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R R  (14) Connect the rod (78) to the pedal (74) with the bolt (79) (Ref. Detail G). 
R  (15) Install the washer (75), the nut (76) and the new cotter pin (77). 
R R  (16) Connect the rod (80) to the pedal (85) with the bolt (81) (Ref. Detail H). 
R  (17) Install the washer (84), the nut (83) and the new cotter pin (82).
 Subtask 27-21-42-710-052
 B. Test
 (1) Preparation for the Test
 (a) Install the pedal position adjuster assembly (Ref. TASK 27-21-43-400-002).
 (b) Install the brake pedal transmitter unit (9GG) (Ref. TASK 32-42-47-400-001).
 (c) Install the brake control master cylinders (2625GM and 2626GM) (Ref. TASK 32-43-12-400-001).
 (2) Do the operational test of the F/O pedals (Ref. TASK 27-24-00-710-001).
 5. Close-up________
 Subtask 27-21-42-860-055
 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).

 

 ADJUSTER ASSY - PEDAL POSITION - SERVICING
__________________________________________
 TASK 27-21-43-600-001
 Lubrication of the Rack/Slider Linkage of the Pedal Position Adjuster
 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

__________________
 Refer to the MPD TASK: 272100-08

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific warning notice(s)
 No specific access platform 2.06 m (6 ft. 9 in.)

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
R  Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
29-10-00-864-003 Depressurize the Blue Hydraulic System
 27-21-43-991-006 Fig. 301

 

 3. Job Set-up
__________
 Subtask 27-21-43-860-057

 A. Aircraft Maintenance Configuration
 (1)
 Depressurize the Blue hydraulic system
 (Ref. TASK 29-10-00-864-003).

 (2)
 Put the warning notice(s) on the CAPT and F/O pedals to tell persons not to use the rudder.

 Subtask 27-21-43-010-054
 B. Get Access R (1) Put the access platform in position at the access door 811.
 (2) Open the access door 811.
 4. Procedure
_________
 (Ref. Fig. 301/TASK 27-21-43-991-006)
 Subtask 27-21-43-640-052
 A. Lubrication
 NOTE : Do these steps on the CAPT and F/O pedals.

____
 (1)
 Apply COMMON GREASE (Material No. 04-004) to the junction (3) of the rack (2) and slider (1).

 (2)
 In the cockpit, operate the pedal position adjuster fully many times so that the grease goes into the mechanism.

 (3)
 Apply a second coat of COMMON GREASE (Material No. 04-004) to the junction (3) of the rack (2) and slider (1).

 

 Rack/Slider Linkage of the Pedal Position Adjuster
 Figure 301/TASK 27-21-43-991-006
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 5. Close-up
________ Subtask 27-21-43-860-056
 A. Aircraft Maintenance Configuration
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Remove the access platform(s). Subtask 27-21-43-410-054
 B. Close Access
 (1)
 Close the access door 811.

 (2)
 Remove the warning notice(s).

 

 ADJUSTER ASSY - PEDAL POSITION - REMOVAL/INSTALLATION
　
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