newton-meters). 2) Without loosening, tighten the bolts again until the torque is kept.

 (f)  
Lubricate the threads of the bolts that attach the right TVCA duct to the TVCA valve.

 (g)  
Install the right TVCA duct to the TVCA valve with the bolts. 1) Tighten the bolts to 85-95 pound-inches (9.6-10.7 newton-meters).

 2)  Without loosening, tighten the bolts again until the torque is kept.

 (h)  
Lubricate the threads of the bolt that attaches the link rod end to the bracket.

 (i)  
Install the link rod end to the bracket with the bolt and the nut. 1) Tighten the bolt to 36-40 pound-inches (4.1-4.5

 newton-meters).

 (j)  
Lubricate the threads of the adapter for the air signal tube with antigalling compound.

 (k)  
Connect the air signal tube to the adapter. 1) Hold the adapter and tighten the tube nut to 200-225 pound-inches (22.6-25.4 newton-meters).

 2)  Safety the tube nut with lockwire or safety cable and safety cable ferrule.
 G.  Return the Aircraft to Its Usual Condition
 S 414-022-N00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (1)  
Close the right thrust reverser (AMM 78-31-00/201).

 (2)  
Close the right core cowl panel (AMM 71-11-06/201).

 (3)  
Close the right fan cowl panel (AMM 71-11-04/201).

 S 414-023-N00
 S 414-024-N00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITH PHASE 3 CHANGES ú

 75-24-16
 ú ú N01 Page 406 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(4)  S 444-025-N00Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
 (5)  S 714-026-N00Do the test of the turbine vane cooling air valve that is shown in the Power Plant Test Reference Table (AMM 71-00-00/501).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ENGINES WITH PHASE 3 CHANGES ú

 75-24-16
 ú ú N01 Page 407 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
TURBINE VANE COOLING AIR VALVE AND TURBINE VANE AND BLADE COOLING AIR
_____________________________________________________________________
 VALVE 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 Turbine Vane and Blade Cooling Air Valve Solenoid
 Removal/Installation (AMM 75-33-03/401).

 B.  This procedure gives the instructions for the removal and the
 installation of the solenoid for the Turbine Vane Cooling Air (TVCA)
 valve and the Turbine Vane and Blade Cooling Air (TVBCA) valve. The
 solenoid for the TVCA valve and the TVBCA valve 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 10 o'clock position.
 D.  You can get access to the solenoid through the left thrust reverser.
 TASK 75-24-17-004-001-N00
 2.  Remove the Turbine Vane Cooling Air Valve and Turbine Vane and Blade Cooling____________________________________________________________________________ Air Valve 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 Zones
 412 Engine 1 - Intermediate Case Aft Face 10 o'clock
 422 Engine 2 - Intermediate Case Aft Face 10 o'clock
 431 Engine 3 - Intermediate Case Aft Face 10 o'clock
 442 Engine 4 - Intermediate Case Aft Face 10 o'clock

 (2)  
　
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