(2)
To get the rigging pins in, adjust the adjustable rods connected to the torque tubes, if necessary.
(3)
Put in the RIGGING PIN (98DNSA20208060) at positions Pin 4 and Pin 8.
(4)
To get the rigging pins in, adjust the adjustable rods connected to the input-lever of the gear-uplock, if necessary.
(5)
Make sure that all the installed rigging pins can be moved freely and easily.
Subtask 32-33-00-080-056-A
E. Remove the Rigging Pins
(1) Remove the rigging pins as follows:
(a) Remove the rigging pins at positions Pin 2 thru Pin 11. Subtask 32-33-00-820-069
F. Continue with the Adjustment Procedure
(1) On the panel 110VU, remove the wedges from the GRAVITY GEAR EXTN handle (18).
CAUTION : DO NOT TURN THE GRAVITY GEAR EXTENSION HANDLE MORE THAN 3
_______ FULL TURNS. THIS CAN CAUSE DAMAGE TO THE FREE FALL EXTENSION SYSTEM.
(2) Release the GRAVITY GEAR EXTN handle (18) from the center console and turn it:
-clockwise three turns
-counterclockwise three turns.
NOTE : This gives one complete cycle.
____
(3) Operate the GRAVITY GEAR EXTN handle (18) through ten cycles. At the same time make sure that the mechanism does not touch the aircraft structure.
1EFF : ALL 1 32-33-00Page 571 1 1 Aug 01/05R 1 1 1CES 1
Subtask 32-33-00-865-062
G. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 52GA.
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 32-33-00-410-058
H. Close Access
(1)
Close the NLG doors (Ref. TASK 32-22-00-410-001).
(2)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
(3)
Install the cockpit floor panels 211FF, 211JF (Ref. TASK 53-12-11-400-001).
(4)
Install the forward cargo-compartment ceiling-panels 131AC, 131BC, 131CC.
(5)
Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-002).
R **ON A/C 151-199, 401-499,
Subtask 32-33-00-410-058-A
H. Close Access
(1)
Close the NLG doors (Ref. TASK 32-22-00-410-001).
(2)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
(3)
Install the cockpit floor panels 211FF, 211JF (Ref. TASK 53-12-11-400-001).
(4)
Install the forward cargo-compartment ceiling-panels 131MC, 131NC.
(5)
Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-002).
1EFF : ALL 1 32-33-00Page 572 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
Subtask 32-33-00-720-055
J. Test CAUTION : MAKE SURE THAT THE RIGGING PINS ARE REMOVED BEFORE OPERATION OF
_______ THE FREE FALL SYSTEM. DAMAGE WILL OCCUR IF THE RIGGING PINS ARE INSTALLED DURING SYSTEM OPERATION.
(1)
Lift the aircraft on jacks (Ref. TASK 07-11-00-581-001).
(2)
Do a functional test of the landing-gear free-fall extension system (Ref. TASK 32-33-00-720-001).
(3)
Lower the aircraft off jacks (Ref. TASK 07-11-00-586-002).
5. Close-up
________ Subtask 32-33-00-869-082
A. Ground Configuration
(1) If you did the flight configuration precautions, put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
Subtask 32-33-00-942-059
B. 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.
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TASK 32-33-00-720-003
Functional Check of Free-Fall Extension with one Downlocking Spring Removed
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.
NOTE : The check that follows is to check for stiffness in the mechanism of
____ each landing gear. The condition of the landing gear is satisfactory when the landing gears can be locked down by one of their two locksprings.
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