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
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REFERENCE DESIGNATION
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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
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REFERENCE DESIGNATION
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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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