DOC AIRBUS | AMM A320FLifting for Aircraft Maintenance Operations
TASK 07-11-00-581-001-A
Lifting for Aircraft Maintenance Operations
To lift the aircraft for maintenance operations.
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 07-11-00-941-050-A
[Rev.10 from 2021]
2026.03.31 22:52:45 UTC
Lifting for Aircraft Maintenance Operations
WARNING:
BEFORE YOU LIFT THE AIRCRAFT WITH JACKS, MAKE SURE THAT THE WEIGHT OF THE FUEL IS EQUAL ON THE TWO SIDES OF THE AIRCRAFT CENTERLINE.
WARNING:
MAKE SURE THAT THE AIRCRAFT IS STABLE:
- BEFORE YOU PUT IT ON JACKS
- DURING ALL THE TIME IT STAYS ON JACKS.
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:
WHEN YOU DO THE LEVELING/LIFTING OR LOWERING OF THE AIRCRAFT, MAKE SURE THAT:
- YOU USE THE CORRECT LIFTING/LOWERING EQUIPMENT FOR THE CONDITIONS
- THE PERSONS WHO OPERATE THE LIFTING/LOWERING EQUIPMENT HAVE THE CORRECT TRAINING AND KNOWLEDGE
- THE NECESSARY SAFETY AREA IS IDENTIFIED
- THERE ARE NO UNWANTED PERSONS OR EQUIPMENT IN THIS AREA
- THERE IS NO WORK IN PROGRESS ON THE AIRCRAFT.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
YOU MUST NOT LIFT THE AIRCRAFT WITH THE SAFETY STAY.
CAUTION:
DO NOT USE THE TAIL SAFETY STAY WHEN THE AIRCRAFT IS ON ITS WHEELS.
1. Reason for the JobTo lift the aircraft for maintenance operations.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE |
| No specific | AR | ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE |
| No specific | AR | CHOCK - WHEEL(S) |
| No specific | 1 | JACK - FORWARD FUSELAGE |
| No specific | AR | JACK - SAFETY STAY |
| No specific | 1 | JACK - WING |
| 98D07103000000 | 1 | DYNAMOMETER-SAFETY STAY |
| 98D07103001000 | 1 | GLOBAL JACKING SA |
| 98D07103500000 | 1 | JACK ADAPTER-FUSELAGE |
| 98D07104000000 | 1 | JACKING PAD SET |
| 98D07104000001 | 1 | JACKING PAD SET |
| 98D07104081000 | 1 | JACKING PAD SET |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.03HBD9) | Synthetic Ester base Grease-General Purpose Low Temp - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 311AL |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 05-57-00-200-001-A | Aircraft Stability |
| TASK 05-57-00-200-001-B | Aircraft Stability |
| TASK 05-57-00-200-001-C | Aircraft Stability |
| TASK 07-11-00-581-003-A | Lifting of the Aircraft at the Forward Jacking Point, MLG Wheels on the Ground |
| TASK 08-21-00-200-001-A | Quick Leveling Using the Attitude Monitor |
| TASK 08-21-00-200-001-A-01 | Quick Leveling with a Spirit Level in the FWD Cargo Compartment |
| TASK 08-21-00-200-001-A-02 | Quick Leveling Procedure with the ADIRU |
| TASK 08-21-00-200-001-A-03 | Quick Leveling with a Spirit Level in the Passenger Compartment |
| TASK 32-00-00-481-001-A | Installation of the Safety Devices on the Landing Gears |
| 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 |
Subtask 07-11-00-941-050-A
A. Safety Precautions
(1) Before the lifting operation, identify a safety area.
(3) Install the CHOCK - WHEEL(S) at the wheels of the main landing gear.
Subtask 07-11-00-582-055-A ** ON A/C NOT FOR ALL (1) Before the lifting operation, identify a safety area.
NOTE: Local safety regulations can contain additional rules and information applicable to safety areas.
(2) Make sure that the safety devices are installed on the landing gears (Ref. AMM TASK 32-00-00-481-001). (3) Install the CHOCK - WHEEL(S) at the wheels of the main landing gear.
B. General Information for Jacking
(1) Selection of the jacks and the safety stay:
Jacking point heights are minimum values, you must use these values to select jacks for the necessary aircraft configuration.
You must lift the aircraft at three points on the structure with three hydraulic jacks:
You must not use the safety stay to lift the aircraft.
You can lift the aircraft with jacks when the tires and the shock absorbers are deflated.
You can lift the aircraft at the forward jacking point only, with the wheels of the MLG on the ground (Ref. AMM TASK 07-11-00-581-003).
The jack load capacity must be higher than the maximum permitted structural load given in the below step "Reaction at the jacking points and the safety stay".
(a) Maximum aircraft weight:
The maximum permitted aircraft weight for the jacking is 59000 kg (130073 lb).
(b) Maximum fitting load:
Make sure that you do not apply more than the permitted load at each jacking point and at the safety stay fitting:
Subtask 07-11-00-582-055-B ** ON A/C NOT FOR ALL (1) Selection of the jacks and the safety stay:
Jacking point heights are minimum values, you must use these values to select jacks for the necessary aircraft configuration.
You must lift the aircraft at three points on the structure with three hydraulic jacks:
- One point is below the forward fuselage at FR8,
- The two other points are below the wings at RIB9.
You must not use the safety stay to lift the aircraft.
You can lift the aircraft with jacks when the tires and the shock absorbers are deflated.
You can lift the aircraft at the forward jacking point only, with the wheels of the MLG on the ground (Ref. AMM TASK 07-11-00-581-003).
The jack load capacity must be higher than the maximum permitted structural load given in the below step "Reaction at the jacking points and the safety stay".
CAUTION:
MAKE SURE THAT THE LOAD ON THE JACKS IS NOT MORE THAN THE MAXIMUM LOAD SPECIFIED IN THIS PROCEDURE.
CAUTION:
MAKE SURE THAT THE WEIGHT OF THE AIRCRAFT IS NOT MORE THAN THE MAXIMUM WEIGHT SPECIFIED IN THIS PROCEDURE.
CAUTION:
WHEN YOU LIFT THE AIRCRAFT ON JACKS OUTDOORS, MAKE SURE THAT YOU OBEY THE JACK OVERLOAD LIMIT IN WIND CONDITIONS. IF YOU DO NOT OBEY THIS LIMIT, DAMAGE TO THE AIRCRAFT STRUCTURE AND/OR THE JACKS CAN OCCUR.
(2) Reaction at the jacking points and the safety stay:(a) Maximum aircraft weight:
The maximum permitted aircraft weight for the jacking is 59000 kg (130073 lb).
(b) Maximum fitting load:
Make sure that you do not apply more than the permitted load at each jacking point and at the safety stay fitting:
- The permitted load at the forward jacking point, at FR8 is 6800 daN (15287 lbf).
- The permitted load at the wing jacking points, at RIB9 is 28500 daN (64071 lbf).
- The permitted load at the safety stay point, between FR73 and FR74 is 2000 daN (4496 lbf).
- The load on the fittings must be measured by the load cells installed between the jacks and the fittings.
- The load on the safety stay must be measured by the 98D07103000000 DYNAMOMETER-SAFETY STAY between the safety stay and the fitting.
NOTE: The load cells and the 98D07103000000 DYNAMOMETER-SAFETY STAY installation procedure is given in the drawing 98D07103001000 GLOBAL JACKING SA.
B. General Information for Jacking
(1) Selection of the jacks and the safety stay:
Jacking point heights are minimum values, you must use these values to select jacks for the necessary aircraft configuration.
You must lift the aircraft at three points on the structure with three hydraulic jacks:
You must not use the safety stay to lift the aircraft.
You can lift the aircraft with jacks when the tires and the shock absorbers are deflated.
You can lift the aircraft at the forward jacking point only, with the wheels of the MLG on the ground (Ref. AMM TASK 07-11-00-581-003).
The jack load capacity must be higher than the maximum permitted structural load given in the below step "Reaction at the jacking points and the safety stay".
(a) Maximum aircraft weight:
The maximum permitted aircraft weight for jacking is 69000 kg (152119 lb).
(b) Maximum fitting load:
Make sure that you do not apply more than the permitted load at each jacking point and at the safety stay fitting:
Subtask 07-11-00-582-055-C ** ON A/C NOT FOR ALL (1) Selection of the jacks and the safety stay:
Jacking point heights are minimum values, you must use these values to select jacks for the necessary aircraft configuration.
You must lift the aircraft at three points on the structure with three hydraulic jacks:
- One point is below the forward fuselage at FR8,
- The two other points are below the wings at RIB9.
You must not use the safety stay to lift the aircraft.
You can lift the aircraft with jacks when the tires and the shock absorbers are deflated.
You can lift the aircraft at the forward jacking point only, with the wheels of the MLG on the ground (Ref. AMM TASK 07-11-00-581-003).
The jack load capacity must be higher than the maximum permitted structural load given in the below step "Reaction at the jacking points and the safety stay".
CAUTION:
MAKE SURE THAT THE LOAD ON THE JACKS IS NOT MORE THAN THE MAXIMUM LOAD SPECIFIED IN THIS PROCEDURE.
CAUTION:
MAKE SURE THAT THE WEIGHT OF THE AIRCRAFT IS NOT MORE THAN THE MAXIMUM WEIGHT SPECIFIED IN THIS PROCEDURE.
CAUTION:
WHEN YOU LIFT THE AIRCRAFT ON JACKS OUTDOORS, MAKE SURE THAT YOU OBEY THE JACK OVERLOAD LIMIT IN WIND CONDITIONS. IF YOU DO NOT OBEY THIS LIMIT, DAMAGE TO THE AIRCRAFT STRUCTURE AND/OR THE JACKS CAN OCCUR.
(2) Reaction at the jacking points and the safety stay:(a) Maximum aircraft weight:
The maximum permitted aircraft weight for jacking is 69000 kg (152119 lb).
(b) Maximum fitting load:
Make sure that you do not apply more than the permitted load at each jacking point and at the safety stay fitting:
- The permitted load at the forward jacking point, at FR8 is 6800 daN (15287 lbf).
- The permitted load at the wing jacking points, at RIB9 is 33400 daN (75086 lbf).
- The permitted load at the safety stay point, between FR73 and FR74 is 2000 daN (4496 lbf).
- The load on the fittings must be measured by the load cells installed between the jacks and the fittings.
- The load on the safety stay must be measured by the 98D07103000000 DYNAMOMETER-SAFETY STAY between the safety stay and the fitting.
NOTE: The load cells and the 98D07103000000 DYNAMOMETER-SAFETY STAY installation procedure is given in the drawing 98D07103001000 GLOBAL JACKING SA.
B. General Information for Jacking
(1) Selection of the jacks and the safety stay:
Jacking point heights are minimum values, you must use these values to select jacks for the necessary aircraft configuration.
You must lift the aircraft at three points on the structure with three hydraulic jacks:
You must not use the safety stay to lift the aircraft.
You can lift the aircraft with jacks when the tires and the shock absorbers are deflated.
You can lift the aircraft at the forward jacking point only, with the wheels of the MLG on the ground (Ref. AMM TASK 07-11-00-581-003).
The jack load capacity must be higher than the maximum permitted structural load given in the below step "Reaction at the jacking points and the safety stay".
(a) Maximum aircraft weight:
The maximum permitted aircraft weight for the jacking is 57000 kg (125663 lb).
(b) Maximum fitting load:
Make sure that you do not apply more than the permitted load at each jacking point and at the safety stay fitting:
Subtask 07-11-00-869-050-A (1) Selection of the jacks and the safety stay:
Jacking point heights are minimum values, you must use these values to select jacks for the necessary aircraft configuration.
You must lift the aircraft at three points on the structure with three hydraulic jacks:
- One point is below the forward fuselage at FR8,
- The two other points are below the wings at RIB9.
You must not use the safety stay to lift the aircraft.
You can lift the aircraft with jacks when the tires and the shock absorbers are deflated.
You can lift the aircraft at the forward jacking point only, with the wheels of the MLG on the ground (Ref. AMM TASK 07-11-00-581-003).
The jack load capacity must be higher than the maximum permitted structural load given in the below step "Reaction at the jacking points and the safety stay".
CAUTION:
MAKE SURE THAT THE LOAD ON THE JACKS IS NOT MORE THAN THE MAXIMUM LOAD SPECIFIED IN THIS PROCEDURE.
CAUTION:
MAKE SURE THAT THE WEIGHT OF THE AIRCRAFT IS NOT MORE THAN THE MAXIMUM WEIGHT SPECIFIED IN THIS PROCEDURE.
CAUTION:
WHEN YOU LIFT THE AIRCRAFT ON JACKS OUTDOORS, MAKE SURE THAT YOU OBEY THE JACK OVERLOAD LIMIT IN WIND CONDITIONS. IF YOU DO NOT OBEY THIS LIMIT, DAMAGE TO THE AIRCRAFT STRUCTURE AND/OR THE JACKS CAN OCCUR.
(2) Reaction at the jacking points and the safety stay:(a) Maximum aircraft weight:
The maximum permitted aircraft weight for the jacking is 57000 kg (125663 lb).
(b) Maximum fitting load:
Make sure that you do not apply more than the permitted load at each jacking point and at the safety stay fitting:
- The permitted load at the forward jacking point, at FR8 is 6800 daN (15287 lbf).
- The permitted load at the wing jacking points, at RIB9 is 28500 daN (64071 lbf).
- The permitted load at the safety stay point, between FR73 and FR74 is 2000 daN (4496 lbf).
- The load on the fittings must be measured by the load cells installed between the jacks and the fittings.
- The load on the safety stay must be measured by the 98D07103000000 DYNAMOMETER-SAFETY STAY between the safety stay and the fitting.
NOTE: The load cells and the 98D07103000000 DYNAMOMETER-SAFETY STAY installation procedure is given in the drawing 98D07103001000 GLOBAL JACKING SA.
C. Aircraft Configuration
(1) Make sure that the aircraft is stable (Ref. AMM TASK 05-57-00-200-001).
(2) Apply the Flight Configuration Precautions (Ref. AMM TASK 32-00-00-860-001).
Subtask 07-11-00-010-050-A (1) Make sure that the aircraft is stable (Ref. AMM TASK 05-57-00-200-001).
(2) Apply the Flight Configuration Precautions (Ref. AMM TASK 32-00-00-860-001).
D. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at RIB9 under each wing. Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position between FR73 and FR74.
(2) Open the access door 311AL.
Subtask 07-11-00-820-050-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at RIB9 under each wing. Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position between FR73 and FR74.
(2) Open the access door 311AL.
E. Installation of Specific Tools
(1) At the forward jacking point:
(a) Examine the 98D07103500000 JACK ADAPTER-FUSELAGE (1) and make sure that there is no damage.
(b) Install the 98D07103500000 JACK ADAPTER-FUSELAGE (1) at FR8.
(c) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the ball of the 98D07103500000 JACK ADAPTER-FUSELAGE (1).
(d) Put the JACK - FORWARD FUSELAGE in the vertical position below the jacking point.
(e) Fully extend the jack threaded rods.
(2) At the wing jacking point:
(a) Remove the plugs to install the dowels (3).
(b) Examine the 98D07104000000 JACKING PAD SET (2) and make sure that there is no damage.
(c) Install the 98D07104000000 JACKING PAD SET (2) at RIB9.
(d) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the receptacle of the 98D07104000000 JACKING PAD SET (2).
(3) At the safety stay:
(a) Examine the 98D07103000000 DYNAMOMETER-SAFETY STAY and make sure that there is no damage.
(b) Install the 98D07103000000 DYNAMOMETER-SAFETY STAY on the safety stay.
(4) For the typical installation of the nose jack, the adapters and the load cells, refer to the drawing 98D07103001000 GLOBAL JACKING SA.
This drawing shows the Airbus recommended installation.
Subtask 07-11-00-820-050-B ** ON A/C NOT FOR ALL (1) At the forward jacking point:
(a) Examine the 98D07103500000 JACK ADAPTER-FUSELAGE (1) and make sure that there is no damage.
(b) Install the 98D07103500000 JACK ADAPTER-FUSELAGE (1) at FR8.
(c) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the ball of the 98D07103500000 JACK ADAPTER-FUSELAGE (1).
(d) Put the JACK - FORWARD FUSELAGE in the vertical position below the jacking point.
(e) Fully extend the jack threaded rods.
(2) At the wing jacking point:
(a) Remove the plugs to install the dowels (3).
(b) Examine the 98D07104000000 JACKING PAD SET (2) and make sure that there is no damage.
(c) Install the 98D07104000000 JACKING PAD SET (2) at RIB9.
(d) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the receptacle of the 98D07104000000 JACKING PAD SET (2).
(3) At the safety stay:
(a) Examine the 98D07103000000 DYNAMOMETER-SAFETY STAY and make sure that there is no damage.
(b) Install the 98D07103000000 DYNAMOMETER-SAFETY STAY on the safety stay.
(4) For the typical installation of the nose jack, the adapters and the load cells, refer to the drawing 98D07103001000 GLOBAL JACKING SA.
This drawing shows the Airbus recommended installation.
E. Installation of Specific Tools
(1) At the forward jacking point:
(a) Examine the 98D07103500000 JACK ADAPTER-FUSELAGE (1) and make sure that there is no damage.
(b) Install the 98D07103500000 JACK ADAPTER-FUSELAGE (1) at FR8.
(c) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the ball of the 98D07103500000 JACK ADAPTER-FUSELAGE (1).
(d) Put the JACK - FORWARD FUSELAGE in the vertical position below the jacking point.
(e) Fully extend the jack threaded rods.
(2) At the wing jacking point:
(a) Remove the plugs to install the dowels (3).
(b) Examine the 98D07104081000 JACKING PAD SET (2) and make sure that there is no damage.
(c) Install the 98D07104081000 JACKING PAD SET (2) at RIB9.
(d) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the receptacle of the 98D07104081000 JACKING PAD SET (2).
(3) At the safety stay:
(a) Examine the 98D07103000000 DYNAMOMETER-SAFETY STAY and make sure that there is no damage.
(b) Install the 98D07103000000 DYNAMOMETER-SAFETY STAY on the safety stay.
(4) For the typical installation of the nose jack, the adapters and the load cells, refer to the drawing 98D07103001000 GLOBAL JACKING SA.
This drawing shows the Airbus recommended installation.
Subtask 07-11-00-820-050-E ** ON A/C NOT FOR ALL (1) At the forward jacking point:
(a) Examine the 98D07103500000 JACK ADAPTER-FUSELAGE (1) and make sure that there is no damage.
(b) Install the 98D07103500000 JACK ADAPTER-FUSELAGE (1) at FR8.
(c) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the ball of the 98D07103500000 JACK ADAPTER-FUSELAGE (1).
(d) Put the JACK - FORWARD FUSELAGE in the vertical position below the jacking point.
(e) Fully extend the jack threaded rods.
(2) At the wing jacking point:
(a) Remove the plugs to install the dowels (3).
(b) Examine the 98D07104081000 JACKING PAD SET (2) and make sure that there is no damage.
(c) Install the 98D07104081000 JACKING PAD SET (2) at RIB9.
(d) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the receptacle of the 98D07104081000 JACKING PAD SET (2).
(3) At the safety stay:
(a) Examine the 98D07103000000 DYNAMOMETER-SAFETY STAY and make sure that there is no damage.
(b) Install the 98D07103000000 DYNAMOMETER-SAFETY STAY on the safety stay.
(4) For the typical installation of the nose jack, the adapters and the load cells, refer to the drawing 98D07103001000 GLOBAL JACKING SA.
This drawing shows the Airbus recommended installation.
E. Installation of Specific Tools
(1) At the forward jacking point:
(a) Examine the 98D07103500000 JACK ADAPTER-FUSELAGE (1) and make sure that there is no damage.
(b) Install the 98D07103500000 JACK ADAPTER-FUSELAGE (1) at FR8.
(c) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the ball of the 98D07103500000 JACK ADAPTER-FUSELAGE (1).
(d) Put the JACK - FORWARD FUSELAGE in the vertical position below the jacking point.
(e) Fully extend the jack threaded rods.
(2) At the wing jacking point:
(a) Remove the plugs to install the dowels (3).
(b) Examine the 98D07104000001 JACKING PAD SET (2) and make sure that there is no damage.
(c) Install the 98D07104000001 JACKING PAD SET (2) at RIB9.
(d) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the receptacle of the 98D07104000001 JACKING PAD SET (2).
(3) At the safety stay:
(a) Examine the 98D07103000000 DYNAMOMETER-SAFETY STAY and make sure that there is no damage.
(b) Install the 98D07103000000 DYNAMOMETER-SAFETY STAY on the safety stay.
(4) For the typical installation of the nose jack, the adapters and the load cells, refer to the drawing 98D07103001000 GLOBAL JACKING SA.
This drawing shows the Airbus recommended installation.
Subtask 07-11-00-080-054-A (1) At the forward jacking point:
(a) Examine the 98D07103500000 JACK ADAPTER-FUSELAGE (1) and make sure that there is no damage.
(b) Install the 98D07103500000 JACK ADAPTER-FUSELAGE (1) at FR8.
(c) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the ball of the 98D07103500000 JACK ADAPTER-FUSELAGE (1).
(d) Put the JACK - FORWARD FUSELAGE in the vertical position below the jacking point.
(e) Fully extend the jack threaded rods.
(2) At the wing jacking point:
(a) Remove the plugs to install the dowels (3).
(b) Examine the 98D07104000001 JACKING PAD SET (2) and make sure that there is no damage.
(c) Install the 98D07104000001 JACKING PAD SET (2) at RIB9.
(d) Apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the receptacle of the 98D07104000001 JACKING PAD SET (2).
(3) At the safety stay:
(a) Examine the 98D07103000000 DYNAMOMETER-SAFETY STAY and make sure that there is no damage.
(b) Install the 98D07103000000 DYNAMOMETER-SAFETY STAY on the safety stay.
(4) For the typical installation of the nose jack, the adapters and the load cells, refer to the drawing 98D07103001000 GLOBAL JACKING SA.
This drawing shows the Airbus recommended installation.
F. Remove the CHOCK - WHEEL(S).
Subtask 07-11-00-869-052-A G. Aircraft Maintenance Configuration
(1) On the panel 110VU:
Subtask 07-11-00-942-050-A (1) On the panel 110VU:
- Set the PARKING BRK control switch to OFF.
H. Removal of Ground Support Equipment
(1) Make sure that the passenger/crew doors, the emergency exits and the cargo doors are closed and locked or fully open and locked.
(2) Remove the access platform(s).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
4. Procedure(1) Make sure that the passenger/crew doors, the emergency exits and the cargo doors are closed and locked or fully open and locked.
(2) Remove the access platform(s).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
WARNING:
WHEN YOU LIFT OR LOWER THE AIRCRAFT, ALWAYS KEEP IT IN A LEVEL ATTITUDE. INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT CAN OCCUR.
Subtask 07-11-00-581-050-A ** ON A/C NOT FOR ALL A. Aircraft Leveling
(1) Operate the lifting control of the nose jack to make the aircraft centerline horizontal.
(2) Make sure that the aircraft is level with:
Subtask 07-11-00-581-050-C ** ON A/C NOT FOR ALL (1) Operate the lifting control of the nose jack to make the aircraft centerline horizontal.
(2) Make sure that the aircraft is level with:
- The attitude monitor (Ref. AMM TASK 08-21-00-200-001) or
- A spirit level in the forward cargo compartment (Ref. AMM TASK 08-21-00-200-001) or
- A spirit level in the passenger compartment (Ref. AMM TASK 08-21-00-200-001) or
- The ADIRU (if installed) (Ref. AMM TASK 08-21-00-200-001).
A. Aircraft Leveling
(1) Operate the lifting control of the nose jack to make the aircraft centerline horizontal.
(2) Make sure that the aircraft is level with:
Subtask 07-11-00-581-051-A (1) Operate the lifting control of the nose jack to make the aircraft centerline horizontal.
(2) Make sure that the aircraft is level with:
- A spirit level in the forward cargo compartment (Ref. AMM TASK 08-21-00-200-001) or
- A spirit level in the passenger compartment (Ref. AMM TASK 08-21-00-200-001) or
- The ADIRU (if installed) (Ref. AMM TASK 08-21-00-200-001).
B. Aircraft Lifting
(1) Put the JACK - WING in position.
For the typical installation of the wing jacks, the adapters and the load cells, refer to the drawing 98D07103001000 GLOBAL JACKING SA.
This drawing shows the Airbus recommended installation.
(2) Slowly operate the controls of the nose and the two wing jacks to lift the aircraft at the same attitude.
Different Heights of the Jacking/Safety Points ** ON A/C NOT FOR ALL
Different Heights of the Jacking/Safety Points ** ON A/C NOT FOR ALL
Different Heights of the Jacking/Safety Points ** ON A/C NOT FOR ALL
(4) Make sure that the safety locknuts of the hydraulic jacks continue to touch the jack collars while you lift the aircraft.
(5) Installation of the safety stay
(a) Set the JACK - SAFETY STAY and put it in position between FR73 and FR74.
(c) Make sure that the safety locknuts of the safety jack touch the jack collars after the installation of the safety jack.
(1) Put the JACK - WING in position.
For the typical installation of the wing jacks, the adapters and the load cells, refer to the drawing 98D07103001000 GLOBAL JACKING SA.
This drawing shows the Airbus recommended installation.
(2) Slowly operate the controls of the nose and the two wing jacks to lift the aircraft at the same attitude.
NOTE: It is necessary to monitor the level attitude of the aircraft during all the jacking procedure.
(3) Continue to lift the aircraft until you get sufficient clearance to do the maintenance operation scheduled for the aircraft. Different Heights of the Jacking/Safety Points ** ON A/C NOT FOR ALL Different Heights of the Jacking/Safety Points ** ON A/C NOT FOR ALL Different Heights of the Jacking/Safety Points ** ON A/C NOT FOR ALL (5) Installation of the safety stay
(a) Set the JACK - SAFETY STAY and put it in position between FR73 and FR74.
NOTE: The installation of the safety stay is necessary to keep the aircraft stable during the maintenance operation.
(b) Operate the safety stay until it touches the safety point. (c) Make sure that the safety locknuts of the safety jack touch the jack collars after the installation of the safety jack.
CAUTION:
REMOVE THE SAFETY STAY BEFORE YOU DO THE LANDING GEAR EXTENSION AND RETRACTION TESTS. DAMAGE TO THE FUSELAGE CAN OCCUR IF THE AIRCRAFT MOVES DURING THE TESTS.
(6) If it is necessary to do the landing gear extension/retraction tests, make sure that you remove the safety stay before the tests. NOTE: The aircraft structure moves lightly during the extension/retraction test.
(7) Airbus recommends that you keep the safety area identified to prevent unwanted persons or equipment in the area.