DOC AIRBUS | AMM A320FExtension of the Flaps/Slats on the Ground
TASK 27-50-00-866-008-A-01
Extension of the Flaps/Slats on the Ground
To extend 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 27-50-00-941-063-A
Subtask 27-50-00-866-061-A ** ON A/C NOT FOR ALL
Subtask 27-50-00-860-066-A
[Rev.10 from 2021]
2026.03.31 23:51:53 UTC
Extension 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 extend 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 | SAFETY CLIP - CIRCUIT BREAKER |
| 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 27-00-00-480-002-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 27-50-00-941-063-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.
Subtask 27-50-00-860-065-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.
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 27-50-00-865-069-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) closed:
Subtask 27-50-00-865-071-A | 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 |
D. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| 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 |
Subtask 27-50-00-866-061-A ** ON A/C NOT FOR ALL
A. Extension of the Flaps/Slats on the Ground
(2) Set the flap/slat control lever to the applicable position 1, 2, 3 or FULL.
(3) Make sure that on the ECAM upper DU:
Subtask 27-50-00-866-061-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.
CAUTION:
IF THE THRUST REVERSER COWLS ARE OPEN, MAKE SURE THAT THE HALF DOORS OF THE THRUST REVERSER ARE CLOSED BEFORE YOU EXTEND THE SLATS. IF THE DOORS ARE OPEN, YOU CAN CAUSE DAMAGE TO THE SLATS AND HALF DOORS WHEN THE SLATS EXTEND.
(1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001). (2) Set the flap/slat control lever to the applicable position 1, 2, 3 or FULL.
(3) Make sure that on the ECAM upper DU:
- the flap position bar moves to the set position
- the slat position bar moves to the set position.
A. Extension of the Flaps/Slats on the Ground
(2) Set the flap/slat control lever to the applicable position 1, 2, 3 or FULL.
(3) Make sure that on the ECAM upper DU:
Subtask 27-50-00-866-061-C ** 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) Set the flap/slat control lever to the applicable position 1, 2, 3 or FULL.
(3) Make sure that on the ECAM upper DU:
- the flap position bar moves to the set position
- the slat position bar moves to the set position.
A. Extension of the Flaps/Slats on the Ground
(2) Set the flap/slat control lever to the applicable position 1, 2, 3 or FULL.
(3) Make sure that on the ECAM upper DU:
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.
CAUTION:
DO NOT EXTEND THE SLATS WHEN THE FAN COWLS AND THE THRUST REVERSER COWLS ARE OPEN. IF YOU DO THIS, DAMAGE TO THE AIRCRAFT CAN OCCUR.
(1) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001). (2) Set the flap/slat control lever to the applicable position 1, 2, 3 or FULL.
(3) Make sure that on the ECAM upper DU:
- the flap position bar moves to the set position
- the slat position bar moves to the set position.
Subtask 27-50-00-860-066-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 27-50-00-942-063-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. 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.