(b) Connect the drain tubes to the shrouds. TORQUE to between 135 and 150 lbf.in (1.52 and 1.69 m.daN).

 (c) Wirelock the head-end and rod-end knurled connection nuts with lockwire 0.032 in. (0.8mm) dia. (Material No. CP8001) or lockwire

 0.032 in. (0.8mm) dia. (Material No. CP8002).
 (3) Do a leak check of the head-end and rod-end drain shrouds as follows:
 (a) Remove the blanking cap from the drain tube tap. NOTE : The drain tube tap is the first tap aft of the 6 o'clock

____ tube bundle junction box.

 (b) Connect a source of dry, regulated air, nitrogen or argon to the tap.

 (c) Apply between 20 psi (1.40 bar) and 25 psi (1.70 bar) to the drain tube.

 (d) Stop the supply of dry, regulated air, nitrogen or argon.

 (e) Monitor the pressure. The pressure cannot decrease more than 10 psi (0.70 bar) in 2 minutes.

R (f) If the pressure decreases more than the limit, apply leak-tek R 160X (Material No. CP2170) to all of the couplings on the drain manifold. Then, make sure there are no leaks.
 (g) If you find leakage, make sure the coupling nuts are tightened to the correct torque. Or, tighten the knurled nut connections by hand until the leaks stop.

 (h) If the leakage continues, remove and replace the O-rings in the area of the leak.

 (i) Do the leak check again if you replaced an O-ring.

 (j) Remove the source of dry, regulated air, nitrogen or argon.

 (k) Install the blanking cap on the drain tube tap aft of the 6 o'clock tube bundle. TORQUE the blanking cap to between 135 and 150 lbf.in (1.52 and 1.69 m.daN).

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 Subtask 75-32-10-410-054

 C. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Close thrust reverser cowl doors : (Ref. TASK 78-36-00-410-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR

 (3) Remove the access platform(s).

 (4) Remove the warning notice(s).

 Subtask 75-32-10-440-052
 D. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).
 Subtask 75-32-10-860-052
 E. On the overhead panel 20VU, push the ENG1(2) FIRE pushbutton switch.
 Lower the guard on the pushbutton switch. R
 Subtask 75-32-10-710-051
 F. Test requirements
 (1) Do a FADEC ground test (engine motoring)

 (2) Do a minimum idle leak check (Ref. TASK 71-00-00-710-006) and make sure that on the CFDS no fault is shown related to the VSV system.

 5. Close-up
________
 Subtask 75-32-10-410-055
 A. Close fan cowl doors : (Ref. TASK 71-13-00-410-040)
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR

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R Subtask 75-32-10-865-056

R B. Remove the safety clip(s) and the tag(s) and close this(these) circuit R breaker(s):
R -------------------------------------------------------------------------------R PANEL DESIGNATION IDENT. LOCATION R -------------------------------------------------------------------------------R 49VU FUEL/LP VALVE/MOT1/ENG2 2QG A09 R 49VU FUEL/LP VALVE/MOT1/ENG1 1QG A08
R Subtask 75-32-10-862-051
R C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-R 002).
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__________________________________________________________________
 TASK 75-32-10-210-002
 Inspection of the Variable Stator Vane Actuator
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific warning notice
 No specific access platform 1 m (3 ft. 3 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
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