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 nose wheels.
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 (7) On the panel 402VU, make sure that the ANTI SKID NOSE WHEEL switch is
R in the ON position.
R (8) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
R (Ref. TASK 31-60-00-860-001).
R (9) On the ECAM control panel, push the WHEEL pushbutton switch.
R (10) Make sure that the rudder pedals and the two nose-wheel steering
R handwheels are in the neutral position.
R 1EFF : 401-499, 1 32-51-00Page 534 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL
Subtask 32-51-00-865-091
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
**ON A/C 001-049, 051-061, 101-105, 201-203,
121VU ADIRS/ADIRU/3/26VAC AND AOA 5FP3 N08
121VU ADIRS/ADIRU/3/115VAC 4FP3 N06
**ON A/C ALL
121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
121VU ADIRS/ADIRU/3/26VAC AND AOA 5FP3 N07 121VU ADIRS/ADIRU/3/115VAC 4FP3 N05
1EFF : ALL 1 32-51-00Page 535 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
Subtask 32-51-00-865-068
C. Open, safety and tag this(these) circuit breaker(s): -------------------------------------------------------------------------------
PANEL ------ DESIGNATION ---------------------------------------- IDENT. LOCATION---------------------------------
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