Inspection of the Aircraft after a Bird Strike

TASK 05-51-14-200-803-A
Inspection of the Aircraft after a Bird Strike

WARNING: THERE IS A POSSIBLE HEALTH RISK TO PERSONNEL WHO DO MAINTENANCE TASKS AFTER A BIRD STRIKE. THE SAFETY MEASURES THAT FOLLOW ARE RECOMMENDED:

USE DISPOSABLE GLOVES.
USE CUT RESISTANT GLOVES OVER THE DISPOSABLE GLOVES.
USE A DISPOSABLE COVERALL IF THERE IS A RISK OF BODY CONTACT WITH THE BIRD REMAINS (ORGANIC MATTER) DURING FEATHER COLLECTION OR ENGINE CLEANING.
DO NOT USE PRESSURIZED AIR OR WATER TO CLEAN THE PARTS WHICH WERE IN CONTACT WITH THE BIRD.
REMOVE THE BIRD REMAINS AND PUT THEM IN A PLASTIC BAG.
DO NOT TOUCH YOUR FACE, EYES, NOSE, ETC. WITH YOUR GLOVES.
REMOVE THE GLOVES AND THE DISPOSABLE COVERALL AND PUT THEM IN THE SAME PLASTIC BAG AS THE REMAINS. SEAL THE BAG.
DISCARD THE BAG AS YOU DO FOR USUAL GARBAGE.
CAREFULLY WASH YOUR HANDS WITH SOAP AND WATER.

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: 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.

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
After a flight crew report of bird strike events, you must do the inspections that follow before the subsequent flight.
Airbus recommends that you do the inspection immediately.

NOTE: It is not easy to find and see signs of bird strike after time and/or bad weather.

2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE
No specific	AR	ACCESS PLATFORM 3M (10 FT)
No specific	AR	BAG - PLASTIC
No specific	AR	BOOT - RUBBER
No specific	AR	GLOVES - RUBBER
No specific	AR	GOGGLES - PROTECTIVE
No specific	1	LIGHT SOURCE - WHITE
No specific	1	MIRROR - INSPECTION, FLEXIBLE
No specific	AR	OVERALL WITH HOOD - WATERPROOF
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	STEPLADDER 3,0 M (9.8 FT)
No specific	AR	WARNING NOTICE(S)

B. Referenced Information

REFERENCE	DESIGNATION
TASK 12-21-11-615-002-A	External Cleaning
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 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 33-48-00-040-001-A	Deactivation of the Anti-Collision (Beacon) Light
TASK 33-48-00-710-002-A	Operational Test of the Anti-Collision/Strobe Lighting
TASK 33-48-11-000-001-A	Removal of the Upper Beacon/Strobe Light from the Outside of the Fuselage
TASK 33-48-11-400-001-A	Installation of the Upper Beacon/Strobe Light from the Outside of the Fuselage
TASK 33-48-12-000-001-A	Removal of the Lower Beacon/Strobe Light from the Fuselage Outside
TASK 33-48-12-400-001-A	Installation of the Lower Beacon/Strobe Light from the Fuselage Outside
TASK 33-49-00-040-001-A	Deactivation of the Wing and Engine Scan Light Lens (Cover)
TASK 33-49-11-000-001-A	Removal of the Wing and Engine Scan Light
TASK 33-49-11-400-001-A	Installation of the Wing and Engine Scan Light
TASK 34-10-00-170-001-A	Flushing of the Total Pressure Lines
TASK 34-10-00-170-003-A	Draining and Flushing of Standby Pneumatic Circuits
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 34-11-18-200-002-A	Inspection/Check 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 34-22-25-170-001-A	Draining and Flushing of Standby Pneumatic Circuits
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
First Step - Walk-Around Inspection Pattern from the Ground
First Step - Walk-Around Inspection Pattern from the Cabin Windows and Platform
First Step - Table for Inspection from the Ground
First Step - Table for Inspection from the Cabin Windows and Platform ** ON A/C NOT FOR ALL
First Step - Table for Inspection from the Cabin Windows and Platform ** ON A/C NOT FOR ALL
Damage Reporting Sheet ** ON A/C NOT FOR ALL
Damage Reporting Sheet ** ON A/C NOT FOR ALL
Damage Reporting Sheet ** ON A/C NOT FOR ALL
Damage Reporting Sheet ** ON A/C NOT FOR ALL

3. Job Set-up
Subtask 05-51-14-941-051-A

A. General Information
(1) Description of the inspection procedure
(a) The inspections are divided into three steps:
1 First step: Walk-around visual inspection
The first step is a walk-around visual inspection of all aircraft surfaces. This is to find signs of bird strike and/or damage (identification of impacted areas).
2 Second step: Cleaning of bird strike signs
3 Third step: Inspection

Examples:
First step:
You find signs of bird strike during the walk-around on the left windshield and on the left engine fan.
Second step:
You clean the signs of bird strike.
Third step:
You do an inspection of the forward fuselage and the left engine/nacelle.
(2) Inspection preparation
(a) Before you start, we recommend that you get information from the crew about the flight conditions:

The engine behavior
The smell in the air conditioning outlets
The navigation and radio system behavior
The aircraft configuration (position of the landing gears and the flight controls)
The flight phase at the time when the impact occurred.

(b) Make sure that you have the related aircraft Post Flight Report (PFR).
(c) You must do a check of all the events in the crew report and in the PFR in addition/conjunction with this inspection.

Subtask 05-51-14-481-053-A

B. Safety Precautions
(1) Make sure that the safety devices 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.

Subtask 05-51-14-010-053-A

C. Get Access
(1) Landing Gear Doors
(a) If the landing gear doors were in transit, opened during the event or if you do not know the position of the landing gear doors:
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 05-51-14-866-056-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) Set the Trimmable Horizontal Stabilizer (THS) pitch-trim control wheel to the full aircraft nose-up position.
(4) Fully extend the flaps and the slats (Ref. AMM TASK 27-50-00-866-008) and (Ref. AMM TASK 27-80-00-866-004).

Subtask 05-51-14-860-056-A

E. Aircraft Maintenance Configuration
(1) Depressurize the aircraft hydraulic systems
(Ref. AMM TASK 29-00-00-864-001).
(2) Put the ACCESS PLATFORM 3M (10 FT) in position near the radome and the aft passenger/crew door.

NOTE: As an alternative tool, you can use a STEPLADDER 3,0 M (9.8 FT) to get a minimum height of 3 m (10 ft.).

(3) After the inspection (first step):
If you find signs of bird strike or damage:

It can be necessary to use an ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE near the area that you must clean and examine (second and third step).

4. Procedure
Subtask 05-51-14-869-053-A

A. General

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

(1) If there is damage to the aircraft structure, refer to the Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures.
(2) If the pilot gave a report of:

The engine stall or
The engine parameter change/exceeded or
The smells in the air conditioning outlet.
Do the related step for the inspection of the engine (refer to the inspection paragraph 4.V. Inspection of the Engines and/or Nacelles).

(3) You must systematically open and examine the radome. In some special conditions, the radome can have delamination without organic residue or signs of impact.

Subtask 05-51-14-210-068-A

B. First Step: Walk-Around Visual Inspection

First Step - Walk-Around Inspection Pattern from the Ground

First Step - Walk-Around Inspection Pattern from the Cabin Windows and Platform

(1) For a better walk-around visual inspection, do the inspection at the checkpoints and while you move from one checkpoint to the other.
The points shown give the checkpoints for the sequence of the walk-around visual inspection.
(2) Do the walk-around visual inspection with a good luminosity level (daylight or hangar light).
(3) Do the walk-around visual inspection of all the aircraft surfaces.
Do the walk-around visual inspection from:

The ground
The cabin windows
The ACCESS PLATFORM 3M (10 FT) near the radome and the aft passenger/crew doors.

(a) Do a check for:

Signs of impact, scratches, dents, damaged paintwork or other damage during the General Visual Inspection (GVI) of the radome
Impact damage or signs of bird strike, for example organic material (i.e. blood spatter, bird remains, feathers etc.)
Fuel, oil or hydraulic leaks
Missing parts.

(b) Record the area(s) with signs of bird strike or damage.

First Step - Table for Inspection from the Ground

First Step - Table for Inspection from the Cabin Windows and Platform ** ON A/C NOT FOR ALL

Damage Reporting Sheet ** ON A/C NOT FOR ALL

Subtask 05-51-14-615-050-A ** ON A/C NOT FOR ALL

C. Second Step: Cleaning of Bird Strike Signs
(1) Put an ACCESS PLATFORM 12M (40 FT) - ADJUSTABLE in position (if necessary) adjacent to the signs of bird strike or damaged area(s).
(2) The persons that do the cleaning must put on BOOT - RUBBER, GLOVES - RUBBER, GOGGLES - PROTECTIVE and OVERALL WITH HOOD - WATERPROOF.
(3) Before cleaning, use a marking pen to identify the damaged area.
(4) Collect organic material for analysis.

NOTE: If you must determine the bird species because of the local regulations, Airbus recommends that you do the steps that follow. If not, you can remove the bird remains and do the cleaning step immediately.

(a) For large pieces of bird, remove different types of feathers (breast, back, wing, tail) and put them in a re-sealable BAG - PLASTIC.
(b) For small pieces of bird feathers and/or tissue, remove and put them in a re-sealable BAG - PLASTIC.
(c) For blood smears or tissue on the surface, remove them with a paper towel, gauze or alcohol wipe and put them in a re-sealable BAG - PLASTIC. Include the material that you used for the removal.

NOTE: It is not permitted to use water to remove blood smears or tissue because water causes mold. Mold causes damage to the material necessary to determine the bird species.

(d) Seal the BAG - PLASTIC and attach a label with the date, aircraft registration number and area that the remains came from.
(e) Send the BAG - PLASTIC with the collected bird remains to the nearest local airport-operations wildlife-administrator to determine the species.
(5) Remove the remaining organic material.
(a) Put all the remaining pieces of bird, GLOVES - RUBBER and other items you will discard in another BAG - PLASTIC. Seal the BAG - PLASTIC and discard it correctly.
(b) Wash your hands with soap and water.
(6) Do a manual cleaning (Ref. AMM TASK 12-21-11-615-002).
(7) Make sure that the pen marks are not removed.

Subtask 05-51-14-615-050-B ** ON A/C NOT FOR ALL

Pieces of bird can be used to determine the bird species. Contact CFM for more information.

(5) Collect organic material for analysis.

NOTE: If you must determine the bird species because of the local regulations, Airbus recommends that you do the steps that follow. If not, remove the bird remains and do the cleaning step immediately.

(a) For large pieces of bird, remove different types of feathers (breast, back, wing, tail) and put them in a re-sealable BAG - PLASTIC.
(b) For small pieces of bird feathers and/or tissue, remove them and put them in a re-sealable BAG - PLASTIC.
(c) For blood smears or tissue on the surface, remove them with a paper towel, gauze or alcohol wipe and put them in a re-sealable BAG - PLASTIC. Include the material that you used for the removal.

NOTE: It is not permitted to use water to remove blood smears or tissue because water causes mold. Mold causes damage to the material necessary to determine the bird species.

(d) Seal the BAG - PLASTIC and attach a label with the date, aircraft registration number and area that the remains came from.
(e) Send the BAG - PLASTIC with the collected bird remains to the nearest local airport-operations wildlife-administrator to determine the species.
(6) Remove the remaining organic material.
(a) Put all the remaining pieces of bird, GLOVES - RUBBER and other items you will discard in another BAG - PLASTIC. Seal the BAG - PLASTIC and discard it correctly.
(b) Wash your hands with soap and water.
(7) Do a manual cleaning (Ref. AMM TASK 12-21-11-615-002).
(8) Make sure that the pen marks are not removed.

Subtask 05-51-14-210-069-A ** ON A/C NOT FOR ALL

D. Third Step: Inspection
(1) Radome systematic inspection:

You must systematically open and examine the radome. In some special conditions, the radome can have delamination without organic residue or signs of impact.

(2) For each sign of bird strike or damage that you found during the first step (walk-around):

Refer to the related inspection paragraph and
Do the applicable inspections (phase 1, then 2 and 3 if necessary).

The list below gives the inspection paragraphs:

Radome
Forward Fuselage (FR1 to FR24)
Center Fuselage (FR24 to FR64)
Aft Fuselage (FR64 to FR87)
Probes and Sensors
Antenna(s)
NLG
MLG
Engines and/or Nacelles
Pylons
Vertical Stabilizer
Horizontal Stabilizer
Wing Leading Edge
Wing Tip and Fence
Wing Main Structure
Wing Trailing Edge

NOTE: It can be necessary to do a special preparation before some inspections (for example, Inspection of the Radome).
The inspection preparation is given in the subtask immediately before the related inspection table.
When necessary, the subtask immediately after the related inspection table gives the circuit breakers you must close.

NOTE: You can refer to the tables that you wrote during the first-step walk-around inspection (and damage reporting sheet for the accurate damage location) to know the title of the paragraph you must refer to.

Subtask 05-51-14-210-069-B ** ON A/C NOT FOR ALL

D. Third Step: Inspection
(1) Radome systematic inspection:

You must systematically open and examine the radome. In some special conditions, the radome can have delamination without organic residue or signs of impact.

(2) For each sign of bird strike or damage that you found during the first step (walk-around):

Refer to the related inspection paragraph and
Do the applicable inspections (phase 1, then 2 and 3 if necessary).

The list below gives the inspection paragraphs:

Radome
Forward Fuselage (FR1 to FR24)
Center Fuselage (FR24 to FR64)
Aft Fuselage (FR64 to FR87)
Probes and Sensors
Antenna(s)
NLG
MLG
Engines and/or Nacelles
Pylons
Vertical Stabilizer
Horizontal Stabilizer
Wing Leading Edge
Sharklet
Wing Main Structure
Wing Trailing Edge

Subtask 05-51-14-865-058-A

E. 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

Subtask 05-51-14-210-070-A

F. Inspection of the Radome

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Radome
A.	Externally examine the radome (skin, studs, latches, etc.) for scratches, dents, damaged paintwork and other damage. Open the radome (Ref. AMM TASK 53-15-11-010-001). Internally examine the radome for the signs of delamination and/or debonding.	X
	If you find damage:
	(1) Do a detailed inspection of the radome (Ref. AMM TASK 53-15-11-200-001).		X
	(2) 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 D/O 34-41-11-00) (Ref. AMM TASK 34-41-11-000-012) (Ref. AMM TASK 34-41-11-000-802) (Ref. AMM TASK 34-41-11-400-005) (Ref. AMM D/O 34-41-11-40) (Ref. AMM TASK 34-41-11-400-014) (Ref. AMM TASK 34-41-11-400-802).			X
	(3) 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 D/O 34-36-00-72) (Ref. AMM TASK 34-36-00-720-002) (Ref. AMM D/O 34-36-00-72) (Ref. AMM D/O 34-36-00-72) (Ref. AMM TASK 34-36-00-720-006) (Ref. AMM D/O 34-36-00-72).			X
	- If an ILS ground test is not available, do an operational test of the ILS function (Ref. AMM D/O 34-36-00-71) (Ref. AMM TASK 34-36-00-710-003) (Ref. AMM D/O 34-36-00-71) (Ref. AMM D/O 34-36-00-71) (Ref. AMM TASK 34-36-00-710-009) (Ref. AMM D/O 34-36-00-71).			X
	(4) Visually examine the adjacent structure (FR0) for damage.		X
B.	Close the radome (Ref. AMM TASK 53-15-11-410-001).
2.	Close the circuit breaker(s) given in the subsequent paragraph.

Subtask 05-51-14-865-059-A

G. 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

Subtask 05-51-14-210-071-A

H. Inspection of the Forward Fuselage (FR1 to FR24)

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Flight Compartment Windshields, Fixed and Sliding Windows
A.	If you found signs of bird strike or damage in the area of the flight compartment windshields, fixed and sliding windows: - Examine them for cracking, delamination and changes in color (this shows damage because of too much heat) - Examine the wipers, the blade wipers and the rain repellant outlets . Make sure there is no damage.	X
	If you find too much damage (heavy bird strike): (1) Examine the windshield and the internal side of the fixed and the sliding window uprights and frames for: - Distortion, cracks and pulled or damaged fasteners.		X
2.	Inspection of the Cabin Windows
A.	If you found signs of bird strike or damage near the cabin windows: - Examine them 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
3.	Inspection of the External Fuselage Structure
A.	If you found signs of bird strike or damage on the external fuselage structure: - Examine the skin, the doors, the fairings and the fillets of the area(s) with signs of bird strike for: . Dents, cracks, missing/pulled or damaged fasteners or damaged paintwork.	X
	If you find damage, get access to and internally examine:
	- All the frames, stringers, fittings and component mounts (at and near the location of the damage) for: . Distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- All the components, pipes, ducts, electrical harnesses, cables, pulleys and mechanical linkages for: . Distortion, cracks, rupture, fluid leakage and breaks.		X

Subtask 05-51-14-210-072-A

I. Inspection of the Center Fuselage (FR24 to FR64)

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Cabin Windows
A.	If you found signs of bird strike or damage near the cabin windows: - Examine them 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
2.	Inspection of the External Fuselage Structure
A.	If you found signs of bird strike or damage on the external fuselage structure: - Examine the skin, the doors, the fairings and the fillets of the area(s) with signs of bird strike for: . Dents, cracks, missing/pulled or damaged fasteners or damaged paintwork.	X
	If you find damage, get access to and internally examine:
	- All the frames, stringers, fittings and component mounts (at and near the location of the damage) for:
	. Distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- All the components, pipes, ducts, electrical harnesses, cables, pulleys and mechanical linkages for:
	. Distortion, cracks, rupture, fluid leakage and breaks.		X
3.	Inspection of the Belly Fairing
A.	Externally examine the belly fairing panels (this includes the packs air inlet) where you found signs of bird strike or damage for: - Dents, cracks, pulled or damaged fasteners and 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 and fluid leakage.		X
4.	Inspection of the Drain Mast
A.	If you found signs of bird strike or damage on the drain mast: If it is bent, has cracks or is damaged: - Replace it.	X
B.	Make sure that the adjacent area is not damaged.	X
5.	Inspection of the Upper and Lower Beacon/Strobe Lights
A.	If you found signs of bird strike or damage on the upper and lower beacon/strobe lights, examine them for: - Distortion, cracks and pulled or damaged fasteners - Lens damage.	X
	If you find damage: (1) Do the deactivation of the anti-collision (beacon) light (Ref. AMM TASK 33-48-00-040-001), or (2) Replace them: - For the upper beacon/strobe light (Ref. AMM TASK 33-48-11-000-001) (Ref. AMM TASK 33-48-11-400-001). - For the lower beacon/strobe light (Ref. AMM TASK 33-48-12-000-001) (Ref. AMM TASK 33-48-12-400-001).		X
B.	Make sure that the adjacent area is not damaged.	X
6.	Inspection of the Wing and Engine Scan Lights
A.	If you found signs of bird strike or damage on the wing and engine scan light, examine it for: - Distortion, cracks and pulled or damaged fasteners - Lens damage.	X
	If you find damage: (1) Do the deactivation of the wing and engine scan light (Ref. AMM TASK 33-49-00-040-001), or (2) Replace it (Ref. AMM TASK 33-49-11-000-001) and (Ref. AMM TASK 33-49-11-400-001).		X
B.	Make sure that the adjacent area is not damaged.	X

Subtask 05-51-14-210-073-A

J. Inspection of the Aft Fuselage (FR64 to FR87)

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	External Fuselage Structure
A.	If you found signs of bird strike or damage on the external fuselage structure (this includes the Auxiliary Power Unit (APU) air inlet and drain mast): - Examine the skin, the doors, the fairings and the fillets of the area(s) with signs of bird strike for: . Dents, cracks, missing/pulled or damaged fasteners or damaged paintwork.	X
	If you find damage, get access to and internally examine:
	- All the frames, stringers, fittings and component mounts (at and near the location of the damage) for: . Distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	- All the components, pipes, ducts, electrical harnesses, cables, pulleys and mechanical linkages for: . Distortion, cracks, rupture, fluid leakage and breaks.		X

Subtask 05-51-14-860-058-A

K. Preparation Before Inspection Phases on the Probes & Sensors
(1) If you find damage on the probes and sensors, open, safety and tag the circuit breakers given in the subsequent paragraph.

Subtask 05-51-14-865-060-A

WARNING: MAKE SURE THAT THE PROBE HEATER AND WINDOW HEATER CIRCUIT-BREAKERS ARE OPEN BEFORE YOU OPEN THE PHC AND WHC CIRCUIT BREAKERS. IF YOU DO NOT OBEY THIS SEQUENCE:

THE PROBES WILL BECOME TOO HOT.
THIS CAN CAUSE INJURY TO MAINTENANCE PERSONNEL AND/OR DAMAGE TO EQUIPMENT.

L. 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/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 05-51-14-865-062-A

M. 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

Subtask 05-51-14-210-074-A ** ON A/C NOT FOR ALL

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

N. Inspection of the Probes & Sensors

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	If you found signs of bird strike or damage on: - 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 detector (if installed) Or on the adjacent structure: do the inspections of the related item(s).
A.	For the: - LH pitot probe 1 or - LH pitot probe 3 or - LH static probes 1 and 2 or the LH standby static probe 3:
	(1) Do an inspection of the pitot probe (Ref. AMM TASK 34-13-00-200-001).	X
	- If the pitot probe is bent, replace it (Ref. AMM TASK 34-11-15-000-001) and (Ref. AMM TASK 34-11-15-400-001).		X
	(2) Do an inspection of the static probes and the standby static probe (Ref. AMM TASK 34-13-00-200-001).	X
	- If you find damage, replace the related probe (Ref. AMM TASK 34-11-16-000-001) and (Ref. AMM TASK 34-11-16-400-002).		X
	(3) Do a detailed structural inspection: - In the red rectangle areas around the static ports, and - In front of the red rectangle areas around the static ports.	X
	(a) 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 Structural Repair Manual (SRM). NOTE: The SRM contains the approved damage limits and repair procedures.		X
	(4) Flush the principal total pressure-lines (Ref. AMM TASK 34-10-00-170-001).	X
	(5) Drain and flush the standby pneumatic circuits (Ref. AMM TASK 34-10-00-170-003).	X
B.	For the: - RH pitot probe 2 or - RH static probes 1 and 2 or RH standby static probe 3:
	(1) Do an inspection of the pitot probe (Ref. AMM TASK 34-13-00-200-001).	X
	- If the pitot probe is bent, replace it (Ref. AMM TASK 34-11-15-000-001) and (Ref. AMM TASK 34-11-15-400-001).		X
	(2) Do an inspection of the static probes and the standby static probe (Ref. AMM TASK 34-13-00-200-001).	X
	- If you find damage, replace the related probe (Ref. AMM TASK 34-11-16-000-001) and (Ref. AMM TASK 34-11-16-400-002).		X
	(3) Do a detailed structural inspection: - In the red rectangle areas around the static ports, and - In front of the red rectangle areas around the static ports.	X
	(a) 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 Structual Repair Manual (SRM). NOTE: The SRM contains the approved damage limits and repair procedures.		X
	(4) Flush the principal total pressure-lines (Ref. AMM TASK 34-10-00-170-001).	X
	(5) Drain and flush the standby pneumatic circuits (Ref. AMM TASK 34-10-00-170-003).	X
C.	For the TAT sensor:
	(1) Do an inspection of the TAT sensor (Ref. AMM TASK 34-11-18-200-002).	X
	- If the TAT sensor is clogged, replace it (Ref. AMM TASK 34-11-18-000-001) and (Ref. AMM TASK 34-11-18-400-001).		X
D.	For the AOA sensor:
	(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
	(2) If there is a hard point or if the AOA is bent: - Replace the related AOA sensor (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).		X
E.	For the visual icing indicator:
	(1) Make sure that it is not damaged.	X
F.	For the ice detector (if installed):
	(1) Make sure that it is not damaged.	X
2.	Close the circuit breaker(s) given in the next paragraph.	X

Subtask 05-51-14-210-074-B ** ON A/C NOT FOR ALL

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

N. Inspection of the Probes & Sensors

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	If you found signs of bird strike or damage on: - 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 detector (if installed) Or on the adjacent structure: do the inspections of the related item(s).
A.	For the: - LH pitot probe 1 or - LH pitot probe 3 or - LH static probes 1 and 2 or the LH standby static probe 3:
	(1) Do an inspection of the pitot probe (Ref. AMM TASK 34-13-00-200-001).	X
	- If the pitot probe is bent, replace it (Ref. AMM TASK 34-11-15-000-001) and (Ref. AMM TASK 34-11-15-400-001).		X
	(2) Do an inspection of the static probes and the standby static probe (Ref. AMM TASK 34-13-00-200-001).	X
	- If you find damage, replace the related probe (Ref. AMM TASK 34-11-16-000-001) and (Ref. AMM TASK 34-11-16-400-002).		X
	(3) Do a detailed structural inspection: - In the red rectangle areas around the static ports, and - In front of the red rectangle areas around the static ports.	X
	(a) 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 Structural Repair Manual (SRM). NOTE: The SRM contains the approved damage limits and repair procedures.		X
	(4) Flush the principal total pressure-lines (Ref. AMM TASK 34-10-00-170-001).	X
	(5) Drain and flush the standby static and standby total pressure- lines (Integrated Standby Instrument-System (ISIS)) (Ref. AMM TASK 34-22-25-170-001).	X
B.	For the: - RH pitot probe 2 or - RH static probes 1 and 2 or RH standby static probe 3:
	(1) Do an inspection of the pitot probe (Ref. AMM TASK 34-13-00-200-001).	X
	- If the pitot probe is bent, replace it (Ref. AMM TASK 34-11-15-000-001) and (Ref. AMM TASK 34-11-15-400-001).		X
	(2) Do an inspection of the static probes and the standby static probe (Ref. AMM TASK 34-13-00-200-001).	X
	- If you find damage, replace the related probe (Ref. AMM TASK 34-11-16-000-001) and (Ref. AMM TASK 34-11-16-400-002).		X
	(3) Do a detailed structural inspection: - In the red rectangle areas around the static ports, and - In front of the red rectangle areas around the static ports.	X
	(a) 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 Structural Repair Manual (SRM). NOTE: The SRM contains the approved damage limits and repair procedures.		X
	(4) Flush the principal total pressure-lines (Ref. AMM TASK 34-10-00-170-001).	X
	(5) Drain and flush the standby static and standby total pressure- lines (Integrated Standby Instrument System (ISIS)) (Ref. AMM TASK 34-22-25-170-001).	X
C.	For the TAT sensor:
	(1) Do an inspection of the TAT sensor (Ref. AMM TASK 34-11-18-200-002).	X
	- If the TAT sensor is clogged, replace it (Ref. AMM TASK 34-11-18-000-001) and (Ref. AMM TASK 34-11-18-400-001).		X
D.	For the AOA sensor:
	(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
	(2) If there is a hard point or if the AOA is bent: - Replace the related AOA sensor (Ref. AMM TASK 34-11-19-000-001) and (Ref. AMM TASK 34-11-19-400-001).		X
E.	For the visual icing indicator:
	(1) Make sure that it is not damaged.	X
F.	For the ice detector (if installed):
	(1) Make sure that it is not damaged.	X
2.	Close the circuit breaker(s) given in the next paragraph.	X

Subtask 05-51-14-865-061-A

O. 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/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 05-51-14-865-063-A

P. 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 05-51-14-210-075-A

Q. Inspection of the Antenna(s)

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Antenna(s)
A.	Examine the antenna(s) where you find the signs of bird strike.	X
	If it is bent, has cracks or is damaged: - Replace it.		X
B.	Make sure that the adjacent area is not damaged.	X

Subtask 05-51-14-210-076-A

R. Inspection of the Nose Landing Gear

ITEM	INSPECTION TASKS	PHASE 1
1.	Inspection of the NLG
A.	If the NLG was in transit/extended during the bird strike or there is a hole in the NLG doors:
	(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 and damaged paintwork.	X
B.	If the NLG was retracted during the bird strike:
	- Do a GVI of the external side of the NLG doors.	X

Subtask 05-51-14-210-077-A

S. Inspection of the Main Landing Gear

ITEM	INSPECTION TASKS	PHASE 1
1.	Inspection of the MLG
A.	If the MLG was in transit/extended during the bird strike or there is a hole in the MLG doors:
	(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 and damaged paintwork.	X
B.	If the MLG was retracted during the bird strike:
	- Do a GVI of the external side of the MLG doors.	X

Subtask 05-51-14-210-078-B ** ON A/C NOT FOR ALL

T. Inspection of the Engines and/or Nacelles

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Nacelles
A.	Externally examine for distortion, dents, delamination, cracked or flaking paint, loose rivets and signs of shearing: - 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.	X
	If you find damage:
	(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). If you find signs of a bird strike or damage on: - The rear side of the fan blades or - The fan Outlet Guide Vanes (OGV) or - The internal path side of the thrust reverser C-Duct or - The inner wall of the thrust reverser (from the engine side):	X
	(1) Do a visual inspection with the LIGHT SOURCE - WHITE and the MIRROR - INSPECTION, FLEXIBLE for signs of a bird strike 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. If you find signs of a bird 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 bird 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

Subtask 05-51-14-210-078-D ** ON A/C NOT FOR ALL

T. Inspection of the Engines and/or Nacelles

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Nacelles
A.	Externally examine for distortion, dents, delamination, cracked or flaking paint, loose rivets and signs of shearing: - 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.	X
	If you find damage:
	(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 72-00-00-200-006). If you find signs of a bird strike or damage on: - The rear side of the fan blades or - The fan Outlet Guide Vanes (OGV) or - The internal path side of the thrust reverser C-Duct or - The inner wall of the thrust reverser (from the engine side):	X
	(1) Do a visual inspection with the LIGHT SOURCE - WHITE and the MIRROR - INSPECTION, FLEXIBLE for signs of a bird strike 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. If you find signs of bird 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 bird 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

Subtask 05-51-14-210-078-E ** ON A/C NOT FOR ALL

T. Inspection of the Engines and/or Nacelles

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Nacelles
A.	Externally examine for distortion, dents, delamination, cracked or flaking paint, loose rivets and signs of shearing: - The air intake - The fan cowls - The thrust reverser cowls.	X
B.	Examine the Common Nozzle Assembly (CNA) for distortion, cracks, loose rivets and signs of shearing.	X
	If you find damage:
	(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 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 CNA 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). If you find signs of a bird strike or damage on: - The rear side of the fan blades or - The fan Outlet Guide Vanes (OGV) or - The internal path side of the thrust reverser C-Duct or - The inner wall of the thrust reverser (from the engine side):	X
	(1) Do a visual inspection with the LIGHT SOURCE - WHITE and the MIRROR - INSPECTION, FLEXIBLE for signs of a bird strike 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. If you find signs of a bird 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 bird 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

Subtask 05-51-14-210-078-G ** ON A/C NOT FOR ALL

T. Inspection of the Engines and/or Nacelles

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Nacelles
A.	Externally examine for distortion, dents, delamination, cracked or flaking paint, loose rivets and signs of shearing: - The air intake - The fan cowls - The thrust reverser cowls.	X
B.	Examine the Common Nozzle Assembly (CNA) for distortion, cracks, loose rivets and signs of shearing.	X
	If you find damage:
	(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 CNA 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). If you find signs of a bird strike or damage on: - The rear side of the fan blades or - The fan Outlet Guide Vanes (OGV) or - The internal path side of the thrust reverser C-Duct or - The inner wall of the thrust reverser (from the engine side):	X
	(1) Do a visual inspection with the LIGHT SOURCE - WHITE and the MIRROR - INSPECTION, FLEXIBLE for signs of a bird strike 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. If you find signs of bird 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 bird 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

Subtask 05-51-14-210-079-A

U. Inspection of the Pylons

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Pylons
A.	Examine the pylon externally for distortion, dents, cracks, pulled or damaged fasteners and damaged paintwork.	X
	If you find damage:
	(1) Get access to and internally examine the pylon for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	(2) Examine all the components, pipes, ducts, electrical harnesses and their mounts for: . Distortions, cracks, rupture, breaks and fluid leakage.		X

Subtask 05-51-14-210-080-A

V. Inspection of the Vertical Stabilizer

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: - Dents, cracks, pulled or damaged fasteners, honeycomb delamination, core damage and damaged paintwork.	X
	If you find damage:
	(1) Get access to and internally examine at and near the damage for: - Dents, cracks, pulled or damaged fasteners, honeycomb delamination or core damage and damaged paintwork.		X
B.	Examine the spar-box external-side shells of the vertical stabilizer for scores.	X
C.	Examine all the static dischargers and retainers for damage.	X
D.	Examine the rudder and the trailing-edge access doors externally for: - Distortion, cracks, pulled or damaged fasteners, honeycomb delamination and core damage.	X
	If you find damage get access to and internally: - Examine the rudder hinge and the actuator attach fittings for distortion, cracks and damaged paintwork.		X

Subtask 05-51-14-210-081-A

W. Inspection of the Horizontal Stabilizer

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Horizontal Stabilizer
A.	Examine the leading edge and the tip fairing externally for: - Dents, cracks, pulled or damaged fasteners, honeycomb delamination, core damage and damaged paintwork.	X
	If you find damage:
	(1) Get access to and internally examine at and near the damage for cracks, distortion, pulled or damaged fasteners and damaged paintwork.		X
B.	Examine the spar-box external-side shells and the logo light of the horizontal stabilizer for scores.	X
C.	Examine all the static dischargers and retainers for damage.	X
D.	Examine the elevators and the trailing-edge access doors externally for: - Distortion, cracks, pulled or damaged fasteners, honeycomb delamination and core damage.	X
	If you find damage get access to and internally: - Examine the elevator hinge and the actuator attach fittings for distortion, cracks and damaged paintwork.		X

Subtask 05-51-14-210-082-A

X. Inspection of the Wing Leading Edge

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Wing Leading Edge
A.	Examine the area with signs of bird strike on the leading edge, the fillets and the slats for distortion, cracks and pulled or damaged fasteners.	X
	If you find damage:
	(1) Examine the leading edge section internally, at and near the damage, for distortion, cracks and pulled or damaged fasteners.		X
	(2) Examine the ducts and the related attach points for damage.		X
	(3) Examine the slat section for distortion, cracks, pulled or damaged fasteners and damaged paintwork.		X
	(4) Examine the actuators, the slat tracks and the slat-track attach points for damage.		X
	(5) Examine the slat tracks for brinelling on the roller tracks.		X

Subtask 05-51-14-210-083-A ** ON A/C NOT FOR ALL

Y. Inspection of the Wing Tip and Fence

ITEM	INSPECTION TASKS	PHASE 1
1.	Inspection of Area(s) with Signs of Bird Strike or Damage on the Wing Tip Fairings, the Navigation Lights and the Strobe Lights
A.	Examine the area(s) for distortion, cracks and pulled or damaged fasteners.	X
B.	Examine all the static dischargers and retainers for damage.	X

Subtask 05-51-14-210-083-B ** ON A/C NOT FOR ALL

Y. Inspection of the Sharklet

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspection of the Sharklet
A.	Examine the sharklet for signs of impact, cracks, and pulled or damaged fasteners.	X
	(1) If you find damage:
	(a) Do an NDT inspection for delamination, on the sharklet composite area. Refer to the NTM 511003.		X
	(b) Refer to the SRM 573123 allowable damage.		X
	If the damage is more than the SRM allowable damage:
	1_ Remove the sharklet: (Ref. AMM TASK 57-31-23-000-801).			X
	2_ Do an inspection of RIB27 (internal and external sides).			X
	3_ Contact Airbus for more instructions.			X
	4_ Install the sharklet (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 all the static dischargers and retainers for damage.	X
	If you find damage: - Replace the static dischargers (Ref. AMM TASK 23-61-41-000-001) and (Ref. AMM TASK 23-61-41-400-001). NOTE: 20% of the static dischargers can be unserviceable or missing on each wing.		X

Subtask 05-51-14-210-084-A

Z. Inspection of the Wing Main Structure

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Main Structure of the Wing and Landing Lights
A.	Examine the area with signs of bird strike or damage on the wing main structure for scores.	X
B.	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 it (Ref. AMM TASK 33-42-11-000-001) and (Ref. AMM TASK 33-42-11-400-003).		X

Subtask 05-51-14-210-085-A

AA. Inspection of the Wing Trailing Edge

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2
1.	Inspection of the Trailing Edge Falsework, the Flaps, the Ailerons and the Spoilers
A.	Externally examine the control surfaces for signs of impact, damaged paintwork, abrasions, scratches or dents, distortion, cracks and pulled and damaged fasteners.	X
	If you find damage:
	(1) Examine the falsework internally at and near the damage for distortion, cracks, pulled or torn fasteners and damaged paintwork.		X
	(2) Examine the flap carriages and the fairing for distortion and cracks.		X
	(3) Examine the flap tracks for brinelling and damage.		X
	(4) Examine the aileron servo-controls and the hinge fittings for damage.		X
	(5) If you found damage near the spoilers: - Extend the spoilers (Ref. AMM TASK 27-60-00-866-002) - Examine the spoiler actuators and the hinge fittings for damage.		X
B.	Examine all the static dischargers and retainers for damage.	X

5. Close-up
Subtask 05-51-14-410-054-A

A. 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 that you opened for this inspection.
(3) If necessary, 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) If necessary, 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 05-51-14-866-057-A

B. Retraction of the Flight Control Surfaces
(1) Retract the spoilers (if extended) (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 05-51-14-710-053-A

C. Operational Test of the Systems

NOTE: The tests below are only necessary if:

You did work on the system subsequent to the inspection for damage.
You found damage on the structure adjacent to a flight control surface.

ITEM	INSPECTION TASKS	PHASE 2
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 elevators 3 times (Ref. AMM TASK 27-34-00-710-001)	X
4.	Operate the Trimmable Horizontal Stabilizer (THS) 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) and (Ref. AMM TASK 27-84-00-710-001).	X
	NOTE: The tests below are necessary only if: - You did work on the system subsequent to the inspection for damage. - You found damage on the structure adjacent to a landing gear door.
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). NOTE: If you find damage only on the main doors of the main 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

Subtask 05-51-14-860-059-A

D. Put the Aircraft Back to its Initial Configuration
(1) Set the THS pitch-trim control-wheel to neutral.
(2) Depressurize the Green hydraulic system
(Ref. AMM TASK 29-10-00-864-001).
(3) Depressurize the Blue hydraulic system
(Ref. AMM TASK 29-10-00-864-003).
(4) Depressurize the Yellow hydraulic system
(Ref. AMM TASK 29-10-00-864-002).
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

Subtask 05-51-14-942-056-A

E. 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 NOTICE(S) from the cockpit.
(3) Remove the access platform(s).
(4) Remove the safety devices from the landing gears (Ref. AMM TASK 32-00-00-081-001).

[Rev.10 from 2021] 2026.03.31 22:51:24 UTC