DOC AIRBUS | AMM A320FInstallation of the Proximity-Sensor of the Interconnecting Strut
TASK 27-51-44-400-002-A
Installation of the Proximity-Sensor of the Interconnecting Strut
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 27-51-44-941-062-A
Subtask 27-51-44-410-056-A
[Rev.10 from 2021]
2026.03.31 23:52:48 UTC
Installation of the Proximity-Sensor of the Interconnecting Strut
WARNING:
MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
1. Reason for the Job- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE |
| No specific | AR | CAP - BLANKING |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| 98D27504031000 | 1 | PIN-SETTING |
| 98D27803000000 | 1 | LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 580 | LEFT WING FLAPS AND SPOILERS |
| 680 | RIGHT WING FLAPS AND SPOILERS |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 27-00-00-080-002-A | Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000) |
| TASK 27-00-00-480-002-A | Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000) |
| TASK 27-50-00-866-008-A | Extension of the Flaps on the Ground |
| TASK 27-50-00-866-008-A-01 | Extension of the Flaps/Slats on the Ground |
| TASK 27-51-00-710-002-A | Operational Test of the Flap Interconnecting Strut and the Flap-Attachment Failure-Detection Sensors |
| TASK 27-54-00-710-001-A | Operational Test of the Flap System |
| TASK 27-54-61-000-002-A | Removal of the Flap Kink-Seals and Cushion-Seals |
| TASK 27-54-61-400-006-A | Installation of the Flap Kink-Seals and Cushion-Seals |
| TASK 32-00-00-860-001-A | Flight Configuration Precautions with Electrical Power |
| TASK 32-00-00-860-001-A-01 | Flight Configuration Precautions without Electrical Power |
| TASK 32-00-00-860-002-A | Ground Configuration after Flight Configuration with Electrical Power |
| TASK 32-00-00-860-002-A-01 | Ground Configuration after Flight Configuration without Electrical Power |
Details of the Proximity-Sensors 37CV (38CV), 39CV (40CV)Subtask 27-51-44-941-062-A
A. Safety Precautions
(2) Make sure that the WARNING NOTICE(S) is in position to tell persons not to operate the flap/slat controls.
Subtask 27-51-44-860-061-A WARNING:
BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS AND ATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
(1) Make sure that the SAFETY BARRIER(S) are in position. (2) Make sure that the WARNING NOTICE(S) is in position to tell persons not to operate the flap/slat controls.
B. Aircraft Maintenance Configuration
(2) Make sure that the flaps are extended at position 1 (Ref. AMM TASK 27-50-00-866-008).
(3) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (Ref. AMM TASK 27-00-00-480-002) is on the flap/slat control lever.
(4) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is in position:
Subtask 27-51-44-869-053-A WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Make sure that the lower kink seal, the cushion seals and the upper kink seals are removed from the flaps (Ref. AMM TASK 27-54-61-000-002). (2) Make sure that the flaps are extended at position 1 (Ref. AMM TASK 27-50-00-866-008).
(3) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (Ref. AMM TASK 27-00-00-480-002) is on the flap/slat control lever.
(4) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is in position:
- For the left wing, below zone 580
- For the right wing, below zone 680.
C. Flight Configuration Precautions
(1) If you did not de-energize the aircraft electrical circuits, make sure that the flight configuration precautions are done (Ref. AMM TASK 32-00-00-860-001).
Subtask 27-51-44-865-071-A (1) If you did not de-energize the aircraft electrical circuits, make sure that the flight configuration precautions are done (Ref. AMM TASK 32-00-00-860-001).
D. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
Subtask 27-51-44-420-058-A - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
A. Preparation for Installation
(1) Clean the component interface and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 27-51-44-420-052-A ** ON A/C NOT FOR ALL (1) Clean the component interface and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
B. Installation of the Proximity Sensor
(1) Put the applicable proximity sensor (1) in position on the bracket (3) as follows:
(a) FOR [37CV] (SENSOR-L FLAP ATTACHMENT FAILURE DETECTION), [38CV] (SENSOR-R FLAP ATTACHMENT FAILURE DETECTION)
1 Install the bolts (5), washers (4) and nuts (2). Do not tighten the nuts (2).
(2) Put the applicable proximity sensor (14) in position on the bracket (8) as follows:
(a) FOR [39CV] (SENSOR-L FLAP ATTACHMENT FAILURE DETECTION), [40CV] (SENSOR-R FLAP ATTACHMENT FAILURE DETECTION)
1 Install the bolts (6), washers (7) and nuts (9). Do not tighten the nuts (9).
(3) Install the 98D27504031000 PIN-SETTING in the interconnecting strut (15).
(4) Make sure that dimension X is between 0.3 mm (0.012 in.) and 0.7 mm (0.028 in.).
(5) Tighten the applicable nuts (2) and (9).
(6) Make sure that dimension X has stayed correct.
(7) Remove CAP - BLANKING from the receptacles (10) and (13).
(8) Connect the applicable electrical connector (11) and (12).
(9) Remove the 98D27504031000 PIN-SETTING from the interconnecting strut (15).
(10) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the slat/flap control lever (Ref. AMM TASK 27-00-00-080-002).
(11) Remove the access platform(s).
Subtask 27-51-44-420-052-B ** ON A/C NOT FOR ALL (1) Put the applicable proximity sensor (1) in position on the bracket (3) as follows:
(a) FOR [37CV] (SENSOR-L FLAP ATTACHMENT FAILURE DETECTION), [38CV] (SENSOR-R FLAP ATTACHMENT FAILURE DETECTION)
1 Install the bolts (5), washers (4) and nuts (2). Do not tighten the nuts (2).
(2) Put the applicable proximity sensor (14) in position on the bracket (8) as follows:
(a) FOR [39CV] (SENSOR-L FLAP ATTACHMENT FAILURE DETECTION), [40CV] (SENSOR-R FLAP ATTACHMENT FAILURE DETECTION)
1 Install the bolts (6), washers (7) and nuts (9). Do not tighten the nuts (9).
(3) Install the 98D27504031000 PIN-SETTING in the interconnecting strut (15).
(4) Make sure that dimension X is between 0.3 mm (0.012 in.) and 0.7 mm (0.028 in.).
(5) Tighten the applicable nuts (2) and (9).
(6) Make sure that dimension X has stayed correct.
(7) Remove CAP - BLANKING from the receptacles (10) and (13).
(8) Connect the applicable electrical connector (11) and (12).
(9) Remove the 98D27504031000 PIN-SETTING from the interconnecting strut (15).
(10) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the slat/flap control lever (Ref. AMM TASK 27-00-00-080-002).
(11) Remove the access platform(s).
B. Installation of the Proximity Sensor
(1) Put the applicable proximity sensor (15) in position on the bracket (2) as follows:
(a) FOR [37CV] (SENSOR-L FLAP ATTACHMENT FAILURE DETECTION), [38CV] (SENSOR-R FLAP ATTACHMENT FAILURE DETECTION)
1 Install the bolts (4), washers (3) and nuts (1). Do not tighten the nuts (1).
(2) Put the applicable proximity sensor (13) in position on the bracket (7) as follows:
(a) FOR [39CV] (SENSOR-L FLAP ATTACHMENT FAILURE DETECTION), [40CV] (SENSOR-R FLAP ATTACHMENT FAILURE DETECTION)
1 Install the bolts (5), washers (6) and nuts (10). Do not tighten the nuts (10).
(3) Install the 98D27504031000 PIN-SETTING in the interconnecting strut (14).
(4) Make sure that dimension "X" is between 0.3 mm (0.012 in.) and 0.7 mm (0.028 in.).
(5) Tighten the applicable nuts (1) and (10).
(6) Make sure that dimension "X" has stayed correct.
(7) Remove the blanking cap from the receptacles (8) and (9).
(8) Connect the applicable electrical connector (11) and (12).
(9) Remove the 98D27504031000 PIN-SETTING from the interconnecting strut (14).
(10) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the slat/flap control lever (Ref. AMM TASK 27-00-00-080-002).
(11) Remove the access platform(s).
Subtask 27-51-44-865-072-A (1) Put the applicable proximity sensor (15) in position on the bracket (2) as follows:
(a) FOR [37CV] (SENSOR-L FLAP ATTACHMENT FAILURE DETECTION), [38CV] (SENSOR-R FLAP ATTACHMENT FAILURE DETECTION)
1 Install the bolts (4), washers (3) and nuts (1). Do not tighten the nuts (1).
(2) Put the applicable proximity sensor (13) in position on the bracket (7) as follows:
(a) FOR [39CV] (SENSOR-L FLAP ATTACHMENT FAILURE DETECTION), [40CV] (SENSOR-R FLAP ATTACHMENT FAILURE DETECTION)
1 Install the bolts (5), washers (6) and nuts (10). Do not tighten the nuts (10).
(3) Install the 98D27504031000 PIN-SETTING in the interconnecting strut (14).
(4) Make sure that dimension "X" is between 0.3 mm (0.012 in.) and 0.7 mm (0.028 in.).
(5) Tighten the applicable nuts (1) and (10).
(6) Make sure that dimension "X" has stayed correct.
(7) Remove the blanking cap from the receptacles (8) and (9).
(8) Connect the applicable electrical connector (11) and (12).
(9) Remove the 98D27504031000 PIN-SETTING from the interconnecting strut (14).
(10) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the slat/flap control lever (Ref. AMM TASK 27-00-00-080-002).
(11) Remove the access platform(s).
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 27-51-44-869-054-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
D. Ground Configuration
(1) If you did the flight configuration precautions, put the aircraft back to the ground configuration (Ref. AMM TASK 32-00-00-860-002).
Subtask 27-51-44-710-054-A (1) If you did the flight configuration precautions, put the aircraft back to the ground configuration (Ref. AMM TASK 32-00-00-860-002).
E. Test
(1) Do the operational test of the failure detection sensors for the flap attachment (Ref. AMM TASK 27-51-00-710-002).
(2) Do an operational test of the flap system (Ref. AMM TASK 27-54-00-710-001).
5. Close-up(1) Do the operational test of the failure detection sensors for the flap attachment (Ref. AMM TASK 27-51-00-710-002).
(2) Do an operational test of the flap system (Ref. AMM TASK 27-54-00-710-001).
Subtask 27-51-44-410-056-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the lower kink seal, the cushion seals and the upper kink seals from the flaps (Ref. AMM TASK 27-54-61-400-006).
Subtask 27-51-44-942-055-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the lower kink seal, the cushion seals and the upper kink seals from the flaps (Ref. AMM TASK 27-54-61-400-006).
B. Removal of Equipment
(1) Remove the safety barriers.
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the safety barriers.
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.