-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION
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No specific access platform 1.5 m (4 ft. 11 in.)
No specific access platform 2.8 m (9 ft. 2 in.)
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) 98A27901002000 2 PIN, RIGGING - RUDDER CONTROL 98D27207516000 1 RIGGING PIN SET 98D27207547000 1 PIN - RIGGING
B. Consumable Materials
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REFERENCE DESIGNATION
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No specific Lockwire corrosion resistant steel dia 0.6 mm (0.02 in.) No specific Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
17 cotter pin 27-21-01 12B-070 29 cotter pin 27-21-01 12B-070 35 cotter pins 27-21-01 12B-010 38 cotter pin 27-21-01 12B-010 40 cotter pin 27-21-01 01 -010 40 cotter pin 27-21-01 01A-010 50 cotter pins 27-21-01 12B-170
D. Referenced Information
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REFERENCE DESIGNATION
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24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power
27-21-00-820-002 Adjustment of the Rudder Control-Cables Length
29-10-00-864-001 Depressurize the Green Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-10-00-864-003 Depressurize the Blue Hydraulic System
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-45-991-001 Fig. 401
**ON A/C 301-399,
27-21-45-991-001-A Fig. 401A
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-45-991-002 Fig. 402
**ON A/C 301-399,
27-21-45-991-002-A Fig. 402A -------------------------------------------------------------------------------
REFERENCE DESIGNATION
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R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-45-991-003 Fig. 403
**ON A/C 301-399,
27-21-45-991-003-A Fig. 403A
**ON A/C ALL
3. Job Set-up
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Subtask 27-21-45-860-051
A. Aircraft Maintenance Configuration
(1) Make sure that the panel 211GF at zone 211 is removed. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-21-45-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 27-21-45-991-001-A)
**ON A/C ALL
(2)
Make sure that the access platform is in position at zone 121.
(3)
Make sure that the access door 811 is open.
(4)
Make sure that the access platform is in position at zone 312.
(5)
Make sure that the access door 312AR is open.
(6)
Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).
(7)
On the overhead panel 23VU, make sure that the FLT CTL/FAC1 pushbutton switch is pushed.
(8)
On the overhead panel 24VU, make sure that the FLT CTL/FAC2 pushbutton switch is pushed (on these pushbuttons switches, the OFF and FAULT legends are off).
(9)
On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator shows 0.
(10) In zone 121, on the CAPT yaw/brake bellcrank (5) make sure that the PIN, RIGGING - RUDDER CONTROL (98A27901002000) (6) (Ref. Detail C) is installed.
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