(2)
On the panel 110VU, remove the wedges from each side of the GRAVITY GEAR EXTN handle.
(3) Close the MLG doors (Ref. TASK 32-12-00-410-001). Subtask 32-33-16-865-055
L. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 52GA.
Subtask 32-33-16-720-051
M. Test
(1) Do a functional test of the free-fall extension system (Ref. TASK 32-33-00-720-001).
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N. Test
(1) After replacement of the cables (37) and/or (38), do an operational test of the pressurization system (Ref. TASK 21-31-00-710-002). (Ref. Fig. 407/TASK 32-33-16-991-004)
5. Close-up
________
Subtask 32-33-16-869-055
A. Flight Configuration Precautions
(1) If you did not de-energize the aircraft electrical circuits, put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
R **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 32-33-16-410-053
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Do the applicable steps that follow:
(3)
Install the cockpit floor-panels 212GF, 212NF (Ref. TASK 53-12-11-400-001).
(4)
Install the cabin floor panels as necessary (Ref. TASK 53-12-12-400-001): 222CF, 222EF, 232DF.
(5)
Install the cabin floor panels as necessary (Ref. TASK 53-32-12-400-002):
-242BF, 241EF, 241FF, 242FF, 242GF, 241JF
-241KF, 242KF, 241LF, 242LF, 241MF, 242MF.
(6)
Install the forward cargo-compartment ceiling-panels 131AC, 131BC, 131CC.
(7)
Install the forward cargo-compartment rear-partition 132PW.
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(8)
Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
(9)
Close the lateral avionics-compartment doors 822 and 824 (Ref. TASK 52-41-00-410-002).
R **ON A/C 151-199, 401-499,
Subtask 32-33-16-410-053-A
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Do the applicable steps that follow:
(3)
Install the cockpit floor-panels 212GF, 212NF (Ref. TASK 53-12-11-400-001).
(4)
Install the cabin floor panels as necessary (Ref. TASK 53-12-12-400-001): 222CF, 222EF, 232DF.
(5)
Install the cabin floor panels as necessary (Ref. TASK 53-32-12-400-002):
-242BF, 241EF, 241FF, 242FF, 242GF, 241JF
-241KF, 242KF, 241LF, 242LF, 241MF, 242MF.
(6)
Install the forward cargo-compartment ceiling-panels 131MC, 131NC.
(7)
Install the forward cargo-compartment rear-partition 132PW.
(8)
Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-002).
(9)
Close the lateral avionics-compartment doors 822 and 824 (Ref. TASK 52-41-00-410-002).
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Subtask 32-33-16-942-052
C. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 32-33-16Page 445 1 1 Feb 01/03 1 1 1CES 1
TORQUE TUBE ASSEMBLY - MLG - REMOVAL/INSTALLATION
_________________________________________________ TASK 32-33-17-000-001 Removal of the Torque Tube Assembly-MLG
1.
Reason for the Job
__________________
Inspection of the Structural Area
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
Power 25-21-41-000-001 Removal of the Passenger Seats 25-28-41-000-001 Removal of the Textile Floor-Covering 32-00-00-481-001 Installation of the Safety Devices on the Landing
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