Inspection after a Tire Burst or Tread Throw or Wheel Failure

TASK 05-51-15-200-001-A
Inspection after a Tire Burst or Tread Throw or Wheel Failure

WARNING: LET THE BRAKES AND THE WHEELS BECOME COOL BEFORE YOU GO NEAR THE LANDING GEAR. DO NOT APPLY A LIQUID OR GAS DIRECTLY ON A HOT WHEEL OR BRAKE UNIT. THIS CAN CAUSE A TIRE EXPLOSION AND/OR A WHEEL RIM BURST.

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 3M (10 FT)
No specific	AR	ACCESS PLATFORM 5M (16 FT)
No specific	AR	WARNING NOTICE(S)

B. Referenced Information

REFERENCE	DESIGNATION
TASK 05-51-16-200-001-A	Inspection After Brake Emergency Application or Overheat
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 27-14-00-710-001-A	Operational Test of the Aileron and Hydraulic Actuation
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 27-54-00-710-001-A	Operational Test of the Flap System
TASK 27-60-00-866-002-A	Extension-Retraction of the Spoilers for Maintenance
TASK 27-64-00-710-001-A	Operational Test of the Spoiler Hydraulic Actuation
TASK 27-80-00-866-004-A	Extending the Slats on the Ground
TASK 27-84-00-710-001-A	Operational Test of the Slat System
TASK 28-10-00-910-002-A	Access to the Fuel Tanks and the Work Areas
TASK 28-25-00-650-001-A	Pressure Defuel
TASK 29-00-00-864-001-A	Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 32-00-00-481-001-A	Installation of the Safety Devices on the Landing Gears
TASK 32-11-00-200-001-A	General Visual Inspection of the Main Landing Gear
TASK 32-12-00-010-001-A	Open the Main Gear Doors for Access
TASK 32-12-00-410-001-A	Close the Main Gear Doors after Access
TASK 32-21-00-200-002-A	General Visual Inspection of the Nose Landing Gear
TASK 32-22-00-010-001-A	Nose Gear Doors - Ground Doors Opening
TASK 32-22-00-410-001-A	Nose Gear Doors - Ground Doors Closing
TASK 32-30-00-867-001-A	Retraction of the Landing Gears for Maintenance
TASK 32-30-00-867-002-A	Extension of the Landing Gears after Maintenance
TASK 32-41-00-210-003-A	Functional Check of Tire Pressures
TASK 32-41-11-000-006-A	Removal of the MLG Wheel
TASK 32-41-11-400-006-A	Installation of the MLG Wheel
TASK 32-41-12-000-001-A	Removal of the NLG Wheel
TASK 32-41-12-400-001-A	Installation of the NLG Wheel
TASK 71-13-00-010-802-A	Opening of the Fan Cowl Doors
TASK 71-13-00-200-010-A	Detailed Inspection of the Fan Cowl Doors
TASK 71-13-11-200-804-A	Visual Inspection of the Fan Cowl Doors
TASK 71-13-11-200-804-C	Visual Inspection of Fan Cowl Doors
TASK 72-00-00-200-001-A	Inspection/Check of Foreign Object Damage (FOD) (Bird Strike Included)
TASK 72-00-00-200-006-A	Inspection/Check of Foreign Object Damage (FOD) (Bird Strike Included)
TASK 72-00-00-200-010-A	Inspection of the Engine after Bird Strike, Foreign Object or Slush Ingestion
TASK 72-00-00-210-807-A	Visual Examination (After Bird Strike (Foreign Object Damage))
TASK 78-31-00-710-040-A	Operational Test of the Thrust Reverser System
TASK 78-31-00-710-040-A-01	Operational Test of the Thrust Reverser without CFDS - Engine not Running
TASK 78-31-00-710-040-A-02	Operational Test of the Thrust Reverser without CFDS - Engine Running
TASK 78-31-00-710-041-A	Operational Test of the Thrust Reverser System with the CFDS
TASK 78-31-00-710-041-A-02	Operational test of the Thrust Reverser without the CFDS and Engine Running
TASK 78-31-00-710-042-A	Operational Test of the Thrust Reverser System
TASK 78-31-00-710-805-A	Operational Test of Thrust Reverser with MCDU
TASK 78-31-00-710-805-A-01	Thrust Reverser Cycling Test (Engine Running)
TSM 05-50-00-810-804	Tire Burst or Tread Throw or Wheel Failure or Flat Spot
TSM 05-50-00-810-825	Brake Emergency Application or Overheat
Tire-Failure Reporting Sheet

3. Job Set-up
Subtask 05-51-15-481-050-A

A. Safety Precautions
(1) Make sure that the safety devices are installed on the landing gears (Ref. AMM TASK 32-00-00-481-001).

Subtask 05-51-15-010-050-A

B. Get Access
(1) Open the main gear doors and install the safety devices (Ref. AMM TASK 32-12-00-010-001).
(2) Open the nose gear doors and install the safety devices (Ref. AMM TASK 32-22-00-010-001).

Subtask 05-51-15-866-050-A

C. Extension of the Flight Control Surfaces
(1) Fully extend the flaps and the slats (Ref. AMM TASK 27-50-00-866-008), (Ref. AMM TASK 27-80-00-866-004).
(2) Extend the spoilers (Ref. AMM TASK 27-60-00-866-002).

Subtask 05-51-15-860-050-A

D. Aircraft Maintenance Configuration
(1) Make sure that the hydraulic systems are depressurized (Ref. AMM TASK 29-00-00-864-001).
(2) Make sure that the electrical circuits are de-energized (Ref. AMM TASK 24-41-00-862-002).
(3) Put the WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the systems.
(4) Put the ACCESS PLATFORM 3M (10 FT) in position.

4. Procedure
Subtask 05-51-15-210-051-A

A. General

NOTE: All the necessary inspections are visual unless the text gives other instructions.
Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.

(1) Before you do all inspections given in this task. Refer to TSM 05-50-00-810-804 and TSM 05-50-00-810-825 to make sure that the hydraulic and electrical connections are correctly connected.
(2) Inspection recommendations for composite parts
(a) If you find damage (signs of impact, damaged paintwork, abrasion, scratches or dents) on a composite part, you must do an inspection of the related damaged area for delamination and internal damage.
(3) If there is damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM gives the approved damage limits and repair procedures.
(4) If you replace a component because of an inspection, you must do an operational test of the related system.
(5) If a tire burst occurs when the landing gear is fully retracted, then only examine the items of equipment that follow:

The landing gear well
The landing gear doors
The landing gear assemblies
The hydraulic bay compartment.

(6) If a tire burst occurs because of emergency operation of the brakes or locking of the brakes, do an inspection (Ref. AMM TASK 05-51-16-200-001).
(7) If there is a tire failure in service, the operator must record the applicable data on the tire-failure reporting sheet and send it to Airbus.

Tire-Failure Reporting Sheet

(8) General wheel inspection
(a) Before you do inspection of the wheel, refer to TSM 05-50-00-810-804.
(b) After a tire burst:

Replace the damaged wheel
Deflate and replace the adjacent wheel.

NOTE: After a tread throw, it is possible that the tire will stay inflated.

1 If the tire is inflated when the aircraft is parked, let the tire become cool for three hours before you measure the pressure.
2 If the measured pressure is more than 80% of the nominal pressure (refer to the pressure tables), deflate and then replace the damaged wheel.

For Main-Landing-Gear (MLG) wheel removal (Ref. AMM TASK 32-41-11-000-006).
For MLG wheel installation (Ref. AMM TASK 32-41-11-400-006).
For Nose-Landing-Gear (NLG) wheel removal (Ref. AMM TASK 32-41-12-000-001).
For NLG wheel installation (Ref. AMM TASK 32-41-12-400-001).

3 If the measured pressure is less than or equal to 80% of the nominal pressure (refer to the pressure tables), deflate and then replace the damaged wheel and the adjacent wheel.

For MLG wheel removal (Ref. AMM TASK 32-41-11-000-006).
For MLG wheel installation (Ref. AMM TASK 32-41-11-400-006).
For NLG wheel removal (Ref. AMM TASK 32-41-12-000-001).
For NLG wheel installation (Ref. AMM TASK 32-41-12-400-001).

Subtask 05-51-15-210-055-A

B. Inspection of the Fuselage (FR1 to FR34)

NOTE: All the necessary inspections are visual unless the text gives other instructions.
Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Fuselage Lower Surface. This includes the cargo doors.
A.	Examine the skin panels for distortion, pulled or torn fasteners and damaged paintwork. If you find damage:	X
	(1) Remove the floor panels of the avionics and/or forward cargo compartment and examine: - The frames - The stringers - The cleats - The fittings for distortion, cracks, pulled or torn fasteners and damaged paintwork adjacent to the damaged area.		X
	(2) Examine: - The components - The pipes - The ducts - The electrical looms - The control cables - The pulleys - The mounts for cracks, rupture and fluid leakage. Also examine the condition of the safety devices.		X

Subtask 05-51-15-210-056-A

C. Inspection of the NLG and the NLG Well

ITEM	INSPECTION TASKS	PHASE 1
1.	Inspection of the Nose-Landing-Gear (NLG)
A.	Do a general visual inspection of the NLG assembly for: - Cracks - Damage - Distortion.	X
	Examine the paint and protective finishes (this includes the chromium plating on the sliding tube) for: - Cracks - Chips - Damaged paintwork (Ref. AMM TASK 32-21-00-200-002).
B.	Do a general visual inspection of the equipment and dressings on the NLG to examine: - The downlock and retraction actuators - The components (this includes the steering system components and the actuators, the valves and the manifolds) - The hydraulic pipes, hoses and hose guides - The electrical harnesses and equipment (this includes the proximity sensors, the lights and the antenna).	X
	Do a check for: - Damage, distortion - Fluid leaks - Damaged paintwork and/or surface treatments - Correct and safe attachment.
2.	Inspection of the Nose-Landing-Gear Doors and Well
A.	Do a general visual inspection of the honeycomb structure of the forward and aft doors and the leg door for: - Delamination - Core damage - Cracks - Pulled or torn fasteners - Dents - Scratches - Damaged paintwork.	X
B.	Do a general visual inspection of: - The door hinges and actuators - The actuator attachment fittings - The hydraulic hoses and pipes - The electrical harnesses and equipment (this includes the proximity sensors).	X
	Do a check for: - Fluid leakage - Distortion - Damage - Damaged paintwork.
C.	Do a general visual inspection of the structure of the nose-landing-gear well. Examine the protective panels and the structure for: - Distortion - Cracks - Pulled or torn fasteners - Honeycomb delamination - Core damage.	X
D.	Do a general visual inspection of the equipment in the NLG well to examine: - The components, the valves and the manifolds - The hydraulic pipes and hoses - The electrical harnesses and equipment - The control cables, rods and pulleys - The transmission systems - The safety devices.	X
	Do a check for: - Damage - Distortion - Fluid leaks - Correct and safe attachment.

Subtask 05-51-15-210-052-A

D. Inspection of the Fuselage (FR35 to FR50)

NOTE: All the necessary inspections are visual unless the text gives other instructions.
Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Belly Fairing
A.	Examine the belly fairing panels for holes, delamination, cracked or flaking paint and loose fasteners. Make sure that the panels are correctly attached. If you find damage:	X
	(1) Remove the panels and internally examine the belly fairing structure for buckling, cracks and damaged paintwork.		X
	(2) Examine: - The pipes - The ducts - The electrical looms - The mounts for fluid leakage, distortion, rupture, breaks and cracks. Make sure that the components are correctly attached and examine the condition of the safety devices.		X

Subtask 05-51-15-210-057-A

E. Inspection of the MLG and the MLG Well

ITEM	INSPECTION TASKS	PHASE 1
1.	Inspection of the MLG
A.	Do a general visual inspection of the applicable MLG assembly for: - Cracks - Damage - Distortion.	X
	Examine the paint and protective finishes (this includes the chromium plating on the sliding tube) for: - Cracks - Chips - Damaged paintwork (Ref. AMM TASK 32-11-00-200-001).
B.	Do a general visual inspection of the equipment and dressings on the MLG to examine: - The downlock and retraction actuators - The components, the valves and the manifolds - The hydraulic pipes, hoses and hose guides - The electrical harnesses and equipment (this includes the proximity sensors).	X
	Do a check for: - Damage - Distortion - Fluid leakage - Damaged paintwork and/or surface treatments - Correct and safe attachment.
2.	Inspection of the MLG Doors and Well
A.	Do a general visual inspection of the honeycomb structure of the MLG doors and the fixed and hinged fairings for: - Delamination - Core damage - Cracks - Pulled or torn fasteners - Dents - Scratches - Damaged paintwork.	X
B.	Do a general visual inspection of: - The door hinges and actuators - The actuator attachment fittings - The hydraulic hoses and pipes - The electrical harnesses and equipment (this includes the proximity sensors).	X
	Do a check for: - Fluid leakage - Distortion - Damage - Damaged paintwork.
C.	Do a general visual inspection of the structure of the MLG well. Examine the protective panels and the structure for: - Distortion - Cracks - Pulled or torn fasteners - Honeycomb delamination - Core damage.	X
D.	Do a general visual inspection of the equipment in the MLG well to examine: - The components, the valves and the manifolds - The hydraulic pipes and hoses - The electrical harnesses and equipment - The control cables, rods and pulleys - The transmission systems - The safety devices.	X
	Do a check for: - Damage - Distortion - Fluid leakage - Correct and safe attachment.

Subtask 05-51-15-210-053-B ** ON A/C NOT FOR ALL

F. Inspection of the Nacelles, Engines and Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Nacelles and Engine
A.	Externally examine the nacelle and the primary nozzle for distortion, cracks, delamination, cracked or flaking paint, loose rivets and signs of shearing. If you find damage:	X
	(1) Open the cowls and internally examine them for distortion, cracks, pulled or torn fasteners and damaged paintwork (Ref. AMM TASK 71-13-11-200-804).		X
	(2) Examine the components, the ducts, the cables and the looms in the cowls for distortion, cracks and rupture.		X
B.	If the tire burst occurred during thrust reverser operation, do a functional test of the thrust reverser system (refer to the Test paragraph). Make sure that the travel is full and that the related controls do not catch or become blocked. Internally examine the doors for damage.	X
2.	Engines	X
A.	Examine the engines for possible foreign object damage (Ref. AMM TASK 72-00-00-200-001).	X
3.	Pylons
A.	Externally examine the pylons for distortion, cracks, pulled or torn fasteners and damaged paintwork. If you find damage:	X
	(1) Internally examine the structure for distortion, cracks, pulled or torn fasteners and damaged paintwork.		X
	(2) Examine the components, the pipes, the ducts, the looms, the cables, the pulleys and the mounts for distortion, cracks, rupture and fluid leakage.		X

Subtask 05-51-15-210-053-C ** ON A/C NOT FOR ALL

F. Inspection of the Nacelles, the Engines and the Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Nacelles and Engine
A.	Externally examine the nacelle and the primary nozzle for distortion, cracks, delamination, cracked or flaking paint, loose rivets and signs of shearing. If you find damage:	X
	(1) Open the cowls and internally examine them for distortion, cracks, pulled or torn fasteners and damaged paintwork (Ref. AMM TASK 71-13-00-200-010).		X
	(2) Examine the components, the ducts, the cables and the looms in the cowls for distortion, cracks and rupture.		X
B.	If the tire burst occurred during thrust reverser operation, do a functional test of the thrust reverser system (refer to the Test paragraph). Make sure that the travel is full and that the related controls do not catch or become blocked. Internally examine the doors for damage.	X
2.	Engines
A.	Examine the engines for possible foreign object damage (Ref. AMM TASK 72-00-00-200-010).	X
3.	Pylons
A.	Externally examine the pylons for distortion, cracks, pulled or torn fasteners and damaged paintwork. If you find damage:	X
	(1) Internally examine the structure for distortion, cracks, pulled or torn fasteners and damaged paintwork.		X
	(2) Examine the components, the pipes, the ducts, the looms, the cables, the pulleys and the mounts for distortion, cracks, rupture and fluid leakage.		X

Subtask 05-51-15-210-053-D ** ON A/C NOT FOR ALL

F. Inspection of the Nacelles, the Engines and the Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Nacelles and Engine
A.	Externally examine the nacelle and the primary nozzle for distortion, cracks, delamination, cracked or flaking paint, loose rivets and signs of shearing. If you find damage:	X
	(1) Open the cowls and internally examine them for distortion, cracks, pulled or torn fasteners and damaged paintwork (Ref. AMM TASK 71-13-11-200-804).		X
	(2) Examine the components, the ducts, the cables and the looms in the cowls for distortion, cracks and rupture.		X
B.	If the tire burst occurred during thrust reverser operation, do a functional test of the thrust reverser system (refer to the Test paragraph). Make sure that the travel is full and that the related controls do not catch or become blocked. Internally examine the doors for damage.	X
2.	Engines	X
A.	Examine the engines for possible foreign object damage (Ref. AMM TASK 72-00-00-200-006).
3.	Pylons
A.	Externally examine the pylons for distortion, cracks, pulled or torn fasteners and damaged paintwork. If you find damage:	X
	(1) Internally examine the structure for distortion, cracks, pulled or torn fasteners and damaged paintwork.		X
	(2) Examine the components, the pipes, the ducts, the looms, the cables, the pulleys and the mounts for distortion, cracks, rupture and fluid leakage.		X

Subtask 05-51-15-210-053-G ** ON A/C NOT FOR ALL

F. Inspection of the Nacelles, the Engines and the Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Nacelles and Engine
A.	Externally examine the nacelle and the primary nozzle for distortion, cracks, delamination, cracked or flaking paint, loose rivets and signs of shearing. If you find damage:	X
	(1) Open the cowls and internally examine them for distortion, cracks, pulled or torn fasteners and damaged paintwork (Ref. AMM TASK 71-13-00-010-802).		X
	(2) Examine the components, the ducts, the cables and the looms in the cowls for distortion, cracks and rupture.		X
B.	If the tire burst occurred during thrust reverser operation, do a functional test of the thrust reverser system (refer to the Test paragraph). Make sure that the travel is full and that the related controls do not catch or become blocked. Internally examine the doors for damage.	X
2.	Engines	X
A.	Examine the engines for possible foreign object damage (Ref. AMM TASK 72-00-00-210-807).	X
3.	Pylons
A.	Externally examine the pylons for distortion, cracks, pulled or torn fasteners and damaged paintwork. If you find damage:	X
	(1) Internally examine the structure for distortion, cracks, pulled or torn fasteners and damaged paintwork.		X
	(2) Examine the components, the pipes, the ducts, the looms, the cables, the pulleys and the mounts for distortion, cracks, rupture and fluid leakage.		X

Subtask 05-51-15-210-054-A

G. Inspection of the Wings

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Skin panels
A.	Examine the skin panels, specially on the bottom surface of the wings, for: - Damage to the paint - Distortion - Cracks - Tears - Fuel leaks. If you find damage or fuel leaks:	X
	(1) Defuel the tanks (Ref. AMM TASK 28-25-00-650-001).		X
	(2) Get access to the wing tanks (Ref. AMM TASK 28-10-00-910-002).
	(3) Examine the front and rear spars, the internal structure and the fasteners for distortion, cracks and pulled fasteners. Make sure that the condition of the sealant beads is good.		X
	(4) Examine the ducts, the cables, the electrical looms, the pipes, the mechanical linkages and their installations for damage, distortion, cracks and fluid leakage. Make sure that the components are correctly attached.		X
	(5) Close access to the wing tanks (Ref. AMM TASK 28-10-00-910-002).
2.	Flaps and Slats
A.	Examine the slats, the flaps, and the fairings for distortion, cracks or pulled fasteners and signs of impact.	X
3.	Ailerons
A.	Examine the ailerons for: - Damaged paintwork - Distortion - Cracks - Pulled fasteners - Signs of impact. If you find damage: (1) Examine the hinges and the actuators for damage, distortion and cracks.	X

Subtask 05-51-15-210-059-A

H. Inspection of the Trimmable Horizontal Stabilizer

NOTE: All the necessary inspections are visual unless the text gives other instructions.
Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures.

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the THS skin
A.	From the ground, examine the lower skin for distortion, cracks, pulled or torn fasteners, damaged paintwork and rubber marks. If you find damage:	X
	(1) Put the ACCESS PLATFORM 5M (16 FT) in position.		X
	(2) Examine the THS for distortion, cracks, pulled or torn fasteners, damaged paintwork and rubber marks: - At the lower skin, - At the upper skin, - At the leading edge.		X

Subtask 05-51-15-410-050-A

I. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the panels and the doors that you opened for the inspection.
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).
(5) Close the main doors of the main gear (Ref. AMM TASK 32-12-00-410-001).
(6) Close the doors of the nose gear (Ref. AMM TASK 32-22-00-410-001).

Subtask 05-51-15-710-050-B ** ON A/C NOT FOR ALL

J. Operational Test of the Systems

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
	NOTE : The subsequent tests are applicable only if the inspection showed damage to a flight control surface, the landing gears or doors or the adjacent structure.
A.	Do an operational test of the thrust reverser system as specified in the inspection procedure (Ref. AMM TASK 78-31-00-710-040).	X
B.	Do an operational test of the aileron. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-14-00-710-001).		X
C.	Do an operational test of the flaps and the slats. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-54-00-710-001) (Ref. AMM TASK 27-84-00-710-001).		X
D.	Do an operational test of the spoilers. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-64-00-710-001).		X
E.	Do a retraction test of the landing gear. Make sure that the travel is smooth and that the related controls do not catch or become blocked (Ref. AMM TASK 32-30-00-867-001) (Ref. AMM TASK 32-30-00-867-002).		X

Subtask 05-51-15-710-050-C ** ON A/C NOT FOR ALL

J. Operational Test of the Systems

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
	NOTE : The subsequent tests are applicable only if the inspection showed damage to a flight control surface, the landing gears or doors or the adjacent structure.
A.	Do an operational test of the thrust reverser system as specified in the inspection procedure (Ref. AMM TASK 78-31-00-710-041).	X
B.	Do an operational test of the aileron. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-14-00-710-001).		X
C.	Do an operational test of the flaps and the slats. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-54-00-710-001) (Ref. AMM TASK 27-84-00-710-001).		X
D.	Do an operational test of the spoilers. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-64-00-710-001).		X
E.	Do a retraction test of the landing gear. Make sure that the travel is smooth and that the related controls do not catch or become blocked (Ref. AMM TASK 32-30-00-867-001) (Ref. AMM TASK 32-30-00-867-002).		X

Subtask 05-51-15-710-050-D ** ON A/C NOT FOR ALL

J. Operational Test of the Systems

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
	NOTE : The subsequent tests are only applicable if the inspection showed damage to a flight control surface, the landing gears or doors or the adjacent structure.
A.	Do an operational test of the thrust reverser system as specified in the inspection procedure (Ref. AMM TASK 78-31-00-710-042).	X
B.	Do an operational test of the aileron. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-14-00-710-001).		X
C.	Do an operational test of the flaps and the slats. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-54-00-710-001) (Ref. AMM TASK 27-84-00-710-001).		X
D.	Do an operational test of the spoilers. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-64-00-710-001).		X
E.	Do a retraction test of the landing gear. Make sure that the travel is smooth and that the related controls do not catch or become blocked (Ref. AMM TASK 32-30-00-867-001) (Ref. AMM TASK 32-30-00-867-002).		X

Subtask 05-51-15-710-050-G ** ON A/C NOT FOR ALL

J. Operational Test of the Systems

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
	NOTE : The subsequent tests are only applicable if the inspection showed damage to a flight control surface, the landing gears or doors or the adjacent structure.
A.	Do an operational test of the thrust reverser system as specified in the inspection procedure (Ref. AMM TASK 78-31-00-710-805).	X
B.	Do an operational test of the aileron. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-14-00-710-001).		X
C.	Do an operational test of the flaps and the slats. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-54-00-710-001) (Ref. AMM TASK 27-84-00-710-001).		X
D.	Do an operational test of the spoilers. Make sure that the travel is full and that the related controls do not catch or become blocked (Ref. AMM TASK 27-64-00-710-001).		X
E.	Do a retraction test of the landing gear. Make sure that the travel is smooth and that the related controls do not catch or become blocked (Ref. AMM TASK 32-30-00-867-001) (Ref. AMM TASK 32-30-00-867-002).		X

[Rev.10 from 2021] 2026.04.01 04:02:37 UTC