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R  (c) TORQUE the borescope plug to between 57 and 63 lbf.in (0.64 and 0.71 m.daN). 
R R  (d) Wirelock the borescope plug. Use Safetywire 0.032 in.(0.8 mm) dia. (Material No. CP8001) or Safetywire 0.032 in.(0.8 mm) dia. (Material No. CP8002).
 (2) Install the stage 6, 7 and 8 borescope plugs (S6, S7 and S8) as follows:
 CAUTION : MAKE SURE YOU FULLY SCREW THE INNER CAP IN. IF NOT FULLY_______ SCREWED IN, THE INNER CAP OF THE BORESCOPE PLUG WILL DEFLECT THE COMPRESSOR REAR CASE AS THE OUTER CAP IS TIGHTENED. THIS WILL CAUSE BINDING OF THE COMPRESSOR ROTOR.
 (a) Make sure the borescope port is open. Insert 0.37 in. (9.40mm) diameter tapered Rod (locally purchased) in the borescope port. 
R R  (b) Apply graphite grease (Material No. CP2101) or Never seez-pure (Material No. CP2619) to the threads and pressure face of the borescope plug.
 (c) Put the plug in the correct borescope port and tighten the inner plug by hand. Use the outer plug to turn the inner plug.
 (d) Torque the inner plug to between 75 and 85 lbf.in (0.84 and 0.96 m.daN). Loosen half a turn and RETORQUE to between 15 and 20 lbf.in (0.16 and 0.22 m.daN).
 (e) Compress the plug spring and tighten the outer plug by hand.
R R R R  NOTE : If the inner plug is correctly installed and the threads____ are not damged, you can install the outer plug by hand. If the outer plug cannot be fully installed by hand , the inner plug is not correctly installed. Remove the plug and repeat steps (c), (d) and (e).
 (f) TORQUE the outer plug to between 57 and 63 lbf.in (0.64 and 0.71 m.daN).
 (g) Wirelock all 3 outer plugs together with Safetywire 0.032 in.(0.8 mm) dia. (Material No. CP8001) or Safetywire 0.032 in.(0.8 mm) dia. (Material No. CP8002).

 E E Feb 01/04 E E ECES E 5. Close-up

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________ Subtask 72-31-00-410-056
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

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

 Subtask 72-31-00-440-053
 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041). Subtask 72-31-00-410-059
 C. Close Access
 (1) Close the fan cowl doors (Ref. TASK 71-13-00-410-040):
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR.

 (2) Remove the access platform(s).

 (3) Remove the warning notice(s).

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 TASK 72-31-00-300-004
 Blend Repair of the High Pressure Compressor (HPC) Rotor Blades Stages 1-9
 1. Reason for the Job
__________________
 This TASK is the blend repair of the HPC rotor blades with a borescope blend tool.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
 No specific CCD video camera and monitor (Wolf Compatible)
 No specific HPC, blade, borescope, blending tool (Wolf tool

 5.08036.00)
 No specific access platform 1 m (3 ft. 3 in.) R No specific Torque Wrench : range 5.00 to 35.00 lbf.in R (0.05 to 0.40 m.daN)
 No specific Torque Wrench : range 36.00 to 220.00 lbf.in
 (0.40 to 2.60 m.daN)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2101 USA MIL-T-5544 graphite grease (Ref. 70-30-00) Material No. CP2619 * Never Seez-Pure Nickel, Special (Ref. 70-30-00) Material No. CP8001 * lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00) Material No. CP8002 * lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00)
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