(7)
Safety the nut (50) with a new cotter pin (51).
(8)
Apply SEALANTS (Material No. 09-016) to the head of the bolt (48) and the nut (50).
R WARNING : CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK.
_______ R LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
(9) Remove and discard the lockwire from the bolts (53) and (56).
(10)
Remove the bolt (56) and the washer (55) from the bracket (52).
(11)
Install the bonding strap (54), the washer (55) and the bolt (56) (Ref. TASK 20-28-00-912-004).
(12)
Safety the bolts (53) and (56) with MISCELLANEOUS (Material No. 19-010).
(13)
Apply SEALANTS (Material No. 09-016) to the heads of the bolts (53) and (56).
(14) Install the fixed fairing assembly (Ref. TASK 32-12-14-400-002). R Subtask 32-12-00-980-051 R F. Manual Operation R WARNING : CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE
_______ R LOCKWIRE CAN CUT OR BLIND YOU. R (1) In the avionics compartment on the panel 188VU:
R (a) Set the L/G DOWN VMO/MMO SELECTION switch 22FP to NORM.
R (b) Lock the safety cover and secure it with MISCELLANEOUS (Material
R No. 19-010).
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Subtask 32-12-00-865-065
R R G. 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 32-12-00-860-064
A. Aircraft Maintenance Configuration
R R (1) Close the access door 824.
R (2) Put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
R (3) Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
R (4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 32-12-00-942-060
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).
Restoration of the Aircraft after Flight with One Fixed Fairing 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)
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.)
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 25 cotter pin 57-26-05 36 -030
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D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 29-00-00-910-002 Safety Procedures of the Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System 32-00-00-481-001 Installation of the Safety Devices on the Landing
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