(2)
In the cockpit, on the panel 400VU make sure that the warning notice is in position to tell persons not to operate the landing gear control lever.
(3)
Make sure that the wheel chocks are in position.
(4)
Make sure that the related axle is lifted with jack (Ref. TASK 07-12-00-582-002)
(5) Make sure that the tyre is fully deflated. Subtask 32-49-16-865-055
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU HYDRAULIC/TIRE/PRESS 1GV M31
1EFF : 051-099, 1 32-49-16Page 414 1 1 May 01/05 1 1 1CES 1
4. Procedure
_________
(Ref. Fig. 402/TASK 32-49-16-991-002) Subtask 32-49-16-420-051
A. Installation of the Pressure Transducer Adaptor
(1)
Make sure that the packing (2) is in position on the adaptor (3). NOTE : If you install the used adaptor (3), put a new packing (2) in
____
position.
(2)
Install the pressure transducer adaptor (3) on the wheel (1).
(3)
TORQUE the adaptor (3) to between 1.35 and 1.65 m.daN (119.46 and
146.01 lbf.in).
(4)
Make sure that the packing (4) is in position on the adaptor (3). NOTE : If you install the used adaptor (3), put a new packing (4) in
____
position.
(5)
Apply a thin layer of COMMON GREASE (Material No. 04-004) to the shaft of the adaptor (4).
(6)
Install the pressure transducer (5) on the adaptor (3). NOTE : Make sure that the pressure transducer (5) is in the correct
____
position.
(7)
Install the nut (7) and TORQUE it to between 0.3 and 0.9 m.daN (26.54 and 79.64 lbf.in).
(8) Safety the nut (7) with the new cotter pin (6). Subtask 32-49-16-865-056
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GV
1EFF : 051-099, 1 32-49-16Page 415 1 1 May 01/05 1 1 1CES 1 Subtask 32-49-16-860-065
C. Preparation before the Test
(1) Inflate the wheel to the unloaded pressure (Ref. TASK 12-14-32-614-001).
(2) Lower the aircraft on its wheels (Ref. TASK 07-12-00-582-002). Subtask 32-49-16-720-051
D. Functional test
(1) Do the functional test of the Tire Pressure Indicating System (Ref. TASK 32-49-00-720-001).
5. Close-up
________ Subtask 32-49-16-942-052
A. Put the aircraft back to its initial configuration.
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
1EFF : 051-099, 1 32-49-16Page 416 1 1 May 01/05 1 1 1CES 1
ROTATING MECHANISM - TPIS NLG (4GV,5GV) - REMOVAL/INSTALLATION
______________________________________________________________
TASK 32-49-17-000-001 Removal of the NLG TPIS Rotating Mechanism WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking cap No specific circuit breaker(s) safety clip(s) No specific cord No specific safety barriers No specific warning notice(s)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-49-17-991-001 Fig. 401
3. Job Set-up
__________ Subtask 32-49-17-941-050
A. Safety Precautions
(1)
In the cockpit, on the panel 400VU put warning notice(s) in position to tell persons not to operate the landing gear control lever.
(2)
Put the safety barriers in position.
1EFF : 051-099, 1 32-49-17Page 401 1 1 May 01/05 1 1 1CES 1 Subtask 32-49-17-865-050
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
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8(62)
