Inspection of the Aircraft after a Hail Strike in Flight

TASK 05-51-14-200-802-A
Inspection of the Aircraft after a Hail Strike in Flight

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:

THE FLIGHT CONTROLS
THE FLIGHT CONTROL SURFACES
THE LANDING GEAR AND THE RELATED DOORS
COMPONENTS THAT MOVE.

MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.

WARNING: BE CAREFUL WHEN YOU DO WORK ON THE PROBES ON THE GROUND. THE PROBES CAN STAY HOT FOR A LONG TIME AND WILL BURN YOU.

WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AND THE ADJACENT COMPONENTS AFTER ENGINE SHUTDOWN. THE ENGINE, THE ENGINE OIL AND THE ADJACENT COMPONENTS CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.

WARNING: BEFORE YOU DO WORK ON OR NEAR THE ENGINES, PUT A WARNING NOTICE IN THE COCKPIT. THIS WARNING NOTICE MUST TELL PERSONS NOT TO START THE ENGINES DURING THE PROCEDURE. IF THE ENGINES START WHILE YOU ARE NEAR THEM, THE SUCTION CAN PULL YOU INTO OR AGAINST THE AIR INTAKE. THIS CAN KILL YOU OR CAUSE INJURY TO YOU.

CAUTION: BEFORE YOU DO WORK ON AN EXTERNAL SURFACE OF THE AIRCRAFT, MAKE SURE THAT THIS SURFACE HAS A CORRECT PROTECTION. IF THE PROTECTION IS NOT CORRECT, YOU CAN CAUSE DAMAGE TO THE SURFACE.

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE
No specific	AR	DEVICE - SAFETY
No specific	1	LIGHT SOURCE - WHITE
No specific	1	MIRROR - INSPECTION, FLEXIBLE
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	WARNING NOTICE(S)

B. Referenced Information

REFERENCE	DESIGNATION
TASK 23-61-41-000-001-A	Removal of the Static Discharger
TASK 23-61-41-400-001-A	Installation of the Static Discharger
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 27-14-00-710-001-A	Operational Test of the Aileron and Hydraulic Actuation
TASK 27-24-00-710-002-A	Operational Test of the Rudder Servocontrols with Individual Hydraulic System
TASK 27-34-00-710-001-A	Operational Test of the Elevator and Hydraulic Actuation
TASK 27-44-00-710-001-A	Operational Test of the Jamming Protection Device of the Trimmable Horizontal Stabilizer Actuator
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 27-50-00-866-009-A	Retraction of the Flaps on the Ground
TASK 27-50-00-866-009-A-01	Retraction 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 27-80-00-866-005-A	Retracting the Slats on the Ground
TASK 27-84-00-710-001-A	Operational Test of the Slat System
TASK 29-00-00-864-001-A	Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
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 29-10-00-864-001-A	Depressurize the Green Hydraulic System
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 29-23-00-863-001-A	Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
TASK 29-24-00-863-001-A	Pressurize the Yellow Hydraulic System with the Electric Pump
TASK 30-81-21-000-001-A	Removal of the Lighted Icing Indicator
TASK 30-81-21-400-001-A	Installation of the Lighted Icing Indicator
TASK 30-81-31-000-001-A	Removal of the Ice Detector
TASK 30-81-31-400-001-A	Installation of the Ice Detector
TASK 32-00-00-081-001-A	Removal of the Safety Devices from the Landing Gears
TASK 32-00-00-481-001-A	Installation of the Safety Devices on the Landing Gears
TASK 32-00-00-481-002-A	Installation of the Safety Devices on the Landing Gear Doors
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 33-41-00-710-001-A	Operational Test of the Navigation Lights
TASK 33-42-00-040-001-A	Deactivation of the Landing Lights
TASK 33-42-11-000-001-A	Removal of the Landing Light
TASK 33-42-11-400-003-A	Installation of the Landing Light
TASK 33-48-00-710-002-A	Operational Test of the Anti-Collision/Strobe Lighting
TASK 34-11-15-000-001-A	Removal of the Pitot Probe
TASK 34-11-15-400-001-A	Installation of the Pitot Probe
TASK 34-11-16-000-001-A	Removal of the Static Probe
TASK 34-11-16-400-002-A	Installation of the Static Probe
TASK 34-11-18-000-001-A	Removal of the TAT Sensor
TASK 34-11-18-400-001-A	Installation of the TAT Sensor
TASK 34-11-19-000-001-A	Removal of the Angle of Attack (AOA) Sensor
TASK 34-11-19-400-001-A	Installation of the Angle of Attack (AOA) Sensor
TASK 34-13-00-200-001-A	Visual Check of Pitot probes, Static ports, AOA and TAT sensors
TASK 34-36-00-710-003-A	Operational Test of the ILS
TASK 34-36-00-710-009-A	Operational Test of the ILS
TASK 34-36-00-720-002-A	Functional Test of the ILS
TASK 34-36-00-720-006-A	Functional Test of the ILS
TASK 34-41-11-000-004-A	Removal of the Weather-Radar Antenna Assembly
TASK 34-41-11-000-012-A	Removal of the Weather-Radar Antenna Assembly
TASK 34-41-11-000-802-A	Removal of the Weather-Radar Antenna Assembly
TASK 34-41-11-400-005-A	Installation of the Weather-Radar Antenna Assembly
TASK 34-41-11-400-014-A	Installation of the Weather-Radar Antenna Assembly
TASK 34-41-11-400-802-A	Installation of the Weather-Radar Antenna Assembly
TASK 36-11-00-200-002-A	Inspection of the Bleed Air Cold Flow Path after Hail and Bird Strike
TASK 36-11-00-200-802-A	Inspection of the Bleed Air Cold Flow Path After Hail and Bird Strike
TASK 53-15-11-010-001-A	Opening of the Radome
TASK 53-15-11-200-001-A	Detailed Inspection of the Radome
TASK 53-15-11-200-001-A-01	Detailed Inspection of the Radome
TASK 53-15-11-410-001-A	Closing of the Radome
TASK 56-21-13-200-001-A	Detailed Inspection of Cabin Window Panes, including Window Panes in Doors
TASK 57-31-23-000-801-A	Removal of the Sharklet
TASK 57-31-23-400-801-A	Installation of the Sharklet
TASK 57-37-13-000-801-A	Removal of the Navigation-Light Glazing Panel
TASK 57-37-13-000-802-A	Removal of the Strobe-Light Glazing Panel
TASK 57-37-13-400-801-A	Installation of the Navigation-Light Glazing Panel
TASK 57-37-13-400-802-A	Installation of the Strobe-Light Glazing Panel
TASK 71-13-00-010-010-A	Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-010-040-A	Opening of the Fan Cowl Doors
TASK 71-13-00-010-040-B	Opening of the Fan Cowl Doors
TASK 71-13-00-010-802-A	Opening of the Fan Cowl Doors
TASK 71-13-00-410-010-A	Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-040-A	Closing of the Fan Cowl Doors
TASK 71-13-00-410-040-B	Closing of the Fan Cowl Doors
TASK 71-13-00-410-802-A	Closing of the 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 78-32-00-010-010-A	Opening of the Thrust Reverser Halves
TASK 78-32-00-410-010-A	Closing of the Thrust Reverser Halves
TASK 78-36-00-010-040-A	Opening of the Thrust Reverser Doors
TASK 78-36-00-010-040-B	Opening of the Thrust Reverser Doors
TASK 78-36-00-010-802-A	Opening of the Thrust Reverser Cowl-Doors
TASK 78-36-00-410-040-A	Closing of the Thrust Reverser Doors
TASK 78-36-00-410-040-B	Closing of the Thrust Reverser Doors
TASK 78-36-00-410-802-A	Closing of the Thrust Reverser Cowl-Doors
NTM 511003
SRM 573123
Area of the Tap Test Inspection of the Radome after a Hail Strike during the Flight ** ON A/C NOT FOR ALL
Area of the Tap Test Inspection of the Radome after a Hail Strike during the Flight ** ON A/C NOT FOR ALL

3. Job Set-up
Subtask 05-51-14-210-062-A

A. Inspection Preparation
(1) Before you start, we recommend that you get information from the crew about the flight conditions:

Engine behavior
Navigation and radio system behavior
Aircraft configuration (position of the landing gears and flight controls)
Flight phase at the time of the impact.

(2) Make sure that you have the related aircraft Post-Flight Report (PFR).
(3) You must do a check of all the events reported by the crew or by the PFR in addition/conjunction with this inspection.

Subtask 05-51-14-481-052-A

B. Safety Precautions
(1) Make sure that the DEVICE - SAFETY are installed on the landing gears (Ref. AMM TASK 32-00-00-481-001).
(2) Put the WARNING NOTICE(S) in the cockpit to tell persons not to operate the systems.
(3) Put the ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE in position.

Subtask 05-51-14-010-052-A

C. Get Access
(1) Open the Main Landing Gear (MLG) doors (Ref. AMM TASK 32-12-00-010-001).
(2) Install the safety devices on the MLG doors (Ref. AMM TASK 32-00-00-481-002).
(3) Open the Nose Landing Gear (NLG) doors (Ref. AMM TASK 32-22-00-010-001).
(4) Install the safety devices on the NLG doors (Ref. AMM TASK 32-00-00-481-002).

Subtask 05-51-14-866-054-A

D. Extension of the Flight Control Surfaces
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Pressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-10-00-863-003), (Ref. AMM TASK 29-23-00-863-001) and (Ref. AMM TASK 29-24-00-863-001).
(3) Fully extend the flaps and the slats (Ref. AMM TASK 27-50-00-866-008) and (Ref. AMM TASK 27-80-00-866-004).
(4) Extend the spoilers (Ref. AMM TASK 27-60-00-866-002).

Subtask 05-51-14-860-054-A

E. 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 aircraft electrical circuits are de-energized
(Ref. AMM TASK 24-41-00-862-002).

Subtask 05-51-14-865-054-A

WARNING: BEFORE YOU OPEN PHC CIRCUIT BREAKERS 2DA1(2,3), OPEN PROBE HEATER CIRCUIT-BREAKERS 1DA1(2), 3DA1(2,3), 4DA1(2,3) AND 5DA1(2,3). IF YOU DO NOT OBEY THIS SEQUENCE: - THE PROBES WILL BECOME TOO HOT. - THIS CAN CAUSE DAMAGE TO EQUIPMENT AND INJURY TO MAINTENANCE PERSONNEL.

F. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
121VU	COM NAV/RADAR/1	5SQ1	K13
** ON A/C NOT FOR ALL
121VU	COM NAV/RADAR/2	5SQ2	K14
** ON A/C ALL
FOR FIN: 9DA1 (PROBEPITOT, 1)
49VU	ANTI ICE/PROBES/AOA/1	4DA1	D04
49VU	ANTI ICE/PROBES/PITOT/1	3DA1	D02
122VU	ANTI ICE/PROBES/1/STATIC	5DA1	Z13
122VU	ANTI ICE/PROBES/1/TAT	1DA1	Z12
FOR FIN: 9DA2 (PROBEPITOT, 2)
122VU	ANTI ICE/PROBES/2/TAT	1DA2	Y15
122VU	ANTI ICE/PROBES/2/PITOT	3DA2	Y14
122VU	ANTI ICE/PROBES/2/AOA	4DA2	Y13
122VU	ANTI ICE/PROBES/2/STATIC	5DA2	Y11
FOR FIN: 9DA3 (PROBEPITOT, 3)
122VU	ANTI ICE/PROBES/3/PITOT	3DA3	Z16
122VU	ANTI ICE/PROBES/3/AOA	4DA3	Z15
122VU	ANTI ICE/PROBES/3/STATIC	5DA3	Z14
FOR FIN: 11FP1 (SENSORTAT, 1)
49VU	NAV PROBES/ADIRU1/115VAC	4FP1	F06
121VU	ADIRS/ADIRU/3/115VAC	4FP3	N05
FOR FIN: 11FP2 (SENSORTAT, 2)
121VU	ADIRS/ADIRU/2/115VAC	4FP2	N06
FOR FIN: 3FP1 (SENSORANGLE OF ATTACK, 1)
49VU	NAV PROBES/ADIRU 1/AND AOA 1/26VAC	5FP1	F07
121VU	ADIRS/ADIRU/3PWR/SWTG	9FP	N09
** ON A/C NOT FOR ALL
FOR FIN: 3FP2 (SENSORANGLE OF ATTACK, 2)
121VU	ADIRS/ADIRU/2PWR/SHED	10FP	N10
** ON A/C ALL
121VU	ADIRS/ADIRU/2/26VAC AND AOA	5FP2	N08
** ON A/C NOT FOR ALL
121VU	ADIRS/2PWR/SHED &/AOA2 MON	10FP	N10
** ON A/C ALL
FOR FIN: 3FP3 (SENSORANGLE OF ATTACK, 3)
121VU	ADIRS/ADIRU/3/26VAC AND AOA	5FP3	N07

Subtask 05-51-14-865-055-A

G. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
FOR FIN: 9DA1 (PROBEPITOT, 1)
49VU	ANTI ICE/PROBES/PHC/1	2DA1	D03
FOR FIN: 9DA2 (PROBEPITOT, 2)
122VU	ANTI ICE/PROBES/PHC/2	2DA2	Y12
FOR FIN: 9DA3 (PROBEPITOT, 3)
122VU	ANTI ICE/PROBES/PHC/3	2DA3	Y16

4. Procedure
Subtask 05-51-14-210-065-B ** ON A/C NOT FOR ALL

A. Inspection of the Nacelles, Engines and Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Nacelles
A.	Examine the nacelles externally for erosion, distortion, dents, delamination, cracked or flaking paint, loose rivets and signs of shearing. This includes: - The air intake - The fan cowls - The thrust reverser cowls.	X
B.	Examine the core nozzle for distortion, cracks, loose rivets and signs of shearing. If you find damage:	X
	(1) Open the fan cowls (Ref. AMM TASK 71-13-00-010-040).		X
	(2) Open the thrust reverser cowls (Ref. AMM TASK 78-36-00-010-040). Examine the cowls internally for signs of damage.		X
	(3) Examine the air-intake attach points on the fan case for: - Distortion, cracks and pulled or damaged fasteners.		X
	(4) Examine the core-nozzle attach points on the engine.		X
	(5) Examine all the cowl attach points on the pylon and all the cowl hinge fittings.		X
	(6) Examine all the cowl latches for damage and make sure that their operation is satisfactory.		X
2.	Inspection of the Engines
A.	If the fan cowls and the thrust reverser cowls are closed, open the fan cowls and the thrust reverser cowls (Ref. AMM TASK 71-13-00-010-040) and (Ref. AMM TASK 78-36-00-010-040) .	X
B.	Examine the engines for Foreign Object Damage (FOD) (Ref. AMM TASK 72-00-00-200-001).	X
	If you find damage or signs of hail strike and/or if the pilot gave a report of an engine stall, engine parameters change or smell in the cabin:
	(1) Do a visual inspection with a LIGHT SOURCE - WHITE and a MIRROR - INSPECTION, FLEXIBLE, for signs of hail strike impact or damage on: - The Fan Air Valve (FAV) scoop intake on the thrust reverser - The FAV intake on the thrust-reverser inner wall - The FAV intake on the bleed duct side - The ducting between the FAV and the firewall.		X
	(2) Do a visual inspection of: - The internal path side of the thrust reverser C-duct or - The inner wall of the thrust reverser (from the engine side). If you find signs of a hail strike or: - Cracks - Marks - Distortions, specially at the connection of the valve and the duct - Missing components, specially at the location of the tubes of the inlet flange and outlet flange of the FAV.		X
	(a) Do the inspection of the bleed-air cold flow-path after hail strike (Ref. AMM TASK 36-11-00-200-002).			X
C.	Close the thrust reverser and the fan cowls (Ref. AMM TASK 78-36-00-410-040) and (Ref. AMM TASK 71-13-00-410-040).	x
3.	Inspection of the Pylons
A.	Examine the pylons externally for erosion, distortion, dents, cracks, pulled or damaged fasteners and damaged paintwork. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the pylon internally for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- Examine all the components, pipes, ducts, electrical harnesses and their mounts for: . Distortion, cracks, rupture breaks and fluid leakage.		X

Subtask 05-51-14-210-065-C ** ON A/C NOT FOR ALL

A. Inspection of the Nacelles, Engines and Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Nacelles
A.	Examine the nacelles externally for erosion, distortion, dents, delamination, cracked or flaking paint, loose rivets and signs of shearing. This includes: - The air intake - The fan cowls - The thrust reverser cowls.	X
B.	Examine the core nozzle for distortion, cracks, loose rivets and signs of shearing. If you find damage:	X
	(1) Open the fan cowls (Ref. AMM TASK 71-13-00-010-010).		X
	(2) Open the thrust reverser cowls (Ref. AMM TASK 78-32-00-010-010). Examine the cowls internally for signs of damage.		X
	(3) Examine the air-intake attach points on the fan case for: - Distortion, cracks, pulled or damaged fasteners.		X
	(4) Examine the common-nozzle assembly attach points on the engine.		X
	(5) Examine all the cowl attach points on the pylon and all the cowl hinge fittings.		X
	(6) Examine all the cowl latches for damage and make sure that their operation is satisfactory.		X
2.	Inspection of the Engines
A.	If the fan cowls and the thrust reverser cowls are closed, open the fan cowls and the thrust reverser cowls (Ref. AMM TASK 71-13-00-010-010) and (Ref. AMM TASK 78-32-00-010-010) .	X
B.	Examine the engines for Foreign Object Damage (FOD) (Ref. AMM TASK 72-00-00-200-010).	X
	If you find damage or signs of hail strike and/or if the pilot gave a report of an engine stall, engine parameters change or smell in the cabin:
	(1) Do a visual inspection with a LIGHT SOURCE - WHITE and a MIRROR - INSPECTION, FLEXIBLE, for signs of hail strike impact or damage on: - The Fan Air Valve (FAV) scoop intake on the thrust reverser - The FAV intake on the thrust-reverser inner wall - The FAV intake on the bleed duct side - The ducting between the FAV and the firewall.		X
	(2) Do a visual inspection of: - The internal path side of the thrust reverser C-duct or - The inner wall of the thrust reverser (from the engine side). If you find signs of hail strike or: - Cracks - Marks - Distortions, specially at the connection of the valve and the duct - Missing components, specially at the location of the tubes of the inlet flange and outlet flange of the FAV.		X
	(a) Do the inspection of the bleed-air cold flow-path after hail strike (Ref. AMM TASK 36-11-00-200-002).			X
C.	Close the thrust reverser and the fan cowls (Ref. AMM TASK 78-32-00-410-010) and (Ref. AMM TASK 71-13-00-410-010).	X
3.	Inspection of the Pylons
A.	Examine the pylons externally for erosion, distortion, dents, cracks, pulled or damaged fasteners and damaged paintwork. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the pylon internally for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- Examine all the components, pipes, ducts, electrical harnesses and their mounts for: . Distortion, cracks, rupture breaks and fluid leakage.		X

Subtask 05-51-14-210-065-D ** ON A/C NOT FOR ALL

A. Inspection of the Nacelles, Engines and Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Nacelles
A.	Examine the nacelles externally for erosion, distortion, dents, delamination, cracked or flaking paint, loose rivets and signs of shearing. This includes: - The air intake - The fan cowls - The thrust reverser cowls.	X
B.	Examine the core nozzle for distortion, cracks, loose rivets and signs of shearing. If you find damage:	X
	(1) Open the fan cowls (Ref. AMM TASK 71-13-00-010-040).		X
	(2) Open the thrust reverser cowls (Ref. AMM TASK 78-36-00-010-040). Examine the cowls internally for signs of damage.		X
	(3) Examine the air-intake attach points on the fan case for: - Distortion, cracks, pulled or damaged fasteners.		X
	(4) Examine the core-nozzle attach points on the engine.		X
	(5) Examine all the cowl attach points on the pylon and all the cowl hinge fittings.		X
	(6) Examine all the cowl latches for damage and make sure that their operation is satisfactory.		X
2.	Inspection of the Engines
A.	If the fan cowls and the thrust reverser cowls are closed, open the fan cowls and the thrust reverser cowls (Ref. AMM TASK 71-13-00-010-040) and (Ref. AMM TASK 78-36-00-010-040) .	X
B.	Examine the engines for Foreign Object Damage (FOD) (Ref. AMM TASK 72-00-00-200-006).	X
	If you find damage or signs of hail strike and/or if the pilot gave a report of an engine stall, engine parameters change or smell in the cabin:
	(1) Do a visual inspection with a LIGHT SOURCE - WHITE and a MIRROR - INSPECTION, FLEXIBLE, for signs of hail strike impact or damage on: - The Fan Air Valve (FAV) scoop intake on the thrust reverser - The FAV intake on the thrust-reverser inner wall - The FAV intake on the bleed duct side - The ducting between the FAV and the firewall.		X
	(2) Do a visual inspection of: - The internal path side of the thrust reverser C-duct or - The inner wall of the thrust reverser (from the engine side). If you find signs of a hail strike or: - Cracks - Marks - Distortions, specially at the connection of the valve and the duct - Missing components, specially at the location of the tubes of the inlet flange and outlet flange of the FAV.		X
	(a) Do the inspection of the bleed-air cold flow-path after hail strike (Ref. AMM TASK 36-11-00-200-002).			X
C.	Close the thrust reverser and the fan cowls (Ref. AMM TASK 78-36-00-410-040) and (Ref. AMM TASK 71-13-00-410-040).	X
3.	Inspection of the Pylons
A.	Examine the pylons externally for erosion, distortion, dents, cracks, pulled or damaged fasteners and damaged paintwork. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the pylon internally for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- Examine all the components, pipes, ducts, electrical harnesses and their mounts for: . Distortion, cracks, rupture breaks and fluid leakage.		X

Subtask 05-51-14-210-065-F ** ON A/C NOT FOR ALL

A. Inspection of the Nacelles, Engines and Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Nacelles
A.	Examine the nacelles externally for erosion, distortion, dents, delamination, cracked or flaking paint, loose rivets and signs of shearing. This includes: - The air intake - The fan cowls - The thrust reverser cowls.	X
B.	Examine the core nozzle for distortion, cracks, loose rivets and signs of shearing. If you find damage:	X
	(1) Open the fan cowls (Ref. AMM TASK 71-13-00-010-802).		X
	(2) Open the thrust reverser cowls (Ref. AMM TASK 78-36-00-010-802). Examine the cowls internally for signs of damage.		X
	(3) Examine the air-intake attach points on the fan case for: - Distortion, cracks and pulled or damaged fasteners.		X
	(4) Examine the common-nozzle assembly attach points on the engine.		X
	(5) Examine all the cowl attach points on the pylon and all the cowl hinge fittings.		X
	(6) Examine all the cowl latches for damage and make sure that their operation is satisfactory.		X
2.	Inspection of the Engines
A.	If the fan cowls and the thrust reverser cowls are closed, open the fan cowls and the thrust reverser cowls (Ref. AMM TASK 71-13-00-010-802) and (Ref. AMM TASK 78-36-00-010-802) .	X
B.	Examine the engines for Foreign Object Damage (FOD) (Ref. AMM TASK 72-00-00-210-807).	X
	If you find damage or signs of hail strike and/or if the pilot gave a report of an engine stall, engine parameters change or smell in the cabin:
	(1) Do a visual inspection with a LIGHT SOURCE - WHITE and a MIRROR - INSPECTION, FLEXIBLE, for signs of hail strike impact or damage on: - The Fan Air Valve (FAV) scoop intake on the thrust reverser - The FAV intake on the thrust reverser inner wall - The FAV intake on the bleed duct side - The ducting between the FAV and the firewall.		X
	(2) Do a visual inspection of: - The internal path side of the thrust reverser C-duct or - The inner wall of the thrust reverser (from the engine side). If you find signs of a hail strike or: - Cracks - Marks - Distortions, specially at the connection of the valve and the duct - Missing components, specially at the location of the tubes of the inlet flange and outlet flange of the FAV.		X
	(a) Do the inspection of the bleed-air cold flow-path after hail strike (Ref. AMM TASK 36-11-00-200-802).			X
C.	Close the thrust reverser and the fan cowls (Ref. AMM TASK 78-36-00-410-802) and (Ref. AMM TASK 71-13-00-410-802).	X
3.	Inspection of the Pylons
A.	Examine the pylons externally for erosion, distortion, dents, cracks, pulled or torn fasteners and damaged paintwork. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the pylon internally for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- Examine all the components, pipes, ducts, electrical harnesses and their mounts for: . Distortion, cracks, rupture breaks and fluid leakage.		X

Subtask 05-51-14-869-052-A

B. 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) Inspection recommendations for composite parts:
(a) If you find damage (signs of impact, damaged paintwork, abrasions, scratches or dents) on a composite part, you must do an inspection of the damaged area for delamination and internal damage.
(2) If there is damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM contains the approved damage limits and repair procedures.
(3) You must systematically open and examine the radome. In some special conditions, the radome can have delamination without signs of impact.

Subtask 05-51-14-210-063-A ** ON A/C NOT FOR ALL

WARNING: BEFORE YOU DO A MAINTENANCE TASK NEAR THE RADOME (IN THE AREA OF 5 METERS/16.4 FT FROM THE WEATHER RADAR ANTENNA AND IN AN ARC OF 135 DEG. ON EACH SIDE OF THE AIRCRAFT CENTERLINE), MAKE SURE THAT THE RADAR DOES NOT OPERATE. THIS WILL PREVENT INJURY TO PERSONNEL BECAUSE OF EMISSIONS AND MOVEMENT OF THE RADAR ANTENNA.

C. Inspection of the Radome, the Windows, the External Structure of the Fuselage and the Landing Gear

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Radome
A.	(1) Externally examine the radome (skin, studs, latches, etc.) for scratches, dents, damaged paintwork and other damage. (2) Make sure that the lightning arrester strips are in the correct condition. (3) Do a tap test for debonding and delamination on the external surface of the radome as follows: - On the cap area (diameter of 700 mm (27.56 in.) around the center of the radome) NTM 511003. Area of the Tap Test Inspection of the Radome after a Hail Strike during the Flight ** ON A/C NOT FOR ALL (4) Open the radome (Ref. AMM TASK 53-15-11-010-001). (5) Internally examine the radome for the signs of delamination and/or debonding.	X
	If you find damage:
	(a) Do a detailed inspection of the radome (Ref. AMM TASK 53-15-11-200-001).		X
	(b) Visually examine the weather-radar antenna drive-unit and the weather radar for damage.		X
	- If you find damage on the weather radar antenna, replace it (Ref. AMM TASK 34-41-11-000-004) (Ref. AMM TASK 34-41-11-000-011) and (Ref. AMM TASK 34-41-11-400-005) (Ref. AMM TASK 34-41-11-400-013).			X
	(c) Visually examine the localizer antenna and the glide/slope antenna for damage.		X
	- If you find damage, do a functional test of the Instrument Landing System (ILS) (Ref. AMM TASK 34-36-00-720-001) (Ref. AMM TASK 34-36-00-720-003) (Ref. AMM TASK 34-36-00-720-006).			X
	- If an ILS ground test is not available, do an operational test of the ILS function (Ref. AMM TASK 34-36-00-710-001) (Ref. AMM TASK 34-36-00-710-004) (Ref. AMM TASK 34-36-00-710-009).			X
	(d) Visually examine the adjacent structure (FR0) for damage.		X
B.	Close the radome (Ref. AMM TASK 53-15-11-410-001).
2.	Inspection of the Flight Compartment Windshields, Fixed and Sliding Windows
A.	Do a check of the flight compartment windshields and the fixed and sliding windows for: - Cracks, delamination and changes in color (indication of damage because of too much heat).	X
	If you find damage:
	(1) Internally examine the windshields and the internal sides of the uprights and frames of the fixed and sliding windows for: - Distortion, cracks and pulled or damaged fasteners.		X
3.	Inspection of the Cabin Windows
A.	Examine the cabin windows for: - Cracks and crazing.	X
	If you find damage: - Do a detailed visual inspection of the cabin window panes. This includes the window panes in the doors (Ref. AMM TASK 56-21-13-200-001).		X
4.	Inspection of the External Fuselage Structure
A.	Examine the skin, the doors, the fairings, the belly fairing and the fillets for: - Erosion, dents, cracks, missing/pulled or damaged fasteners or damaged paintwork. If you find: (1) Only erosion: - No other inspection is necessary.	X
	(2) Other damage:
	a_ Get access to and internally examine:		X
	- All the frames, stringers, fittings and component mounts (at and near the location of the damage) for: . Distortion, cracks, pulled or damaged fasteners or damaged paintwork.
	- All the components, pipes, ducts, electrical harnesses, cables, pulleys and mechanical linkages for: . Distortion, cracks, rupture, fluid leakage or breaks.
5.	Inspection of the Belly Fairing
A.	Externally examine all the belly fairing panels, specially the leading-edge root fairing and the upper and lower wing fairings for: - Dents, erosion, cracks, pulled or damaged fasteners or damaged paintwork. If you find damage:	X
	(1) Remove the damaged panel and internally examine the belly fairing structure.		X
	(2) Examine all the components, pipes, ducts, electrical harnesses and their mounts for distortion, cracks, breaks and fluid leakage.		X
6.	Inspection of the NLG
A.	If the NLG was extended during the hail strike or there is a hole in the NLG door:
	(1) Do a General Visual Inspection (GVI) of the NLG (Ref. AMM TASK 32-21-00-200-002).	X
	(2) Do a GVI of the internal and external sides of the NLG doors.	X
	(3) Do a GVI of the components, the pipes, the cables and the pulleys in the NLG bay.	X
	(4) Do a GVI of the NLG bay structure for dents, distortion, cracks, pulled or damaged fasteners or damaged paintwork.	X
B.	If the NLG was retracted during the hail strike: - Examine the NLG doors for damage.	X
7.	Inspection of the MLG
A.	If the MLG was extended during the hail strike or there is a hole in the MLG door:
	(1) Do a GVI of the MLG (Ref. AMM TASK 32-11-00-200-001).	X
	(2) Do a GVI of the internal and external sides of the MLG doors.	X
	(3) Do a GVI of the components, the pipes, the cables and the pulleys in the MLG bay.	X
	(4) Do a GVI of the MLG bay structure for dents, distortion, cracks, pulled or damaged fasteners or damaged paintwork.	X
B.	If the MLG was retracted during the hail strike: - Examine the MLG doors for damage.	X

Subtask 05-51-14-210-063-B ** ON A/C NOT FOR ALL

C. Inspection of the Radome, the Windows, the External Structure of the Fuselage and the Landing Gear

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Radome
A.	(1) Externally examine the radome (skin, studs, latches, etc.) for scratches, dents, damaged paintwork and other damage. (2) Make sure that the lightning arrester strips are in the correct condition. (3) Do a tap test for debonding and delamination on the external surface of the radome as follows: - On the cap area (diameter of 700 mm (27.56 in.) around the center of the radome) NTM 511003. Area of the Tap Test Inspection of the Radome after a Hail Strike during the Flight ** ON A/C NOT FOR ALL (4) Open the radome (Ref. AMM TASK 53-15-11-010-001). (5) Internally examine the radome for the signs of delamination and/or debonding.	X
	If you find damage:
	(a) Do a detailed inspection of the radome (Ref. AMM TASK 53-15-11-200-001).		X
	(b) Visually examine the weather-radar antenna drive-unit and the weather radar for damage:		X
	- If you find damage on the weather radar antenna, replace it (Ref. AMM TASK 34-41-11-000-004) (Ref. AMM TASK 34-41-11-000-802) and (Ref. AMM TASK 34-41-11-400-005) (Ref. AMM TASK 34-41-11-400-802).			X
	(c) Visually examine the localizer antenna and the glide/slope antenna for damage.		X
	- If you find damage, do a functional test of the Instrument Landing System (ILS) (Ref. AMM TASK 34-36-00-720-002) (Ref. AMM TASK 34-36-00-720-004).			X
	- If an ILS ground test is not available, do an operational test of the ILS function (Ref. AMM TASK 34-36-00-710-003) (Ref. AMM TASK 34-36-00-710-006).			X
	(d) Visually examine the adjacent structure (FR0) for damage.		X
B.	Close the radome (Ref. AMM TASK 53-15-11-410-001).
2.	Inspection of the Flight Compartment Windshields and the Fixed and Sliding Windows
A.	Do a check of the flight compartment windshields and the fixed and sliding windows for cracks, delamination and changes in color (indication of damage because of too much heat).	X
	If you find damage:
	(1) Internally examine the windshields and the internal sides of the uprights and frames of the fixed and sliding windows for: - Distortion, cracks and pulled or damaged fasteners.		X
3.	Inspection of the Cabin Windows
A.	Examine the cabin windows for: - Cracks or crazing.	X
	If you find damage:
	- Do a detailed visual inspection of the cabin window panes. This includes the window panes in the doors (Ref. AMM TASK 56-21-13-200-001).		X
4.	Inspection of the External Fuselage Structure
A.	Examine the skin, the doors, the fairings, the belly fairing and the fillets for: - Erosion, dents, cracks, missing/pulled or damaged fasteners or damaged paintwork.	X
	If you find damage:
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage:
	(a) Get access to and internally examine:		X
	- All the frames, stringers, fittings and component mounts (at and near the location of the damage) for: . Distortion, cracks, pulled or damaged fasteners or damaged paintwork.
	- All the components, pipes, ducts, electrical harnesses, cables, pulleys and mechanical linkages for: . Distortion, cracks, rupture, fluid leakage or breaks.
5.	Inspection of the Belly Fairing
A.	Externally examine all the belly fairing panels, specially the leading-edge root fairing and the upper and lower wing fairings for: - Dents, erosion, cracks, pulled or damaged fasteners or damaged paintwork.	X
	If you find damage:
	(1) Remove the damaged panel and internally examine the belly fairing structure.		X
	(2) Examine all the components, pipes, ducts, electrical harnesses and their mounts for distortion, cracks, breaks or fluid leakage.		X
6.	Inspection of the NLG
A.	If the NLG was extended during the hail strike or if there is a hole in the NLG door:
	(1) Do a General Visual Inspection (GVI) of the NLG (Ref. AMM TASK 32-21-00-200-002).	X
	(2) Do a GVI of the internal and external sides of the NLG doors.	X
	(3) Do a GVI of the components, the pipes, the cables and the pulleys in the NLG bay.	X
	(4) Do a GVI of the NLG bay structure for dents, distortion, cracks, pulled or damaged fasteners or damaged paintwork.	X
B.	If the NLG was retracted during the hail strike: - Examine the NLG doors for damage.	X
7.	Inspection of the MLG
A.	If the MLG was extended during the hail strike or if there is a hole in the MLG door:
	(1) Do a GVI of the MLG (Ref. AMM TASK 32-11-00-200-001).	X
	(2) Do a GVI of the internal and external sides of the MLG doors.	X
	(3) Do a GVI of the components, the pipes, the cables and the pulleys in the MLG bay.	X
	(4) Do a GVI of the MLG bay structure for dents, distortion, cracks, pulled or damaged fasteners or damaged paintwork.	X
B.	If the MLG was retracted during the hail strike: - Examine the MLG doors for damage.	X

Subtask 05-51-14-210-064-A

CAUTION: WHEN YOU MOVE THE VANE, BE CAREFUL NOT TO HIT AND NOT TO APPLY FORCE TO THE END STOPS OF THE AOA SENSOR.

D. Inspection of the Probes, Sensors and Antennas

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the probes, sensors and antennas
A.	Examine all the probes and sensors and their adjacent structures: - The pitot probes - The static probes and the standby static probes - The Total Air Temperature (TAT) sensors - The Angle Of Attack (AOA) sensors - The visual icing indicator - The ice detectors (if installed). Make sure that none of the probes or sensors have signs of impact or cracks or are bent or damaged. Make sure that there are no signs of impact in the adjacent area.	X
	(1) Slowly move the AOA sensor from the maximum to the minimum mechanical stop (+85° to -35°) with your hand and make sure that there are no hard points. Do not apply force at the mechanical stops.	X
	(a) If you find a hard point or damage on the AOA sensor, replace it (Ref. AMM TASK 34-11-19-000-001) (Ref. AMM TASK 34-11-19-400-001).		X
	(2) If you find a bent or damaged pitot probe, replace it (Ref. AMM TASK 34-11-15-000-001) (Ref. AMM TASK 34-11-15-400-001).		X
	(3) If you find damage on the LH/RH static probes 1 or 2 and/or the LH/RH standby static probe 3, make sure that the damage is not more than the permitted damage (Ref. AMM TASK 34-13-00-200-001).		X
	(a) If the damage is more than the permitted damage, replace the LH/RH static probes 1 or 2 and/or the LH/RH standby static probe 3 (Ref. AMM TASK 34-11-16-000-001) (Ref. AMM TASK 34-11-16-400-002).			X
	(4) If you find signs of impact or damage: - In the red rectangle area around a static port, or - In front of the red rectangle area around a static port: Refer to the Structural Repair Manual (SRM). NOTE: The SRM contains the approved damage limits and repair procedures.		X
	(5) If you find damage on the TAT sensor, replace it (Ref. AMM TASK 34-11-18-000-001) (Ref. AMM TASK 34-11-18-400-001).		X
	(6) If you find damage on the visual icing indicator, replace it (Ref. AMM TASK 30-81-21-000-001) (Ref. AMM TASK 30-81-21-400-001).		X
	(7) If you find damage on the ice detector (if installed), replace it (Ref. AMM TASK 30-81-31-000-001) (Ref. AMM TASK 30-81-31-400-001).		X
B.	Examine all the antennas and the beacon lights for: - Signs of cracks or damage.	X

Subtask 05-51-14-210-066-A

E. Inspection of the Stabilizers

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Vertical Stabilizer
A.	Examine the dorsal fin, the leading edge and the tip fairing externally for: - Erosion, dents, cracks, pulled or damaged fasteners, honeycomb delamination, core damage and damaged paintwork. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: (a) Examine internally at and near the damage for: - Dents, cracks, pulled or damaged fasteners, honeycomb delamination, core damage and damaged paintwork.		X
B.	Examine the spar box of the vertical stabilizer for erosion and scores.	X
C.	Examine the rudder and the trailing-edge access doors externally for: - Erosion, distortion, cracks, pulled or damaged fasteners, honeycomb delamination and core damage. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the rudder hinge and the actuator attach fittings for distortion, cracks and damaged paintwork.		X
D.	Examine all the static dischargers and retainers for damage.	X
2.	Inspection of the Horizontal Stablizer
A.	Examine the leading edge and the tip fairing externally for: - Erosion, dents, cracks, pulled or damaged fasteners, honeycomb delamination, core damage and damaged paintwork. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: Examine internally at and near the damage for cracks, distortion, pulled or damaged fasteners and damaged paintwork.		X
B.	Examine the spar box and the logo light of the horizontal stabilizer for erosion and scores.	X
C.	Examine the elevators and the trailing-edge access doors externally for: - Erosion, distortion, cracks, pulled or damaged fasteners, honeycomb delamination and core damage. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the elevator hinge and the actuator fittings for distortion, cracks and damaged paintwork.		X
	- Examine all the components, the pipes, the electrical harnesses and the mechanical linkages for distortion, cracks, rupture, breaks or fluid leakage.
D.	Examine all the static dischargers and retainers for damage.	X

Subtask 05-51-14-210-067-A ** ON A/C NOT FOR ALL

F. Inspection of the Wings

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Leading Edge, the Fillets and the Slats
A.	Examine for erosion, distortion, cracks and pulled or damaged fasteners. If you find:	X
	(1) Only erosion: No other inspection is necessary.
	(2) Other damage: - Examine the leading edge section internally, at and near the damage, for distortion, cracks and pulled or damaged fasteners.		X
	- Examine the ducts and the related attach points for damage.		X
	- Examine the slat section for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- Examine the actuators, the slat tracks and the slat-track attach points for damage.		X
	- Examine the slat tracks for brinelling on the roller tracks.		X
	- Examine the aileron servo-controls and the hinge fittings for damage.		X
	- Examine the spoiler actuators and the hinge fittings for damage.		X
2.	Inspection of the Wing Tip Fairings, the Anti-Collision Strobe and Beacon Lights, the Navigation Lights and the Landing Lights
A.	Examine for erosion, distortion, cracks and pulled or damaged fasteners.	X
B.	Examine all the static dischargers and retainers for damage.	X
3.	Inspection of the Main Structure of the Wing
A.	Examine for erosion and scores.	X
4.	Inspection of the Trailing Edge Falsework, the Flaps, the Ailerons and the Spoilers
A.	Examine the control surfaces externally for erosion, signs of impact, damaged paintwork, abrasions, scratches or dents, distortion, cracks and pulled or damaged fasteners. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the falsework internally, at and near the damage, for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- Examine the flap carriages and the fairing for distortion and cracks.		X
	- Examine the flap tracks for brinelling and damage.		X
B.	Examine all the static dischargers and retainers for damage.	X

Subtask 05-51-14-210-067-B ** ON A/C NOT FOR ALL

F. Inspection of the Wings

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Leading Edge, the Fillets and the Slats
A.	Examine for erosion, distortion, cracks and pulled or damaged fasteners. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the leading edge section internally, at and near the damage, for distortion, cracks and pulled or damaged fasteners.		X
	- Examine the ducts and the related attach points for damage.		X
	- Examine the slat section for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- Examine the actuators, the slat tracks and the slat-track attach points for damage.		X
	- Examine the slat tracks for brinelling on the roller tracks.		X
	- Examine the aileron servo-controls and the hinge fittings for damage.		X
	- Examine the spoiler actuators and the hinge fittings for damage.		X
2.	Inspection of the Sharklet, the Anti-Collision Strobe and Beacon Lights, the Navigation Lights and the Landing Lights
A.	Examine the sharklet for erosion, signs of impact, cracks and pulled or damaged fasteners. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: (a) Do a Non-Destructive Testing (NDT) inspection for delamination. Refer to the Non-Destructive Testing Manual: NTM 511003.		X
	(b) Refer to the SRM 573123 for allowable damage.		X
	If the damage is more than the SRM allowable damage:
	- Replace the sharklet (Ref. AMM TASK 57-31-23-000-801) and (Ref. AMM TASK 57-31-23-400-801).			X
B.	Do a visual inspection of the navigation-light and strobe-light glazing panels. If you find damage:	X
	(1) Replace the glazing panel(s). - For the navigation-light glazing panel: (Ref. AMM TASK 57-37-13-000-801) and (Ref. AMM TASK 57-37-13-400-801). - For the strobe-light glazing panel: (Ref. AMM TASK 57-37-13-000-802) and (Ref. AMM TASK 57-37-13-400-802).		X
	(2) Do an operational test of the light with the replaced glazing panel. - For the navigation light: (Ref. AMM TASK 33-41-00-710-001). - For the strobe light: (Ref. AMM TASK 33-48-00-710-002).		X
C.	Examine the landing lights for: (1) Distortion, cracks and pulled or damaged fasteners. (2) Lens damage.	X
	If you find damage: - Do the deactivation of the landing lights (Ref. AMM TASK 33-42-00-040-001) or - Replace the landing lights (Ref. AMM TASK 33-42-11-000-001) and (Ref. AMM TASK 33-42-11-400-003).		X
D.	Do a visual inspection of the static dischargers and retainers for damage.	X
	(1) If you find damage: - Replace the static dischargers (Ref. AMM TASK 23-61-41-000-001) (Ref. AMM TASK 23-61-41-400-001). NOTE: 20% of the static dischargers can be unserviceable or missing on each wing.		X
3.	Inspection of the Main Structure of the Wing
A.	Examine for erosion and scores.	X
4.	Inspection of the Trailing Edge Falsework, the Flaps, the Ailerons and the Spoilers
A.	Examine the control surfaces externally for erosion, signs of impact, damaged paintwork, abrasions, scratches or dents, distortion, cracks and pulled or damaged fasteners. If you find:	X
	(1) Only erosion: - No other inspection is necessary.
	(2) Other damage: - Examine the falsework internally, at and near the damage, for distortion, cracks, pulled or torn fasteners and damaged paintwork.		X
	- Examine the flap carriages and the fairing for distortion and cracks.		X
	- Examine the flap tracks for brinelling and damage.		X
B.	Examine all the static dischargers and retainers for damage.	X

Subtask 05-51-14-410-053-A

G. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close all the panels and doors you opened during this inspection.
(3) Remove the safety devices from the MLG doors (Ref. AMM TASK 32-00-00-081-001) and close the MLG doors (Ref. AMM TASK 32-12-00-410-001).
(4) Remove the safety devices from the NLG doors (Ref. AMM TASK 32-00-00-081-001) and close the NLG doors (Ref. AMM TASK 32-22-00-410-001).

Subtask 05-51-14-866-055-A

H. Retraction of the Flight Control Surfaces
(1) Retract the spoilers (Ref. AMM TASK 27-60-00-866-002).
(2) Retract the flaps (Ref. AMM TASK 27-50-00-866-009).
(3) Retract the slats (Ref. AMM TASK 27-80-00-866-005).

Subtask 05-51-14-710-052-A

I. Operational Test of the Systems

ITEM	INSPECTION TASKS	PHASE 2
	NOTE : The tests that follow are necessary only if: - You did work on the system after the inspection for damage - You found damage on the structure adjacent to a flight control surface.
1.	Operate the ailerons 3 times. (Ref. AMM TASK 27-14-00-710-001).	X
2.	Operate the rudder 3 times. (Ref. AMM TASK 27-24-00-710-002).	X
3.	Operate the elevator 3 times. (Ref. AMM TASK 27-34-00-710-001).	X
4.	Operate the trimmable horizontal stabilizer 3 times. (Ref. AMM TASK 27-44-00-710-001).	X
5.	Operate the spoilers 3 times. (Ref. AMM TASK 27-64-00-710-001).	X
6.	Operate the flaps and the slats 3 times. (Ref. AMM TASK 27-54-00-710-001) (Ref. AMM TASK 27-84-00-710-001). NOTE : The tests that follow are necessary only if: - You did work on the system after the inspection for damage - You found damage on the structure adjacent to the landing gear doors.	X
7.	Retract and extend the landing gear 3 times (Ref. AMM TASK 32-30-00-867-001) (Ref. AMM TASK 32-30-00-867-002). Make sure that the landing gear and the doors move smoothly and freely. NOTE : If you find damage only on the main doors of the main landing gear or only on the fuselage structure adjacent to the main doors: - Do a test of the main doors only. Use the circuit which opens/closes the doors when the aircraft is on the ground.	X

5. Close-up
Subtask 05-51-14-865-056-A

A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
121VU	COM NAV/RADAR/1	5SQ1	K13
** ON A/C NOT FOR ALL
121VU	COM NAV/RADAR/2	5SQ2	K14
** ON A/C ALL
FOR FIN: 9DA1 (PROBEPITOT, 1)
49VU	ANTI ICE/PROBES/AOA/1	4DA1	D04
49VU	ANTI ICE/PROBES/PITOT/1	3DA1	D02
122VU	ANTI ICE/PROBES/1/STATIC	5DA1	Z13
122VU	ANTI ICE/PROBES/1/TAT	1DA1	Z12
FOR FIN: 9DA2 (PROBEPITOT, 2)
122VU	ANTI ICE/PROBES/2/TAT	1DA2	Y15
122VU	ANTI ICE/PROBES/2/PITOT	3DA2	Y14
122VU	ANTI ICE/PROBES/2/AOA	4DA2	Y13
122VU	ANTI ICE/PROBES/2/STATIC	5DA2	Y11
FOR FIN: 9DA3 (PROBEPITOT, 3)
122VU	ANTI ICE/PROBES/3/PITOT	3DA3	Z16
122VU	ANTI ICE/PROBES/3/AOA	4DA3	Z15
122VU	ANTI ICE/PROBES/3/STATIC	5DA3	Z14
FOR FIN: 11FP1 (SENSORTAT, 1)
49VU	NAV PROBES/ADIRU1/115VAC	4FP1	F06
121VU	ADIRS/ADIRU/3/115VAC	4FP3	N05
FOR FIN: 11FP2 (SENSORTAT, 2)
121VU	ADIRS/ADIRU/2/115VAC	4FP2	N06
FOR FIN: 3FP1 (SENSORANGLE OF ATTACK, 1)
49VU	NAV PROBES/ADIRU 1/AND AOA 1/26VAC	5FP1	F07
121VU	ADIRS/ADIRU/3PWR/SWTG	9FP	N09
** ON A/C NOT FOR ALL
FOR FIN: 3FP2 (SENSORANGLE OF ATTACK, 2)
121VU	ADIRS/ADIRU/2PWR/SHED	10FP	N10
** ON A/C ALL
121VU	ADIRS/ADIRU/2/26VAC AND AOA	5FP2	N08
** ON A/C NOT FOR ALL
121VU	ADIRS/2PWR/SHED &/AOA2 MON	10FP	N10
** ON A/C ALL
FOR FIN: 3FP3 (SENSORANGLE OF ATTACK, 3)
121VU	ADIRS/ADIRU/3/26VAC AND AOA	5FP3	N07

Subtask 05-51-14-865-057-A

B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
FOR FIN: 9DA1 (PROBEPITOT, 1)
49VU	ANTI ICE/PROBES/PHC/1	2DA1	D03
FOR FIN: 9DA2 (PROBEPITOT, 2)
122VU	ANTI ICE/PROBES/PHC/2	2DA2	Y12
FOR FIN: 9DA3 (PROBEPITOT, 3)
122VU	ANTI ICE/PROBES/PHC/3	2DA3	Y16

Subtask 05-51-14-860-055-A

C. Put the aircraft back to its initial configuration.
(1) Depressurize the Green hydraulic system
(Ref. AMM TASK 29-10-00-864-001).
(2) Depressurize the Blue hydraulic system
(Ref. AMM TASK 29-10-00-864-003).
(3) Depressurize the Yellow hydraulic system
(Ref. AMM TASK 29-10-00-864-002).
(4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

Subtask 05-51-14-942-055-A

D. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the warning notices from the cockpit.
(3) Remove the access platform(s).

[Rev.10 from 2021] 2026.03.31 22:51:21 UTC