W DOC AIRBUS | AMM A320F

Inspection of the Aft Fixed Fairing


TASK 54-54-00-200-001-A
Inspection of the Aft Fixed Fairing


WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
ZONE: 470
ZONE: 480
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
470
ENGINE 1 AFT PYLON
480
ENGINE 2 AFT PYLON
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 54-54-00-000-001-A
Removal of the Aft Fixed Fairing
TASK 54-54-00-000-001-A-01
Removal of the Aft Fixed Fairing
TASK 54-54-00-400-001-A
Installation of the Aft Fixed Fairing
TASK 54-54-00-400-001-A-01
Installation of the Aft Fixed Fairing
TASK 78-30-00-040-012-A
Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance
TASK 78-30-00-081-041-A
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-081-041-B
Make the Thrust Reverser Serviceable after Maintenance
TASK 78-30-00-440-012-A
Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after Ground Maintenance
TASK 78-30-00-481-041-A
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-30-00-481-041-B
Make the Thrust Reverser Unserviceable for Maintenance
F Aft Fixed Fairing ** ON A/C NOT FOR ALL
F Aft Fixed Fairing ** ON A/C NOT FOR ALL
F Aft Fixed Fairing ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 54-54-00-941-052-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) On the center pedestal, on the ENG panel 115VU:
     (a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
   (2) Make sure that the engine 1 (2) shutdown occurred not less than 5 minutes before you do this procedure.
   (3) On the overhead maintenance panel 50VU:
     (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1 (2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2)
Subtask 54-54-00-040-050-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 54-54-00-040-050-B ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-040-012).
Subtask 54-54-00-941-053-A ** ON A/C NOT FOR ALL
C. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position:
     (a) in the zone 470 for the left pylon
     (b) in the zone 480 for the right pylon.
Subtask 54-54-00-020-051-A ** ON A/C NOT FOR ALL
D. Removal of Component
   (1) Remove the aft fixed fairing (Ref. AMM TASK 54-54-00-000-001).
4. Procedure
Subtask 54-54-00-220-050-A ** ON A/C NOT FOR ALL
A. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
E
0.3740
0.3745


0.3733


OD 1
(9.4996)
(9.5123)


(9.4818)





0.0003
0.0014


0.0028



(0.0076)
(0.0356)


(0.0711)
E
0.3748
0.3754



0.3761

ID 2
(9.5199)
(9.5351)



(9.5529)

Subtask 54-54-00-220-051-A ** ON A/C NOT FOR ALL
B. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
E
0.3740
0.3745


0.3728


OD 1
(9.4996)
(9.5123)


(9.4691)





0.0003
0.0022


0.0046



(0.0076)
(0.0559)


(0.1168)
E
0.3748
0.3762



0.3774

ID 3
(9.5199)
(9.5555)



(9.5859)

Subtask 54-54-00-220-052-A ** ON A/C NOT FOR ALL
C. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
E
0.4718
0.4722


0.4711


OD 3
(11.9837)
(11.9939)


(11.9659)





0.0002
0.0013


0.0028



(0.0051)
(0.0330)


(0.0711)
E
0.4724
0.4731



0.4739

ID 4
(11.9989)
(12.0167)



(12.0370)

Subtask 54-54-00-220-053-A ** ON A/C NOT FOR ALL
D. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
F
0.3740
0.3745


0.3733


OD 5
(9.4996)
(9.5123)


(9.4818)





0.0003
0.0014


0.0028



(0.0076)
(0.0356)


(0.0711)
F
0.3748
0.3754



0.3761

ID 6
(9.5199)
(9.5351)



(9.5529)

Subtask 54-54-00-220-054-A ** ON A/C NOT FOR ALL
E. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
F
0.3740
0.3745


0.3728


OD 5
(9.4996)
(9.5123)


(9.4691)





0.0003
0.0022


0.0046



(0.0076)
(0.0559)


(0.1168)
F
0.3748
0.3762



0.3774

ID 7
(9.5199)
(9.5555)



(9.5859)

Subtask 54-54-00-220-055-A ** ON A/C NOT FOR ALL
F. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
F
0.4718
0.4722


0.4711


OD 7
(11.9837)
(11.9939)


(11.9659)





0.0002
0.0013


0.0028



(0.0051)
(0.0330)


(0.0711)
F
0.4724
0.4731



0.4739

ID 8
(11.9989)
(12.0167)



(12.0370)

Subtask 54-54-00-220-056-A ** ON A/C NOT FOR ALL
G. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
G
0.4365
0.4370


0.4349


OD 9
(11.0871)
(11.0998)


(11.0464)





0.0020
0.0032


0.0064



(0.0508)
(0.0813)


(0.1626)
G
0.4390
0.4397



0.4413

ID 12
(11.1506)
(11.1684)



(11.2090)

Subtask 54-54-00-220-057-A ** ON A/C NOT FOR ALL
H. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
G
0.4365
0.4370


0.4346


OD 9
(11.0871)
(11.0998)


(11.0388)





0.0020
0.0032


0.0078



(0.0508)
(0.0813)


(0.1981)
G
0.4390
0.4397



0.4424

ID 10
(11.1506)
(11.1684)



(11.2369)

Subtask 54-54-00-220-058-A ** ON A/C NOT FOR ALL
I. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
G
0.5505
0.5509


0.5498


OD 10
(13.9827)
(13.9928)


(13.9649)





0.0003
0.0014


0.0028



(0.0076)
(0.0356)


(0.0711)
G
0.5512
0.5519



0.5526

ID 13
(14.0005)
(14.0182)



(14.0360)

Subtask 54-54-00-220-059-A ** ON A/C NOT FOR ALL
J. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
G
0.4365
0.4370


0.4361


OD 11
(11.0871)
(11.0998)


(11.0769)





-0.0004
0.0009


0.0017



(-0.0102)
(0.0229)


(0.0432)
G
0.4366
0.4374



0.4378

ID 14
(11.0896)
(11.1099)



(11.1201)

Subtask 54-54-00-220-060-A ** ON A/C NOT FOR ALL
K. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
G
0.3139
0.3144


0.3094


OD 11
(7.9730)
(7.9857)


(7.8587)





0.0006
0.0089


0.0179



(0.0152)
(0.2261)


(0.4547)
G
0.3150
0.3228



0.3273

ID 13
(8.0010)
(8.1991)



(8.3134)

Subtask 54-54-00-220-061-A ** ON A/C NOT FOR ALL
L. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
H
0.4365
0.4370


0.4350


OD 16
(11.0871)
(11.0998)


(11.0490)





0.0020
0.0032


0.0063



(0.0508)
(0.0813)


(0.1600)
H
0.4390
0.4397



0.4413

ID 15
(11.1506)
(11.1684)



(11.2090)

Subtask 54-54-00-220-062-A ** ON A/C NOT FOR ALL
M. Inspection of the Aft Fixed Fairing
   (1) Measure the dimension of the aft fixed fairing and make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
H
0.3740
0.3745


0.3733


OD 17
(9.4996)
(9.5123)


(9.4818)





0.0003
0.0014


0.0028



(0.0076)
(0.0356)


(0.0711)
H
0.3748
0.3754



0.3761

ID 18
(9.5199)
(9.5351)



(9.5529)

5. Close-up
Subtask 54-54-00-420-051-A ** ON A/C NOT FOR ALL
A. Installation of Component
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install the aft fixed fairing (Ref. AMM TASK 54-54-00-400-001).
Subtask 54-54-00-440-050-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-081-041).
Subtask 54-54-00-440-050-B ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-440-012).
Subtask 54-54-00-942-052-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.01 02:02:59 UTC