(3)
 Open the lateral avionics-compartment door 822.

 (4)
 Remove the cockpit floor panels 211FF, 211JF (Ref. TASK 53-12-11-000-001).

 (5) Remove the floor panel 221AF (Ref. TASK 53-12-12-000-001).
 Subtask 32-33-16-869-052

 C. Flight Configuration Precautions
 (1)
 If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002). Then, it is not necessary to operate the LGCIU circuit breakers.

 (2)
 If the electrical power is necessary, do the precautions for flight configuration (Ref. TASK 32-00-00-860-001) before you open the LGCIU circuit breakers.

 Subtask 32-33-16-865-050
 D. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------
PANEL DESIGNATION  IDENT. LOCATION
 -------------------------------------------------------------------------------
R  49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
 1EFF : ALL 1 32-33-16Page 404 1 1 Feb 01/99 1 1 1CES 1 Subtask 32-33-16-480-050

 E. Installation of the Rigging Pins
 (Ref. Fig. 402/TASK 32-33-16-991-001)

 (1)
 Put the RIGGING PIN (98A27801001000) in the Pin 1 position.

 (2)
 Put the PIN, RIGGING - RUDDER CONTROL (98A27901002000) in the Pin 4 position.

 4. Procedure
_________
 (Ref. Fig. 403/TASK 32-33-16-991-002) Subtask 32-33-16-020-050
 A. Removal of the NLG Free-Fall Extension Cables WARNING : MAKE SURE THAT THE NLG DOWNLOCK SAFETY PIN AND THE TWO DOOR
_______
 SAFETY PINS ARE INSTALLED.

 (1) Remove the applicable cable(s) (1) and/or (2) as follows:
 (a)
 Remove and discard the cotter pins (8).

 (b)
 Remove these items:

 -
the nuts (9) and the washers (7)

 -
the bolts (4) and the spacers (6)

 -
the cable-guard (5)

 (c)
 Remove the cable-guide locking-devices (11) and the fairleads (10).

 (d)
 Remove the locking clips (16) from the turnbuckles (17).

 (e)
 Loosen the turnbuckles (17) for the cables (1) and (2) until the tension in the cables is released.

 (f)
 On the cable(s) to be removed, continue to loosen the turnbuckle(s) (17) until the cable(s) is/are disconnected.

 (g)
 If necessary, temporarily attach the loose cable(s) (12) and/or

 (14) to the adjacent structure.

 (h)
 Release the cable(s) (1) and/or (2) from the cable pulley (3) and remove it/them from the aircraft.

 1EFF : ALL 1 32-33-16Page 405 1 1 Feb 01/98 1 1 1CES 1

R R  Location of the Rigging Pins Figure 402/TASK 32-33-16-991-001- 12 (SHEET 1)
 1EFF : 1 1 1CES  ALL  1 111 32-33-16 Page 406 Nov 01/00

R R  Location of the Rigging Pins Figure 402/TASK 32-33-16-991-001- 22 (SHEET 2)
 1EFF : 1 1 1CES  ALL  1 111 32-33-16 Page 407 Nov 01/00

 Free-fall Extension Cables - NLG Figure 403/TASK 32-33-16-991-002
 1EFF : 1 1R 1CES  ALL  1 11 1 32-33-16 Page 408 Nov 01/00

 (2) Remove the applicable cable(s) (12) and/or (14) as follows:
 (a)
 Remove these items:

 -
the cotter pin (21), the nut (22) and the washer (23)

 -
the bolts (13) and (20) and the washer (19)

 -
the spacers (18) and the cable-guard (25)

 (b)
 Remove the locking clips (16) from the turnbuckles (17).

 (c)
 Loosen the turnbuckles (17) for the cables (12) and (14) until the tension in the cables is released.

 (d)
 On the cable(s) to be removed, continue to loosen the
 turnbuckle(s) until the cable(s) is/are disconnected.

 (e)
 If necessary, temporarily attach the loose cable(s) (1) and/or

 (2) to the adjacent structure.

 (f)
 Release the cable(s) (12) and/or (14) from the cable quadrant

 (15) on the reduction gearbox and remove it/them from the aircraft.
 1EFF : ALL 1 32-33-16Page 409 1 1 Nov 01/00R 1 1 1CES 1

 TASK 32-33-16-400-001
 Installation of the NLG Free-Fall Extension Cables
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
　
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