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) 98A27103500000 1 FTU PROTECTION TOOL 98A27103500001 1 FTU PROTECTION TOOL 98A27901002000 1 PIN, RIGGING - RUDDER CONTROL 98D27207516000 1 RIGGING PIN SET 98D27207545000 1 PIN - RIGGING 98D27207546000 1 PIN - RIGGING 98D27207547000 1 PIN - RIGGING 98D27207548000 1 PIN - RIGGING
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
No specific  lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
 Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Expendable Parts -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ------------------------------------ |IPC-CSN----------------------------------
38  cotter pins  27-21-04 22 -470
 38  cotter pins  27-21-04 22 -470A
 D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002  Energize the Aircraft Electrical Circuits from the
 External Power
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 27-21-00-820-002  Adjustment of the Rudder Control-Cables Length
 27-21-00-840-001  Removal/Installation of the control rod on the rudder
 mechanical control
 27-22-00-820-001  Adjustment of the Rudder Trim Actuation
 27-24-00-710-001  Operational Test of the Rudder Hydraulic Actuation
 27-24-00-820-001  Adjustment of the Rudder Neutral Position
 27-26-00-820-001  Adjustment of the Yaw Damper Actuation
 29-10-00-863-003  Pressurize the Blue Hydraulic System with a Ground
 Power Supply
 29-10-00-864-003  Depressurize the Blue Hydraulic System
 29-23-00-863-001  Pressurize the Green Hydraulic System from the Yellow
 Hydraulic System through the PTU with the Electric
 Pump
 29-23-00-864-001  Depressurize the Green and Yellow Hydraulic Systems
 after Operation of the PTU
 29-24-00-863-001  Pressurize the Yellow Hydraulic System with the
 Electric Pump
 29-24-00-864-001  Depressurize the Yellow Hydraulic System
 53-12-11-000-001  Removal of the Cockpit Floor Panels from FR1 Thru
 FR12
 53-12-11-400-001  Installation of the Cockpit Floor Panels from FR1
 thru FR12
 27-21-61-000-001  Removal of the Rudder Control Cables (for corrective
 action)
 27-21-61-400-001  Installation of the Rudder Control Cables (for
 corrective action)

 1EFF : ALL 1 27-21-00Page 508 1 1 Aug 01/04R 1 1 1CES 1

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 27-21-00-991-004 Fig. 502
 **ON A/C 301-399,
 27-21-00-991-004-A Fig. 502A
 **ON A/C ALL
 27-21-00-991-005 Fig. 503
 27-21-00-991-012 Fig. 504
 27-21-00-991-003 Fig. 505

 3. Job Set-up
__________
 Subtask 27-21-00-860-052

 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 On the overhead panel 23VU, make sure that:

 -the FLT CTL/FAC1 and FLT CTL/ELAC1 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).

 (3)
 On the overhead panel 24VU, make sure that:

 -the FLT CTL/FAC2 and FLT CTL/ELAC2 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).

 (4)
 Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-10-00-863-003).

 (5)
 On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator is at 0.
　
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