____ You can use Material No. 04-022 as an alternative to Material No. 04-004. Clean and degrease the parts before you use Material No. 04-022.
 (c)
 Put the other steel plate on the top of the greased steel plate.

 (d)
 Move the aircraft and position the nose wheels on the greased steel plates (Ref. TASK 09-10-00-584-002).

 (4) If the test is to be done with the nose wheels clear of the ground do this:
 (a) Lift the nose gear (Ref. TASK 07-12-00-582-001). NOTE : Use only a compact axle jack to lift the nose gear.
____
 (5)
 On the nose gear leg, on the electrical box, make sure that the
 towing lever is in the normal position (engaged position).

 (6)
 On the panel 400VU, make sure that the landing gear control lever is in the DOWN position.

 (7)
 On the panel 402VU, make sure that the ANTI SKID NOSE WHEEL switch is in the ON position.

 (8)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
 (Ref. TASK 31-60-00-860-001).

 (9)
 On the ECAM control panel, push the WHEEL pushbutton switch.

 (10)
 Make sure that the rudder pedals and the two nose-wheel steering handwheels are in the neutral position.

 (11)
 On the overhead panel 23VU: - Make sure that the FLT CTL/ELAC 1 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are OFF).

 (12)
 On the overhead panel 24VU: - Make sure that the FLT CTL/ELAC 2 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are OFF).

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-51-00Page 518 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1

R  **ON A/C 401-499, 
R  Subtask 32-51-00-860-054-A 
R  A. Aircraft Maintenance Configuration 
R  (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-
R  002). 
R  (2) Pressurize the Yellow hydraulic system (Ref. TASK 29-10-00-863-002). 
R  (3) If the test is to be done with the nosewheels on the ground, do these 
R  steps: 
R  NOTE : You will need two 1.2 m (3.93 ft.) square steel plates.____ 
R  (a) Position a steel plate in front of the nosewheels. 
R  (b) Apply a thick layer of COMMON GREASE (Material No. 04-004) or 
R  COMMON GREASE (Material No. 04-022) to the upper surface of the 
R  steel plate. 
R  NOTE : Do not mix Material No. 04-004 with Material No. 04-022.____ 
R  You can use Material No. 04-022 as an alternative to 
R  Material No. 04-004. Clean and degrease the parts before 
R  you use Material No. 04-022. 
R  (c) Put the other steel plate on the top of the greased steel plate. 
R  (d) Move the aircraft and position the nose wheels on the greased 
R  steel plates (Ref. TASK 09-10-00-584-002). 
R  (4) If the test is to be done with the nose wheels clear of the ground do 
R  this: 
R  (a) Lift the nose gear (Ref. TASK 07-12-00-582-001). 
R  NOTE : Use only a compact axle jack to lift the nose gear.____ 
R  (5) On the nose gear leg, on the electrical box, make sure that the 
R  towing lever is in the normal position (engaged position). 
R  (6) On the panel 400VU, make sure that the landing gear control lever is 
R  in the DOWN position. 

R 1EFF : 401-499, 1 32-51-00Page 519 1 1 Aug 01/05 1 1 1CES 1

R R  (7) On the panel 402VU, make sure that the ANTI SKID NOSE WHEEL switch is in the ON position. 
R R  (8) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001). 
R  (9) On the ECAM control panel, push the WHEEL pushbutton switch. 
R R  (10) Make sure that the rudder pedals and the two nose-wheel steering handwheels are in the neutral position. 
R R R  (11) On the overhead panel 23VU: - Make sure that the FLT CTL/ELAC 1 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are OFF). 
R R R  (12) On the overhead panel 24VU: - Make sure that the FLT CTL/ELAC 2 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are OFF). 
R  **ON A/C ALL
 Subtask 32-51-00-865-089
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU L/G/LGCIU/SYS1/NORM 1GA C09 49VU NAV PROBES/ADIRU 1/AND AOA 1/26VAC 5FP1 F07 49VU NAV PROBES/ADIRU1/115VAC 4FP1 F06
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架8(81)