DOC AIRBUS | AMM A320FRetraction of the Flaps/Slats on the Ground
TASK 27-50-00-866-009-A-01
Retraction of the Flaps/Slats on the Ground
To retract the flaps and slats at the same time
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 27-50-00-941-064-A
Subtask 27-50-00-866-062-A ** ON A/C NOT FOR ALL
Subtask 27-50-00-860-068-A
[Rev.10 from 2021]
2026.03.31 23:51:57 UTC
Retraction of the Flaps/Slats on the Ground
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
To retract the flaps and slats at the same time
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| 98D27803000000 | 1 | LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| 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 29-10-00-863-002-A | Pressurize the Yellow Hydraulic System with a Hydraulic Ground Power-Cart |
| TASK 29-10-00-863-003-A | Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart |
| TASK 29-10-00-863-003-A-01 | Pressurize the Blue Hydraulic System with the Blue Electric Pump |
| TASK 29-10-00-864-002-A | Depressurize the Yellow Hydraulic System |
| TASK 29-10-00-864-003-A | Depressurize the Blue Hydraulic System |
| TASK 29-23-00-860-001-A | Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU) |
| TASK 29-23-00-860-002-A | Connection of the Isolation Coupling of the Power Transfer Unit (PTU) |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 27-50-00-941-064-A
A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Put the WARNING NOTICE(S) in position to tell persons that the flap and slat systems are in operation.
(3) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is in position on the flap/slat control lever (Ref. AMM TASK 27-00-00-480-002).
Subtask 27-50-00-860-067-A (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Put the WARNING NOTICE(S) in position to tell persons that the flap and slat systems are in operation.
(3) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is in position on the flap/slat control lever (Ref. AMM TASK 27-00-00-480-002).
B. Aircraft Maintenance Configuration
(2) If applicable, disconnect the Power Transfer Unit (PTU) (Ref. AMM TASK 29-23-00-860-001).
(4) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
Subtask 27-50-00-865-072-A WARNING:
OBEY THE HYDRAULIC SAFETY PROCEDURES.
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002). (2) If applicable, disconnect the Power Transfer Unit (PTU) (Ref. AMM TASK 29-23-00-860-001).
NOTE: The flaps move at full-speed if the Power Transfer Unit (PTU) is in operation. If the PTU is disconnected (electrically or hydraulically), only the yellow flap motor operates and the flaps move at half-speed.
NOTE: An ECAM F/CTL FLAP SYS 1 FAULT message will show when the PTU is isolated. This message can be ignored.
(3) Pressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-863-002). (4) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
NOTE: The Blue and/or Green hydraulic system(s) operate(s) the slat system. If necessary, use the alternative hydraulic system.
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 27-50-00-865-070-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | B03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | H09 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/FAC2/26VAC | 14CC2 | M18 |
D. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B06 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| 49VU | FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 | 5CV | B01 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/WTB/FLP/SYS2 | 12CV | P20 |
| 121VU | FLIGHT CONTROLS/WTB/SLT/SYS2 | 11CV | P19 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/SLT/CTL/SYS2 | 7CV | R21 |
| 122VU | FLIGHT CONTROLS/WTB/FLP/SYS1 | 10CV | S07 |
| 122VU | FLIGHT CONTROLS/WTB/SLT/SYS1 | 9CV | S06 |
Subtask 27-50-00-866-062-A ** ON A/C NOT FOR ALL
A. Retraction of the Flaps/Slats on the Ground
(2) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (Ref. AMM TASK 27-00-00-080-002).
(3) Set the flap/slat control lever to the applicable position 3, 2, 1 or 0.
Subtask 27-50-00-866-062-B ** ON A/C NOT FOR ALL 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) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001). (2) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (Ref. AMM TASK 27-00-00-080-002).
(3) Set the flap/slat control lever to the applicable position 3, 2, 1 or 0.
NOTE: If the flaps/slats are in position 3, 2, or 1, do not close the circuit breakers 14CC1 and 14CC2. This is to prevent RTLU-backup function activation on ground and to prevent more RTLU stroke mechanical stop damage. If the flaps/slats are in position 0, you can close the circuit breakers 14CC1 and 14CC2.
(4) Make sure that on the ECAM upper DU, the flap and slat position bar moves to the set position. A. Retraction of the Flaps/Slats on the Ground
(2) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (Ref. AMM TASK 27-00-00-080-002).
(3) Set the flap/slat control lever to the applicable position 3, 2, 1 or 0.
5. Close-upWARNING:
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) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001). (2) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (Ref. AMM TASK 27-00-00-080-002).
(3) Set the flap/slat control lever to the applicable position 3, 2, 1 or 0.
NOTE: If the flaps/slats are in position 3, 2, or 1, do not close the circuit breakers 14CC1 and 14CC2. This is to prevent RTLU-backup function activation on ground and to prevent more RTLU stroke mechanical stop damage. If the flaps/slats are in position 0, you can close the circuit breakers 14CC1 and 14CC2.
(4) Make sure that on the ECAM upper DU, the flap and slat position bar moves to the set position. Subtask 27-50-00-860-068-A
A. Aircraft Maintenance Configuration
(1) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
(2) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(3) If applicable, connect the PTU (Ref. AMM TASK 29-23-00-860-002).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 27-50-00-865-073-A (1) Depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002).
(2) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(3) If applicable, connect the PTU (Ref. AMM TASK 29-23-00-860-002).
(4) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 27-50-00-942-064-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | B03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | H09 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/FAC2/26VAC | 14CC2 | M18 |
C. Removal of Equipment
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.