(3)
 On the panel 110VU, make sure that the free fall control handle is folded into the center console.

 (4)
 Install shim(s) on each side of the free fall control handle to lock the handle in position. (Ref. Fig. 401/TASK 32-33-15-991-002)

 Subtask 32-33-15-010-050
 B. Get Access
 (1)
 Open the NLG doors (Ref. TASK 32-22-00-010-001).

 (2)
 Open the lateral avionics-compartment door 822.

 (3)
 Remove the cockpit floor panel 211FF (Ref. TASK 53-12-11-000-001).

 (4)
 Put the access platform in position in zone 123.

 (5)
 Put the access platform in position below the lateral
 avionics-compartment door 822.

 Subtask 32-33-15-480-050
 C. Installation of the Rigging Pins
 (Ref. Fig. 402/TASK 32-33-15-991-001)

 (1)
 In the nose landing gear well, put the tool PIN, RIGGING - RUDDER CONTROL (98A27901002000) (9) in the bottom bellcrank (10).

 (2)
 Put the RIGGING PIN (98A27801001000) (1) in position to lock the quadrant (2).

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 Free Fall Control Handle
 Figure 401/TASK 32-33-15-991-002
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 Reduction Gearbox - Component Location
 Figure 402/TASK 32-33-15-991-001
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 4. Procedure
_________
 (Ref. Fig. 402/TASK 32-33-15-991-001) Subtask 32-33-15-020-050
 A. Removal of the Free Fall Reduction Gearbox
 (1)
 Remove the cotter pin (15), the nut (14) and the washer (13).

 (2)
 Remove the screw (5) and disconnect the rod (8).

 (3)
 Cut and remove the lockwire from the screw (19). Remove the screw

 (19) and the washer (18).

 (4)
 Remove the cotter pin (20), the nut (21) and the washer (22).

 (5)
 Remove the cable guide (23) and the shims (24) and (17).

 (6)
 Remove the pins (12) from the cable tension adjusters (11).

 (7)
 To do this, turn the cable tension adjusters (11). Decrease the tension to release the cable reels (29) and (31).

 (8)
 Remove the cables (29) and (31) from the gearbox (3). Attach the cables to the structure.

 (9)
 Remove the nuts (16) and the bolts (4).

 (10) Remove the free fall gearbox (3) from its support and remove the screw (30).
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 Installation of the Reduction Gearbox
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific shim(s)
 No specific warning notice(s)
 No specific access platform 1.7 m (5 ft. 7 in.)

R No specific  Torque Wrench : range 0.00 to 1.20 m.daN
R  (0.00 to 9.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
No specific  lockwire corrosion resistant steel dia. 0.8 mm
 (0.0314 in.)

 Material No. 04-004  USA MIL-PRF-23827 TYPE I
 SYNTH.ESTER BASED GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 Material No. 04-022  USA MIL-PRF-81322 GRADE 2
 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 Material No. 11-002  USA MIL-PRF-680
 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT)
 (Ref. 20-31-00)

 1EFF : ALL 1 32-33-15Page 406 1 1 May 01/05 1 1 1CES 1 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-00-00-481-001 Installation of the Safety Devices on the Landing
 Gears
 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening
　
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