(4)
Install the bolt (104), the screw (100), the washers (110) and the nuts (111). Tighten the nuts (111).
(5)
Put the upper electrical harness through the protector (91).
(6)
Attach the electrical harness with the clamp (95), the support (96), the bolt (94), the washer (97) and the nut (98). Tighten the nut (98).
(7)
Remove the blanking caps and connect the electrical connector (90).
(8)
Install the clamp (101), the washer (102) and the nut (103). Tighten the nut (103).
NOTE : Use a flat spanner to make sure that the screw (100) does not
____
turn.
(9) Do a check for possible damage on connectors, proximity sensors and targets.
(10)
Apply COMMON GREASE (Material No. 04-022) to the hinges of the torque links (Ref. TASK 12-22-32-640-001).
(11)
Install the removed wheel of the nose gear (Ref. TASK 32-41-12-400-001).
(12) Apply SEALANTS (Material No. 09-001) to the areas identified E. R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 32-21-27-720-051
D. Test
(1)
Do a functional test of the normal extension and retraction of the nose landing gear (Ref. TASK 32-31-00-720-003).
(2)
Do a functional test of the Nose Wheel Steering (Ref. TASK 32-51-00-720-003).
R 1EFF : 001-049, 051-054, 101-149, 151-199, 1 32-21-27Page 436 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 1EFF : ALL 1 32-21-27Page 437 1 1 May 01/05 1 1 1CES 1 ATTACHMENT - NLG TOWING (2701GM) - REMOVAL/INSTALLATION
R **ON A/C 051-099,
R Subtask 32-21-27-720-051-A
R D. Test
R R (1) Do a functional test of the normal extension and retraction of the nose landing gear (Ref. TASK 32-31-00-720-003).
R R (2) Do a functional test of the Nose Wheel Steering (Ref. TASK 32-51-00-720-003).
R R (3) Do an operational test of the Tire Pressure Indicating System (Ref. TASK 32-49-00-710-001).
R **ON A/C ALL
5. Close-up________
Subtask 32-21-27-860-052
A. Put the aircraft back to its initial configuration.
(1) Lower the aircraft on its wheels (Ref. TASK 07-11-00-586-001).
(2) Remove the safety barriers.
(3) Remove the warning notice(s).
(4) Make sure that the work area is clean and clear of tool(s) and other items.
_______________________________________________________
TASK 32-21-41-000-001
Removal of the NLG TOWING attachment (2701GM)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific spatula
No specific warning notices
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 32-21-41-991-001-A Fig. 401
3. Job Set-up
__________
Subtask 32-21-41-941-050
A. Safety Precaution
(1)
In the cockpit, on the panel 400VU, put the warning notice in position to tell persons not to operate the landing gear control lever.
(2)
Put the warning notices in position to tell persons not to operate the nose wheel steering system: - on the brake pedals - on the nose wheel steering handwheel (18VU, 19VU).
1EFF : ALL 1 32-21-41Page 401 1 1 Feb 01/05 1 1 1CES 1
4. Procedure
_________ R (Ref. Fig. 401/TASK 32-21-41-991-001-A) Subtask 32-21-41-020-050
A. Removal of the NLG Towing Attachment
(1)
Remove the rubber sealant with a spatula to prevent damage to the surface protection.
(2)
Remove and discard the cotter pins (6).
(3)
Remove the nuts (5), the washers (3) and (4).
(4)
Remove the bolts (1) and the washers (2).
(5)
Remove the NLG towing attachment (7).
1EFF : ALL 1 32-21-41Page 402 1 1 Feb 01/05 1 1 1CES 1
R R NLG Towing Attachment - Installation Figure 401/TASK 32-21-41-991-001-A
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架3(117)
