-192KB
 -192FB.

 (3) Remove the warning notice(s). Subtask 21-52-32-862-050
 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 CONDENSER (10HM2,11HM2) - INSPECTION/CHECK
__________________________________________
 TASK 21-52-32-200-001
 Attachment Components (In-Service Wear Limits) - Condensor 10HM2 (11HM2)

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-52-00-300-001 Attachment Components - Repair/Replacement
 CMM 215210
 21-52-32-991-003 Fig. 601

 3. Job Set-up
__________
 Subtask 21-52-32-860-054

 A. Aircraft Maintenance Configuration
 (1) Make sure that the applicable components are disassembled to do the inspection procedure.
 4. Procedure
_________
 (Ref. Fig. 601/TASK 21-52-32-991-003)
 Subtask 21-52-32-210-051

 A. Visual Inspection of the Spherical Bearings in the Support Rod
 (1) On the support rods (72a), (72b) and (73):
R (a) Use an applicable measurement method and do a check for radial R and axial play at the spherical bearings (1).

R  Attachment Components Figure 601/TASK 21-52-32-991-003
 1EFF : 1 1 1CES  ALL  1 111 21-52-32 Page 602 May 01/00

R R R R  (b) If you find more than 0.05 mm (0.0019 in.) radial play or more than 0.2 mm (0.0078 in.) axial play in a spherical bearing (1) then you must replace the related rod eye-end (Ref. TASK 21-52-00-300-001).
 Subtask 21-52-32-220-050
 B. In-Service Wear Limits
 (1) Use applicable measurement equipment and measure the outside diameter (OD) of the bushing (31) and the inside diameter (ID) of the shouldered bushing (3).
 NOTE : If any of the components are 'out of limits' then you must____ replace them, - for item (3) (Ref. TASK 21-52-00-300-001).
 -------------------------------------------------------------------------------
R R R R R R R  | FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | DD | 8.986 | 8.995 | | | 8.979 | | | | OD 31 |(0.3537) |(0.3541) | | |(0.3535) | | | | | | | 0.005 | 0.029 | | | 0.043 | | | | | (0.0001)| (0.0011)| | |(0.0016)| | DD | 9.000 | 9.015 | | | | 9.022 | | | ID 3 |(0.3543) |(0.3549) | | | |(0.3551) | | -------------------------------------------------------------------------------
Subtask 21-52-32-220-051
 C. In-Service Wear Limits
 (1) Use applicable measurement equipment and measure the OD of the bolt (29) and the ID of the bushing (31).
 NOTE : If any of the components are 'out of limits' then you must____ replace them.

 -------------------------------------------------------------------------------
R R R R R R R  | FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | DD | 6.325 | 6.335 | | | 6.318 | | | | OD 29 |(0.2490) |(0.2494) | | |(0.2487) | | | | | | | 0.015 | 0.040 | | | 0.054 | | | | | (0.0005)| (0.0015)| | |(0.0021)| | DD | 6.350 | 6.365 | | | | 6.372 | | | ID 31 |(0.2500) |(0.2505) | | | |(0.2508) | | -------------------------------------------------------------------------------
Subtask 21-52-32-220-052
 D. In-Service Wear Limits
 (1) Use applicable measurement equipment and measure the OD of the bolt (29) and the ID of the shouldered bushing (2).
 NOTE : If any of the components are 'out of limits' then you must____ replace them, - for item (2) (Ref. TASK 21-52-00-300-001).
 -------------------------------------------------------------------------------
R R R R R R R  | FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | DD | 6.325 | 6.335 | | | 6.318 | | | | OD 29 |(0.2490) |(0.2494) | | |(0.2487) | | | | | | | 0.015 | 0.035 | | | 0.049 | | | | | (0.0005)| (0.0013)| | |(0.0019)| | DD | 6.350 | 6.360 | | | | 6.367 | | | ID 2 |(0.2500) |(0.2503) | | | |(0.2506) | | -------------------------------------------------------------------------------
　
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