(a)
 FOR 10HM8

 -191KB.

 (b)
 FOR 11HM8

 -192KB. Subtask 21-52-16-862-050
 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 EXTRACTOR - WATER (10HM8,11HM8) - INSPECTION/CHECK__________________________________________________
 TASK 21-52-16-200-001
 Attachment Components (In-Service Wear Limits) - Water Extractor 10HM8 (11HM8)
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-52-00-300-001 CMM 215204 21-52-16-991-003  Attachment Components - Repair/ReplacementFig. 601
 3. Job Set-up__________
 Subtask 21-52-16-860-052
 A. Aircraft Maintenance Configuration
 (1) Make sure that the applicable components are disassembled to do the inspection procedure.
 4. Procedure_________
 (Ref. Fig. 601/TASK 21-52-16-991-003)
 Subtask 21-52-16-210-051 
R  A. Visual Inspection of the Spherical Bearings in the Support Rod 
R R  (1) Use an applicable measurement method and do a check for radial and axial play at the spherical bearings (1) in the support rod (71). 
R R R R  (a) 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).

R  Attachment Components Figure 601/TASK 21-52-16-991-003
 1EFF : 1 1 1CES  ALL  1 111 21-52-16 Page 602 May 01/00

 Subtask 21-52-16-220-050 
R  B. In-Service Wear Limits
 (1) Use applicable measurement equipment and measure the outside diameter (OD) of the bushing (14) 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | BB | 8.986 | 8.995 | | | 8.979 | | | | OD 14 |(0.3537) |(0.3541) | | |(0.3535) | | | | | | | 0.005 | 0.029 | | | 0.043 | | | | | (0.0001)| (0.0011)| | |(0.0016)| | BB | 9.000 | 9.015 | | | | 9.022 | | | ID 3 |(0.3543) |(0.3549) | | | |(0.3551) | | -------------------------------------------------------------------------------
Subtask 21-52-16-220-051 
R  C. In-Service Wear Limits
 (1) Use applicable measurement equipment and measure the OD of the bolt (15) and the ID of the bushing (14).
 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | BB | 6.325 | 6.335 | | | 6.318 | | | | OD 15 |(0.2490) |(0.2494) | | |(0.2487) | | | | | | | 0.015 | 0.040 | | | 0.054 | | | | | (0.0005)| (0.0015)| | |(0.0021)| | BB | 6.350 | 6.365 | | | | 6.372 | | | ID 14 |(0.2500) |(0.2505) | | | |(0.2508) | | -------------------------------------------------------------------------------
Subtask 21-52-16-220-052 
R  D. In-Service Wear Limits
 (1) Use applicable measurement equipment and measure the OD of the bolt (15) 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.)| |--------|---------|---------|---------|---------|---------|---------|--------| | BB | 6.325 | 6.335 | | | 6.318 | | | | OD 15 |(0.2490) |(0.2494) | | |(0.2487) | | | | | | | 0.015 | 0.035 | | | 0.049 | | | | | (0.0005)| (0.0013)| | |(0.0019)| | BB | 6.350 | 6.360 | | | | 6.367 | | | ID 2 |(0.2500) |(0.2503) | | | |(0.2506) | | -------------------------------------------------------------------------------
　
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