-
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 -------------------------------------------------------------------------------
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)
 1EFF : ALL 1 27-21-42Page 416 1 1 Feb 01/05R 1 1 1CES 1

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
R  51 cotter pin 27-21-01 03A-161 61 cotter pin 32-42-01 04 -010 68 cotter pin 27-21-01 01 -010 68 cotter pin 27-21-01 01A-010 77 cotter pin 32-42-01 04 -010 82 cotter pin 32-42-01 04 -010 89 cotter pin 32-42-01 04 -010 94 cotter pin 27-21-01 01 -010 94 cotter pin 27-21-01 01A-010 108 nuts 27-21-01 06 -010
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
27-21-43-000-001 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 32-42-47-000-001 Removal of the Transmitter Unit - Brake Pedal (9GG) 32-42-47-400-001 Installation of the Transmitter Unit - Brake Pedal
 (9GG) 32-43-12-000-001 Removal of the Brake Control Master Cylinder (2625GM,2626GM) 32-43-12-400-001 Installation of the Brake Control Master Cylinder (2625GM,2626GM)
 3. Job Set-up
__________
 Subtask 27-21-42-860-054
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the pedal position adjuster assembly is removed (Ref. TASK 27-21-43-000-001).

 (2)
 Make sure that the brake control master cylinders (2625GM, 2626GM) are removed (Ref. TASK 32-43-12-000-001).

 (3) Make sure that the brake pedal transmitter unit (9GG) is removed
 (Ref. TASK 32-42-47-000-001).
 (4) 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_________ 
R  Subtask 27-21-42-420-051-A 
R  A. Installation of the F/O pedals 
R  (1) Apply COMMON GREASE (Material No. 04-004) on the attachment hardware. 
R  (2) Install the pedal assembly between the structure (107) through the 
R  avionics compartment. 
R  NOTE : Make sure that the rods (66), (67), (71) and (90) are____ 
R  correctly installed in their bellcranks (60), (88), (72) and 
R  (91). 
R  (3) Install the bushes (105), the bolts (106) and the new nuts (108). 
R  (4) Install the bolt (95), the washer (92), the nut (93) and the new 
R  cotter pin (94) (Ref. Detail C). 
R  (5) Install the bolt (64), the washer (63), the nut (62) and the new 
R  cotter pin (61) (Ref. Detail D). 
R  (6) Install the bolt (65), the washer (87), the nut (86) and the new 
R  cotter pin (89) (Ref. Detail D). 
R  (7) Install the bolt (73), the washer (70), the nut (69) and the new 
R  cotter pin (68) (Ref. Detail E). 
R  (8) Install the bolt (55), the washer (54), the bonding strip (53), the 
R  nut (52) and the new cotter pin (51) (Ref. Detail B). 
R  (9) Install the bolt (104) on the post (72) with the bush (103) and the 
R  pedal (74). 
R  (10) Install the washer (101) and the nut (100). 
R  (11) Install the bolt (113) on the post (91) with the bush (112) and the 
R  pedal (85). 
R  (12) Install the washer (110) and the nut (109).

R R  (13) Safety the nuts (100) and (109) with Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.). 
　
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