structure (32).
TASK 27-21-42-400-001 Installation of the CAPT Pedals WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
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
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
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C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
2 cotter pin 27-21-01 03A-161 6 cotter pin 27-21-01 01 -010 6 cotter pin 27-21-01 01A-010 16 cotter pin 27-21-01 01 -010 16 cotter pin 27-21-01 01A-010 25 cotter pin 32-42-01 04 -010 33 nuts 27-21-01 05 -010
R 33 nuts 27-21-01 05A-010 38 cotter pin 32-42-01 04 -010
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-21-43-000-002 Removal of the Pedal Position Adjuster Assembly 27-21-43-400-002 Installation of the Pedal Position Adjuster Assembly 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-21-42-991-001 Fig. 401 27-21-42-991-002 Fig. 402
3. Job Set-up
__________
Subtask 27-21-42-860-052
A. Aircraft Maintenance Configuration
(1)
Make sure that the pedal position adjuster assembly is removed (Ref. TASK 27-21-43-000-002).
(2)
On the pedals (CAPT and F/O) make sure that the warning notices are in position to tell persons not to operate them.
4. Procedure
_________
(Ref. Fig. 401/TASK 27-21-42-991-001, 402/TASK 27-21-42-991-002)
Subtask 27-21-42-420-052
A. Installation of the CAPT pedals
(1)
Apply COMMON GREASE (Material No. 04-004) on the attachment hardware.
(2)
Install the pedal assembly (29) between the structure (32) through the cockpit.
NOTE : Make sure that the rods (9), (12), (28) and (34) are correctly
____ installed in their bellcranks (10), (13), (41) and (35).
(3)
Install the bushes (30), the bolts (31) and the new nuts (33) (Ref. Detail F).
(4)
Install the bolt (40), the washer (27), the nut (26) and tighten it. Secure with the new cotter pin (25) (Ref. Detail E).
(5)
Install the bolt (39), the washer (36), the nut (37) and tighten it. Secure with the new cotter pin (38) (Ref. Detail E).
(6)
Install the bolt (17), the washer (14), the nut (15) and tighten it. Secure with the new cotter pin (16) (Ref. Detail D).
(7)
Install the bolt (11), the washer (8), the nut (7) and tighten it. Secure with the new cotter pin (6) (Ref. Detail C).
(8)
Install the bolt (1), the washer (3), the bonding strip (4), the nut
R (5) and tighten it. Secure with the new cotter pin (2) (Ref. Detail B).
(9) Install the pedal position adjuster assembly (Ref. TASK 27-21-43-400-002).
Subtask 27-21-42-710-050
B. Test
(1) Do the operational test of the CAPT pedals (Ref. TASK 27-24-00-710-001).
5. Close-up
________ Subtask 27-21-42-860-053
A. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the warning notice(s). Subtask 27-21-42-410-051
B. Close Access
(1)
Close the access door 811.
(2)
Remove the access platform(s).
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