(0.40 to 2.60 m.daN)
No specific Torque Wrench : range 96.00 to 900.00 lbf.in
(1.00 to 10.00 m.daN)
856A1084 1 CART - STATOR ACTUATOR
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2170 *
leak-tek 160X (Ref. 70-30-00) R Material No. CP5070 * R vaseline (Ref. 70-30-00)
Material No. CP8001 *
lockwire 0.032 in. (0.8mm) dia. (Ref. 70-30-00)
Material No. CP8002 *
lockwire 0.032 in. (0.8mm) dia. (Ref. 70-30-00)
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C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
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120 O-ring 75-32-10 01 -130 140 O-rings 75-32-10 01 -020 150 O-rings 75-32-10 01 -010 190 O-ring 75-32-10 01 -130
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
R from the External Power 71-00-00-710-006 Minimum Idle Check 71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 78-30-00-081-041 Make the Thrust Reverser Serviceable after Maintenance 78-30-00-481-041 Make the Thrust Reverser Unserviceable for Maintenance 78-36-00-010-040 Opening of the Thrust Reverser Doors 78-36-00-410-040 Closing of the Thrust Reverser Doors 75-32-10-991-300 Fig. 401 75-32-10-991-301 Fig. 402 75-32-10-991-302 Fig. 403
3. Job Set-up
__________
Subtask 75-32-10-860-051
A. Aircraft Maintenance Configuration
(1) On the center pedestal, on the ENG panel 115VU, make sure that a warning notice is in position to tell persons not to start the engine.
(2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that a warning notice is in position to tell persons not to energize the FADEC 1(2).
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(3) On the overhead panel 20VU, make sure that the ENG1(2) FIRE pushbutton switch is released.
(4) Make sure that the access platform is in position.
Subtask 75-32-10-010-058
B. Get Access
(1) Make sure that the fan cowl doors are open: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
(2) Make sure that the thrust reverser doors are open: (Ref. TASK 78-36-00-010-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
Subtask 75-32-10-040-054
C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00-481-041).
4. Procedure
_________
(Ref. Fig. 401/TASK 75-32-10-991-300, 402/TASK 75-32-10-991-301, 403/TASK 75-32-10-991-302)
Subtask 75-32-10-420-051
A. Installation of the VSV actuator
(1) Clean the component interface and/or the adjacent area.
(2) Do a visual inspection of the component interface and/or the adjacent area.
(3) Install the nipples in the VSV actuator as follows:
(a) Remove all the blanking plugs from the head-end, rod-end and actuator drain ports.
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R (b) Lubricate the new O-ring (120) and O-ring (190) with vaseline (Material No. CP5070) and install them on the nipples (130), (200).
R R (c) Install the nipples (130) in the head-end and rod-end ports of the actuator. TORQUE the nipples (130) to between 135 and 150 lbf.in (1.52 and 1.69 m.daN).
(d) Install the nipple (200) in the drain port of the actuator located at the two o'clock position.
R R (e) Install the plug (210) in the drain port of the actuator located at the 8:00 o'clock position.
(f) TORQUE the nipple (200) and the plug (210) to between 135 and 150 lbf.in (1.52 and 1.69 m.daN).
(g) Wirelock the plug (210) with lockwire 0.032 in. (0.8mm) dia. (Material No. CP8001) or lockwire 0.032 in. (0.8mm) dia. (Material No. CP8002).
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