(13)
 Apply SEALANTS (Material No. 09-016) to the heads of the bolts (8) and (10).

 1EFF : ALL 1 32-12-00Page 418 1 1 May 01/01R 1 1 1CES 1

 Bonding Straps to MLG Leg - Removal/Installation Figure 405/TASK 32-12-00-991-016
 1EFF : 1 1R 1CES  ALL  1 11 1 32-12-00 Page 419 Nov 01/00

 Subtask 32-12-00-020-066
 B. Removal of the Secondary Hinged Fairing and Attaching Parts
 (Ref. Fig. 406/TASK 32-12-00-991-017)

 CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
 CARBONFIBER REINFORCED PLASTIC.

 NOTE : With one secondary hinged fairing missing, the maximum speeds
____
 during flight must be not more than:

 -250 knots (MLG extended)
 -350 knots (MLG retracted).
 (1)
 Remove the MLG fixed fairing assembly (Ref. TASK 32-12-14-000-001).

 (2)
 Remove the secondary hinged fairing (Ref. TASK 32-12-13-000-001).

 (3)
 Remove and retain all attaching nuts and bolts for the secondary hinged fairing from the MLG.

 (4)
 Remove the secondary-hinged-fairing attachment (Ref. TASK 57-26-21-000-001).

 (5)
 Remove and retain all attaching nuts and bolts for the
 secondary-hinged-fairing attachment from the MLG.

 (6)
 Identify the position of the hinged fairing mounting plate (22) before you remove it.

 (7)
 Remove and discard the cotter pin (25) from the nut (24).

 (8)
 Remove and retain the nut (24) and the washer (26).

 (9)
 Remove and retain the nuts (21), the bolts (23), the hinged fairing mounting plate (22), the shim (27) and the packer (28).

 (10)
 Remove and retain the bolt (38), the washer (37), the bonding strap

 (39) and the nut (30) from the transfer block (35).

 (11)
 Remove and retain the bolt (33), the washer (32), the pin (31), the spacer (34) and the threaded insert (36) from the transfer block (35).

 (12)
 Remove and retain the actuating rod (29) from the transfer block (35).

 (13)
 Install the MLG fixed fairing assembly (Ref. TASK 32-12-14-400-001).

 1EFF : ALL 1 32-12-00Page 420 1 1 May 01/01R 1 1 1CES 1

 Attaching Parts for the Secondary Hinged Fairing - Removal/Installation Figure 406/TASK 32-12-00-991-017
 1EFF : ALL 1 32-12-00Page 421 1 1 Nov 01/00R 1 1 1CES 1

 Subtask 32-12-00-865-069
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 1GG, 2GG, 3GG, 4GG, 52GA, 1701GK, 1702GK, 3700GD, 3701GD.
 5. Close-up
________ Subtask 32-12-00-860-068
 A. Aircraft Maintenance Configuration
 (1)
 Put the aircraft back to ground configuration (Ref. TASK 32-00-00-860-002).

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 Subtask 32-12-00-942-063
 B. Removal of Equipment
 (1)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 (2)
 Remove the access platform(s).

 (3)
 Remove the warning notice(s).

 1EFF : ALL 1 32-12-00Page 422 1 1 May 01/01R 1 1 1CES 1

 TASK 32-12-00-040-006
 Preparation of the Aircraft for Flight with a Failed or Missing Ground Door Opening Cable
 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.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 32-12-01
 Main Gear Doors
 Ground Opening Cable

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  cable-tie
R  No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice No specific access platform 2 m (6 ft. 7 in.) 460005835 2 GROUND LOCK SLEEVE 98DNSA20208040 1 RIGGING PIN
　
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