1EFF : ALL 1 32-42-00Page 406 1 1 May 01/04 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 32-42-00-040-053
C. Deactivation with the Brake Removal
(Ref. Fig. 402/TASK 32-42-00-991-002)
(1) Remove the brake (Ref. TASK 32-42-27-000-001). NOTE : Install the nuts (8) and the washers (7) on the brake unit
____ bolts (10) when you remove the brake unit.
NOTE : When you remove the brake unit, you must use the high-pressure
____
blanking plugs.
(2)
Clean the sleeves (4) and (12) and the electrical connector (9) of the brake temperature sensor. Apply two or three turns of the wide self-adhesive fabric tape (20 mm (0.7874 in.) to 30 mm (1.1811 in.):
-
around the sleeves (4) and (12),
-
around the electrical connector (9) of the brake temperature sensor.
(3)
Tightly wind two or three turns of the corrosion-resistant steel lockwire dia 0.8 mm:
-
around the tape on the sleeves (4) and (12),
-
around the tape on the electrical connector (9).
(4)
Twist the lockwire. Put it through the nearest locking hole you can get access to.
NOTE : Make sure that the lockwire cannot rub when the landing gear
____
operates.
(5)
Remove the PROTECTIVE CONE (J47779) from the wheel axle (6).
(6)
Install the main landing-gear wheel (Ref. TASK 32-41-11-400-006).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-42-00Page 407 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Deactivation with Brake Removal
Figure 402/TASK 32-42-00-991-002
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 32-42-00Page 408 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 301-399,
R Subtask 32-42-00-040-053-A
R C. Deactivation with the Brake Removal
R (Ref. Fig. 402A/TASK 32-42-00-991-002-A)
R (1) Remove the brake (Ref. TASK 32-42-27-000-001).
R NOTE : Install the nuts (8) and the washers (7) on the brake unit____
R bolts (10) when you remove the brake unit.
R NOTE : When you remove the brake unit, you must use the high-pressure____
R blanking plugs.
R (2) Clean the sleeves (4) and (12) and the electrical connector (9) of
R the brake temperature sensor. Apply two or three turns of the wide
R self-adhesive fabric tape (20 mm (0.7874 in.) to 30 mm (1.1811 in.):
R - around the sleeves (4) and (12),
R - around the electrical connector (9) of the brake temperature
R sensor.
R (3) Tightly wind two or three turns of the corrosion-resistant steel
R lockwire dia 0.8 mm:
R - around the tape on the sleeves (4) and (12),
R - around the tape on the electrical connector (9).
R (4) Twist the lockwire. Put it through the nearest locking hole you can
R get access to.
R NOTE : Make sure that the lockwire cannot rub when the landing gear____
R operates.
R (5) Remove the GUIDE CONE (Q47323-1) from the wheel axle (6).
R (6) Install the main landing-gear wheel (Ref. TASK 32-41-11-400-006).
R 1EFF : 301-399, 1 32-42-00Page 409 1 1 May 01/04 1 1 1CES 1
R Deactivation with Brake Removal
R Figure 402A/TASK 32-42-00-991-002-A
R 1EFF : 301-399, 1 32-42-00 Page 410
1 1 May 01/04
1 1
1CES 1
R **ON A/C ALL
Subtask 32-42-00-865-063
D. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------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
Subtask 32-42-00-860-069
E. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Pressurize the Yellow hydraulic system with the Yellow electric pump. (Ref. TASK 29-24-00-863-001)
(3)
On the panel 402VU, make sure that the A/SKID & NOSE WHEEL switch is set to ON.
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