(0.40 to 2.60 m.daN) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 06-006 USA DOD-L-25681
ANTI-SEIZE COMPOUND (Ref. 20-31-00)
Material No. 19-018 USA AMS 5687
LOCKWIRE 0.6 MM (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R R R 13 13 20 20 21 21 union union packing packing packing packing 36-11-54 01B-030 36-11-54 01C-03036-11-54 01B-020 36-11-54 01C-02036-11-54 01B-020 36-11-54 01C-020
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-21-12-911-001 24-41-00-861-002 24-41-00-862-002 36-11-00-710-001 36-11-54-720-001 71-13-00-010-040 71-13-00-410-040 78-30-00-081-041 78-30-00-481-041 78-36-00-010-040 78-36-00-410-040 Tightening Torques for Pipes Unions (not for OXYGEN unions)Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerOperational Test to read the CURRENT STATUS of the Engine Bleed Air SystemFunctional Test of the Opening of the Fan Air ValveOpening of the Fan Cowl DoorsClosing of the Fan Cowl DoorsMake the Thrust Reverser Serviceable after MaintenanceMake the Thrust Reverser Unserviceable for MaintenanceOpening of the Thrust Reverser DoorsClosing of the Thrust Reverser Doors
**ON A/C 001-003, 051-054,
36-11-54-991-001 Fig. 401
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
36-11-54-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 36-11-54-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
(2)
Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3)
On the AIR COND panel 30VU:
-
Make sure that the ENG 1(2) BLEED pushbutton switch is released (the OFF legend is on).
-
Make sure that the APU BLEED pushbutton switch is released (the ON legend is off).
-
Make sure that the warning notice to tell persons not to operate the pneumatic system is in position.
(4)
On the ENG panel 115VU:
-Make sure that the warning notice to tell persons not to start the engine 1(2) is in position.
(5)
On the HP ground connector:
-Make sure that the warning notice to tell persons not to pressurize the pneumatic system is in position.
(6)
On the ENG section of the maintenance panel 50VU:
-
Make sure that the ON legend of the ENG/FADEC GND PWR 1(2) pushbutton switch is off.
-
Make sure that the warning notice to tell persons not to energize the FADEC 1(2) is in position.
(7)
Make sure that the access platform is in position below the engine.
1EFF : ALL 1 36-11-54Page 413 1 1 May 01/01R 1 1 1CES 1
Subtask 36-11-54-010-054
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 36-11-54-040-052
C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00-481-041).
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