W DOC AIRBUS | AMM A320F

Attachment Components (In-Service Wear Limits) - Heat Exchanger


TASK 21-52-24-200-001-A
Attachment Components (In-Service Wear Limits) - Heat Exchanger


FIN: 10HM4
FIN: 11HM4
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TASK 21-52-00-300-001-A
Attachment Components - Repair/Replacement
3. Job Set-up
Subtask 21-52-24-860-054-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the applicable components are disassembled to do the inspection procedure.
4. Procedure
Subtask 21-52-24-210-053-A
A. Visual Inspection of the Spherical Bearings in the Support Rods and Bracket
   (1) on the support rods (80), (82) and (83):
     (a) Use an applicable measurement method and do a check for radial and axial play at the spherical bearings (1) in the support rods (80), (82) and (83):
  • if you find more than 0.05 mm (0.0020 in.) radial play, or more than 0.2 mm (0.0079 in.) axial play in a spherical bearing (1) then you must replace the related eye-end in the support rod (80), (82) and (83) (Ref. AMM TASK 21-52-00-300-001).
   (2) Use an applicable measurement method and do a check for radial play at the spherical bearing (7) in the bracket (30):
  • if you find more than 0.2 mm (0.0079 in.) radial play in the spherical bearing (7) then you must replace it.
Subtask 21-52-24-220-050-A
B. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the outside diameter (OD) of the bushing (58) 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,

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
8.986
8.995


8.979


OD 58
(0.3538)
(0.3541)


(0.3535)





0.0050
0.0290


0.0430



(0.0002)
(0.0011)


(0.0017)
CC
9.000
9.015



9.022

ID 3
(0.3543)
(0.3549)



(0.3552)

Subtask 21-52-24-220-051-A
C. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (56) and the ID of the bushing (58).
NOTE: If any of the components are 'out of limits' then you must replace them.

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
6.325
6.335


6.318


OD 56
(0.2490)
(0.2494)


(0.2487)





0.0150
0.0400


0.0540



(0.0006)
(0.0016)


(0.0021)
CC
6.350
6.365



6.372

ID 58
(0.2500)
(0.2506)



(0.2509)

Subtask 21-52-24-220-052-A
D. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (56) and the ID of the shouldered bushing (2).
NOTE: If any of the components are 'out of limits' then you must replace them,

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
6.325
6.335


6.318


OD 56
(0.2490)
(0.2494)


(0.2487)





0.0150
0.0350


0.0490



(0.0006)
(0.0014)


(0.0019)
CC
6.350
6.360



6.367

ID 2
(0.2500)
(0.2504)



(0.2507)

Subtask 21-52-24-220-053-A
E. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bushing (58) and the ID of the shouldered bushing (5).
NOTE: If any of the components are 'out of limits' then you must replace them,

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
DD
8.986
8.995


8.979


OD 58
(0.3538)
(0.3541)


(0.3535)





0.0050
0.0290


0.0430



(0.0002)
(0.0011)


(0.0017)
DD
9.000
9.015



9.022

ID 5
(0.3543)
(0.3549)



(0.3552)

Subtask 21-52-24-220-054-A
F. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (56) and the ID of the bushing (58).
NOTE: If any of the components are 'out of limits' then you must replace them.

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
DD
6.325
6.335


6.318


OD 56
(0.2490)
(0.2494)


(0.2487)





0.0150
0.0400


0.0540



(0.0006)
(0.0016)


(0.0021)
DD
6.350
6.365



6.372

ID 58
(0.2500)
(0.2506)



(0.2509)

Subtask 21-52-24-220-055-A
G. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (56) and the ID of the shouldered bushing (4).
NOTE: If any of the components are 'out of limits' then you must replace them,

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
DD
6.325
6.335


6.318


OD 56
(0.2490)
(0.2494)


(0.2487)





0.0150
0.0350


0.0490



(0.0006)
(0.0014)


(0.0019)
DD
6.350
6.360



6.367

ID 4
(0.2500)
(0.2504)



(0.2507)

Subtask 21-52-24-220-056-A
H. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bushing (38) and the ID of the shouldered bushing (8).
NOTE: If any of the components are 'out of limits' then you must replace them,

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
EE
8.986
8.995


8.979


OD 38
(0.3538)
(0.3541)


(0.3535)





0.0050
0.0290


0.0430



(0.0002)
(0.0011)


(0.0017)
EE
9.000
9.015



9.022

ID 8
(0.3543)
(0.3549)



(0.3552)

Subtask 21-52-24-220-057-A
I. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (40) and the ID of the bushing (38).
NOTE: If any of the components are 'out of limits' then you must replace them.

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
EE
6.325
6.335


6.318


OD 40
(0.2490)
(0.2494)


(0.2487)





0.0150
0.0400


0.0540



(0.0006)
(0.0016)


(0.0021)
EE
6.350
6.365



6.372

ID 38
(0.2500)
(0.2506)



(0.2509)

Subtask 21-52-24-220-058-A
J. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (40) and the ID of the shouldered bushing (6).
NOTE: If any of the components are 'out of limits' then you must replace them,

FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
EE
6.325
6.335


6.318


OD 40
(0.2490)
(0.2494)


(0.2487)





0.0150
0.0350


0.0490



(0.0006)
(0.0014)


(0.0019)
EE
6.350
6.360



6.367

ID 6
(0.2500)
(0.2504)



(0.2507)

[Rev.10 from 2021] 2026.04.02 06:11:29 UTC