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时间:2011-03-25 17:58来源:蓝天飞行翻译 作者:admin
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 (1) To let the cables and linkages become stable, operate the free-fall extension system through ten full cycles:
 (a) For one full cycle, on the panel 110VU: - operate the GRAVITY GEAR EXTN handle three turns in a clockwise direction at a rate of one turn every five seconds
 - operate the GRAVITY GEAR EXTN handle three turns in a counter-clockwise direction at a rate of one turn every five seconds.
 (2) Lock the GEAR GRAVITY EXTN operating handle (1):
 (a)
 Put the handle (1) in the stowed position.

 (b)
 Put a wedge at each side of the handle (1), to keep it in position and prevent its movement.


 Subtask 32-33-00-860-076
 M. Aircraft Maintenance Configuration
 (1)
 Open the NLG doors (Ref. TASK 32-22-00-010-001).

 (2)
 Make sure that a SAFETY PIN - NLG DOOR is installed in each NLG door.

 (3)
 Open the MLG doors (Ref. TASK 32-12-00-010-001).


 1EFF : ALL 1 32-33-00Page 558 1 1 Aug 01/05R 1 1 1CES 1


 (4) Make sure that a GROUND LOCK SLEEVE (460005835) is installed on each MLG door.
 Subtask 32-33-00-480-063
 N. Installation of the Rigging Pins
 (Ref. Fig. 505/TASK 32-33-00-991-013)

 (1)
 Install the RIGGING PIN (98A27801001000) at position Pin 12 and Pin

 1.

 (2)
 Install the RIGGING PIN (98DNSA20208060) at position Pin 2 and Pin

 11.

 (3)
 Make sure that the related parts are locked. NOTE : If the rigging pins can not be installed, adjust the MLG

____ mechanical system (Ref. TASK 32-33-00-820-004).

 (4)
 On the panel 110VU:


 -lock the GRAVITY GEAR EXTN handle (18) as follows:
 (a)
 Make sure that the handle (18) is folded into the center console.

 (b)
 Put a wedge at each side of the handle (18) to keep it in position and prevent its movement.


 Subtask 32-33-00-820-075
 P. Adjustment of the cables (1) and (2)
 (1) Adjust the MLG free-fall cables (1) and (2) again, as specified in paragraph 4. B.
 Subtask 32-33-00-820-076
 Q. Adjustment of the cables (3) and (4)
 (1) Adjust the MLG free-fall cables (3) and (4) again, as specified in paragraph 4. C.
 1EFF : ALL 1 32-33-00Page 559 1 1 Aug 01/05R 1 1 1CES 1


 Subtask 32-33-00-820-077 
R R  R. Adjustment of the cables (5) and (6) (Ref. Fig. 509/TASK 32-33-00-991-015, 510/TASK 32-33-00-991-024)
 (1) Adjust the MLG free-fall cables (5) and (6) again, as specified in paragraph 4. D.
 Subtask 32-33-00-820-078
 S. Adjustment of the cables (7) and (8)
 (1) Adjust the MLG free-fall cables (7) and (8) again, as specified in paragraph 4. E.
 Subtask 32-33-00-820-079 
R R  T. Adjustment of the cables (9) and (10) (Ref. Fig. 509/TASK 32-33-00-991-015, 510/TASK 32-33-00-991-024)
 (1) Adjust the MLG free-fall cables (9) and (10) again, as specified in paragraph 4. F.
 Subtask 32-33-00-820-080
 U. Adjustment of the cables (11) and (12)
 (1) Adjust the MLG free-fall cables (11) and (12) again, as specified in paragraph 4. G.
 Subtask 32-33-00-080-060
 V. Removal of the Rigging Pins (Ref. Fig. 505/TASK 32-33-00-991-013)
 (1) Remove the RIGGING PIN at position Pin 12 and Pin 1.
 (2) Remove the RIGGING PIN at position Pin 2 and Pin 11.
 (3) On the panel 110VU: - remove the wedges from the GRAVITY GEAR EXTN handle (18).

 1EFF : ALL 1 32-33-00Page 560 1 1 Aug 01/05 1 1 1CES 1 Subtask 32-33-00-869-071


 W. 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).
 **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
 Subtask 32-33-00-410-056
 X. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the NLG doors (Ref. TASK 32-22-00-410-001).

 (3)
 Close the MLG doors (Ref. TASK 32-12-00-410-001).

 (4)
 Install the cockpit floor panels 211FF, 211JF (Ref. TASK 53-12-11-400-001).

 (5)
 Install the passenger compartment floor panels 241EF, 242FF (Ref. TASK 53-32-12-400-002).

 (6)
 Install the forward cargo-compartment ceiling-panels 131AC, 131BC, 131CC.

 (7)
 Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-002).


R **ON A/C 151-199, 401-499,
 Subtask 32-33-00-410-056-A
 
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