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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