W DOC AIRBUS | AMM A320F

Air-Inlet Flap Mechanism - In-Service Wear Limits


TASK 21-61-51-200-003-A
Air-Inlet Flap Mechanism - In-Service Wear Limits


1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TASK 21-61-00-300-001-A
Attachment and Linkage Components - Repair/Replacement
TASK 21-61-51-000-003-A
Removal of the Air-Inlet Flap Mechanism
TASK 21-61-51-200-003-A
Air-Inlet Flap Mechanism - In-Service Wear Limits
TASK 21-61-51-400-003-A
Installation of the Air-Inlet Flap Mechanism
3. Job Set-up
Subtask 21-61-51-860-058-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the applicable components are disassembled to do the inspection procedure.
4. Procedure
Subtask 21-61-51-210-052-B
A. Visual Inspection of the Spherical Bearings
NOTE: The tolerance for radial play in a spherical bearing is 0.05 mm (0.0020 in.).
The tolerance for axial play in a spherical bearing is 0.2 mm (0.0079 in.).
   (1) Use an applicable measurement method and:
     (a) Do a check for radial and axial play at the spherical bearings (3) in the tie-rod (10):
     (b) Do a check for radial and axial play at the spherical bearings (4) and (6) in the bracket (15):
  • if you find radial and/or axial play more than the tolerances then replace the bracket (15).
     (c) Do a check for radial and axial play at the spherical bearing (11):
Subtask 21-61-51-220-052-B
B. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the outside diameter (OD) of the bolt (16) and the inside diameter (ID) of the bushings (2).
NOTE: If any of the components are 'out of limits' then replace them.

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


6.318


OD 16
(0.2490)
(0.2494)


(0.2487)





0.0230
0.0550


0.0690



(0.0009)
(0.0022)


(0.0027)
AA
6.358
6.380



6.387

ID 2
(0.2503)
(0.2512)



(0.2515)

Subtask 21-61-51-220-053-B
C. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (16) and the ID of the 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
AA
6.325
6.335


6.317


OD 16
(0.2490)
(0.2494)


(0.2487)





0.0050
0.0190


0.0340



(0.0002)
(0.0007)


(0.0013)
AA
6.340
6.344



6.351

ID 3
(0.2496)
(0.2498)



(0.2500)

Subtask 21-61-51-220-054-B
D. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (1) and the ID of the spacer (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
BB
9.499
9.509


9.492


OD 1
(0.3740)
(0.3744)


(0.3737)





0.0050
0.0290


0.0430



(0.0002)
(0.0011)


(0.0017)
BB
9.514
9.528



9.535

ID 5
(0.3746)
(0.3751)



(0.3754)

Subtask 21-61-51-220-055-B
E. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (1) and the ID of the bushing (18).
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
BB
9.499
9.509


9.492


OD 1
(0.3740)
(0.3744)


(0.3737)





0.0050
0.0290


0.0430



(0.0002)
(0.0011)


(0.0017)
BB
9.514
9.528



9.535

ID 18
(0.3746)
(0.3751)



(0.3754)

Subtask 21-61-51-220-056-B
F. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bushing (18) and the ID of the spherical bearing (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
BB
12.683
12.694


12.684


OD 18
(0.4993)
(0.4998)


(0.4994)





0.0060
0.0350


0.0410



(0.0002)
(0.0014)


(0.0016)
BB
12.700
12.718



12.725

ID 6
(0.5000)
(0.5007)



(0.5010)

Subtask 21-61-51-220-057-B
G. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (14) and the ID of the bushing (13).
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
6.337


6.318


OD 14
(0.2490)
(0.2495)


(0.2487)





0.0030
0.0270


0.0410



(0.0001)
(0.0011)


(0.0016)
CC
6.340
6.352



6.359

ID 13
(0.2496)
(0.2501)



(0.2504)

Subtask 21-61-51-220-058-B
H. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bushing (13) 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
CC
9.983
9.992


9.976


OD 13
(0.3930)
(0.3934)


(0.3928)





0.0080
0.0350


0.0490



(0.0003)
(0.0014)


(0.0019)
CC
10.000
10.018



10.025

ID 4
(0.3937)
(0.3944)



(0.3947)

Subtask 21-61-51-220-059-B
I. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (14) 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
CC
6.325
6.337


6.318


OD 14
(0.2490)
(0.2495)


(0.2487)





0.0030
0.0270


0.0410



(0.0001)
(0.0011)


(0.0016)
CC
6.340
6.352



6.359

ID 5
(0.2496)
(0.2501)



(0.2504)

Subtask 21-61-51-220-060-A
J. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (7) 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
7.905
7.925


7.898


OD 7
(0.3112)
(0.3120)


(0.3109)





0.0050
0.0360


0.0500



(0.0002)
(0.0014)


(0.0020)
DD
7.930
7.941



7.948

ID 4
(0.3122)
(0.3126)



(0.3129)

Subtask 21-61-51-220-061-A
K. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bolt (7) and the ID of the 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
DD
7.905
7.925


7.898


OD 7
(0.3112)
(0.3120)


(0.3109)





0.0050
0.0360


0.0500



(0.0002)
(0.0014)


(0.0020)
DD
7.930
7.941



7.948

ID 8
(0.3122)
(0.3126)



(0.3129)

Subtask 21-61-51-220-062-A
L. In-Service Wear Limits
   (1) Use applicable measurement equipment and measure the OD of the bushing (8) 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
11.983
11.994


11.976


OD 8
(0.4718)
(0.4722)


(0.4715)





0.0060
0.0350


0.0490



(0.0002)
(0.0014)


(0.0019)
DD
12.000
12.018



12.025

ID 5
(0.4724)
(0.4731)



(0.4734)

[Rev.10 from 2021] 2026.04.02 06:48:58 UTC