(b)
 Put a warning notice in position to tell persons not to operate these pushbutton switches.

 (2)
 On the HP ground connector put a warning notice in position to tell persons not to supply the ground air.

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 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 Subtask 21-52-32-020-050
 A. Removal of the Condensor
 (Ref. Fig. 401/TASK 21-52-32-991-001)

 (1)
 Disconnect the electrical connector (27).

 (2)
 Put blanking caps on the disconnected electrical connectors.

 (3)
 Disconnect the sense lines (3), (8), and (18).

 (4)
 Put blanking plugs on the disconnected line ends.

 (5)
 Loosen the clamp (24) and disconnect the sleeve (23).

 (6)
 Remove the clamp (20).

 (7)
 Remove and discard the nuts (6), the washers (7) and disconnect the retaining cables (11).

 NOTE : Hold the hexagon part of the retaining cables (11) to prevent
____ twisting of the cables when you remove the nuts (6).
 (8)
 Remove and discard the lockwire and remove the clamp (15).

 (9)
 Remove the half clamps (13) and move the sleeve (14) away from the condensor (22).

 (10) Hold the condensor (22) and:
R (a) Remove the nuts (34), the washers (33), the bolts (29), (where R installed, the washers (30)) and the bushes (31).
 (b) Disconnect the support rods (72A) and (73) and remove the condensor (22) from the aircraft.
 (11)
 Remove the sleeves (10) and (14).

 (12)
 Remove and discard the seals (9) and the packings (16) and (21).

 (13)
 Put blanking plugs on the disconnected line ends.

 Condensor - Component Location Figure 401/TASK 21-52-32-991-001- 12 (SHEET 1)
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 Condensor - Component Location Figure 401/TASK 21-52-32-991-001- 22 (SHEET 2)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 21-52-32Page 407 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1R **ON A/C 401-499,

 Subtask 21-52-32-020-050-A
 A. Removal of the Condensor
 (Ref. Fig. 401A/TASK 21-52-32-991-001-A)

 (1)
 Disconnect the electrical connector (24).

 (2)
 Put blanking caps on the disconnected electrical connectors.

 (3)
 Loosen the clamp (21) and disconnect the sleeve (20).

 (4)
 Remove the clamp (17).

 (5)
 Remove and discard the nuts (5), the washers (6) and disconnect the retaining cables (7).

 NOTE : Hold the hexagon part of the retaining cables (7) to prevent
____ twisting of the cables when you remove the nuts (5).
 (6)
 Remove and discard the lockwire and remove the clamp (13).

 (7)
 Remove the half clamps (11) and move the sleeve (12) away from the condensor (19).

 (8)
 Hold the condensor (19) and:

R (a) Remove the nuts (34), the washers (33), the bolts (29), (where R installed, the washers (30)) and the bushes (31).
 (b) Disconnect the support rods (72A) and (73) and remove the condensor (19) from the aircraft.
 (9) Remove the sleeves (8) and (12).
 (10)
 Remove and discard the seals (7) and the packings (14) and (18).

 (11)
 Put blanking plugs on the disconnected line ends.

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 **ON A/C ALL
 Subtask 21-52-32-020-052
 B. Removal of the Attachment Components (Ref. Fig. 402/TASK 21-52-32-991-002) 
R R R  (1) Remove the nuts (34), the washers (33), the bolts (29), and if installed, the washers (30), the bushes (31) and the support rods (72A), (72B) and (73). 
R R  NOTE : Identify the support rods, to make sure they have the correct____ position in the installation procedure.
 (2) Remove the nut (3), the washer (2), the bolt (4) and disconnect the support rod (72A) from the support rod (72B).
 (3) Do the inspection of the components for in-service wear (Ref. TASK 21-52-32-200-001). 

R 1EFF : ALL 1 21-52-32Page 409 1 1 Aug 01/05 1 1 1CES 1

 Condensor - Component Location
 Figure 401A/TASK 21-52-32-991-001-A12 (SHEET 1)

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 Condensor - Component Location
　
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