_______
 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).

 1EFF : ALL 1 32-12-00Page 411 1 1 Nov 01/03 1 1 1CES 1

 Attaching Parts for the Secondary Hinged Fairing - Removal/Installation Figure 404/TASK 32-12-00-991-010
 1EFF : ALL 1 32-12-00Page 412 1 1 Nov 01/00R 1 1 1CES 1

R R  (3) Remove and retain all the nuts and bolts that attach the secondary hinged fairing from the MLG. 
R  (4) Remove the secondary hinged fairing attachment (Ref. TASK 57-26-21-000-001). 
R R  (5) Remove and retain all the nuts and bolts that attach the secondary hinged fairing attachment from the MLG.
 (6) Identify the position of the hinged fairing mounting plate (66) before you remove it.
 (7) Remove and discard the cotter pin (69) from the nut (68).
 (8) Remove and retain the nut (68) and the washer (70).
 (9) Remove and retain the nuts (73), the bolts (67), the hinged fairing mounting plate (66), the shim (71) and the packer (72).
 (10) Remove and retain the bolt (83), the washer (82), the bonding strap (84) and the nut (75) from the transfer block (80).
 (11) Remove and retain the bolt (79), the washer (78), the pin (77), the spacer (76) and the threaded insert (81) from the transfer block (80).
 (12) Remove and retain the actuating rod (74) from the transfer block (80).
 (13) Install the MLG fixed fairing assembly (Ref. TASK 32-12-14-400-001).
 Subtask 32-12-00-865-058 
R  F. 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 32-12-00-860-057
 A. Aircraft Maintenance Configuration 
R  (1) Close the access door 824. 
R  (2) Put the aircraft back to ground configuration (Ref. TASK 32-00-00-860-002).

 1EFF : ALL 1 32-12-00Page 413 1 1 Nov 01/03 1 1 1CES 1

R (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 Subtask 32-12-00-942-057
 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 414 1 1 Nov 01/03 1 1 1CES 1 TASK 32-12-00-040-005

 Preparation of the Aircraft for Flight with One MLG Fixed Fairing Assembly Removed or One Secondary Hinged Fairing Removed
 1. Reason for the Job
__________________
 Refer to the CDL TASK: 52-12 MAIN LANDING GEAR DOORS (732, 733, 742, R 743) (Flight with gear up) CDL TASK: 52-12
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific safety barriers
 No specific warning notice
 No specific access platform 3 m (9 ft. 10 in.)
 No specific Torque Wrench : range 0.20 to 3.60 m.daN

 (2.00 to 26.00 lbf.ft) 460005833 1 GROUND LOCK SLEEVE
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (Ref. 20-31-00)

 Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
6 cotter pin 32-11-11 80 -090 6 cotter pin 32-11-11 80C-090 6 cotter pin 32-11-11 80D-090
 1EFF : ALL 1 32-12-00Page 415 1 1 May 01/05 1 1 1CES 1 D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
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