid for the Turbine Vane and Blade Cooling Air Valve and
IDG Air/Oil Heat Exchanger Valve - Installation
Figure 401

D20479
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITH PHASE 3 CHANGES ú

 75-24-15
 ú ú N01 Page 402 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
7) 6C15, ENG 4 PERF SOL PWR A
 
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