ata 72 seus putos

ÃIRBUS

JOB CARD MPD-TASK :

ÃIRBUS Wm - A318/A319/A320/A321 A M M T A S K :

72-00-00-200-006 72-00-00 P B 601 ÃIRBUS

TITLE: 72-00-00-200-006-A - Inspection/Check of

Foreign Object Damage (FOD) (Bird Strike Included)

A M M T A S K : 72-00-00-200-006 72-00-00 P B 601

A/C Reg.: ALL



A M M T A S K : 72-00-00-200-006 72-00-00 P B 601

C A R D Z O N E I N T E R V A L

S K I L L A C C E S S

** ON A/C 201-299, 451-599, 601-650 MECH INSP

TASK 72-00-00-200-006-A Inspection/Check of Foreign Object Damage (FOD) (Bird Strike Included)

FIN :

** ON A/C 201-299, 451-599, 601-650

1000EM1

** ON A/C 2.01-299, 451-599, 601-650

** ON A/C 201-299, 451-599, 601-650

1000EM2

** ON A/C 201-299, 451-599, 601-650

WARNING: THERE IS A POSSIBLE HEALTH RiSK T O PERSONNEL WHO DO MAiNTENANCE TASKS AFTER A BIRD STRIKE. THE S/^FETY M E A S U R Í T S THAT F O L L O W ARE RECOMMENDED: - USE DISPOSABLE GLOVES. - USE CUT RESISTANT GLOVES OVER THE DISPOSABLE GLOVES. - USE A DISPOSABLE COVERALL I F THERE I S A RISK O F BODY CONTACT WITH THE BIRD

REMAINS (ORGANIC MATTER) DURING FEATHER COLLECTION O R ENGINE CLEANING. - DO NOT USE PRESSURIZED AIR OR WATER T O CLEAN THE PARTS WHICH WERE IN

CONTACT WITH THE BIRD. - REMOVE THE BIRD REMAINS AND P U T THEM IN A PLASTIC BAG. - DO NOT TOUCH YOUR FACE, EYES, NOSE, ETC. WITH YOUR GLOVES. - REMOVE THE GLOVES AND THE DISPOSABLE COVERALL A N D P U T 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.

NOTE: In any case, operators and maintenance personnel should comply with the recommendations of the local medicai authorities. The requirements of the relevant medicai authority take precedence over any C F M guidelines in these matters and their advice must always be sought.

EFF : o f11 DATABASE REV DATE : February 1, 2014 PRINT DATE : March 21, 2014 Local Time

AIRBUS

JOB CARD MPD-TASK :

AIRBUS Wm - A318/A319/A320/A321 AMM TASK :

72-00-00-200-006 72-00-00 PB 601 AIRBUS



AMM TASK : 72-00-00-200-006 72-00-00 PB 601

A/C Reg.: ALL



AMM TASK : 72-00-00-200-006 72-00-00 PB 601

NOTE: Parts of remains can be used to determine the bird species ingested. Contact CFM for further information.

1. Reason for the Job You must do a visual inspection and, when applicable, a borescope inspection when unwanted materiais (foreign objects) have gone into the engine.

2. Job Set-up Information

A. Fixtures, Tools, Test and Support Equipment

R E F E R E N C E QTY DESIGNATION No specific AR WARNING NOTICE(S)

B. Work Zones and Access Paneis

Z O N E / A C C E S S ZONE DESCRIPTION FOR 1000EM1 (ENGIN E-1) 437AL, 438AR, 451 AL, 452AR FOR 1000EM2 (ENGINE-2) 447AL, 448AR, 461AL, 462AR

C. Referenced Information

R E F E R E N C E DESIGNATION 71-00-00-710-008-B Power Assurance Check 71-13-00-010-040-B Opening of the Fan Cowl Doors 71-13-00-410-040-B Closing of the Fan Cowl Doors 72-21-00-210-005-A Inspection/Check of the Spinner Cone 72-21-00-210-009-A Inspection of Fan Rotor Blades Installed on the Fan Disk 72-21-00-290-003-A Borescope Inspection of the Booster Rotor Blades, Stages 2,3,4 and 5

through the Booster Inlet and Borescope Ports S03 and S05 72-23-00-210-004-A Visual Inspection of the Fan Frame Assembly 72-31-00-290-002-A Inspection of the High Pressure Compressor Rotor Assembly 72-42-00-290-005-A Inspection of the Combustion Chamber and HPT Nozzle Following a

Birdstrike/FOD (SAC engine) 72-42-00-290-005-A-01 Inspection of the Combustion Chamber and HPT Nozzle Following a

Birdstrike/FOD (DAC engine) 72-54-00-290-006-A Inspection of the Stage 4 Blades 73-21-40-210-002-A Visual Inspection of the T12 Temperature Sensor 78-30-00-081 -041-B Make the Thrust Reverser Serviceable after Maintenance 78-30-00-481-041-B Make the Thrust Reverser Unserviceable for Maintenance 78-36-00-010-040-B Opening of the Thrust Reverser Doors 78-36-00-410-040-B Closing of the Thrust Reverser Doors TSM 77-00-00-810-864 Fan Vibrations Higher than or Equal to 6 Units on Engine 1 or 2 PS3 Line SHEET 1 PS3 Line SHEET 1 SHEET 2 PS3 Line SHEET 1 SHEET 2 SHEET 3 PS3 Line SHEET 1 SHEET 2 SHEET 3 SHEET 4 PS3 Line SHEET 1 SHEET 2 SHEET 3 SHEET 4 SHEET 5

o f11 DATABASE REV DATE : February 1, 2014 PRINT DATE : March 21, 2014 Local Time:

AIRBUS

J 0 3 CARD MPD-TASK:

AIRBUS Itm - A318/A319/A320/A321 AMM TASK:

72-00-00-200-006 72-00-00 PB 601 AIRBUS

TITLE: 72-00-00-200-006-A - Inspection/Check of Foreign Object Damage (FOD) (Bird Strike

Included)

AMM TASK: 72-00-00-200-006 72-00-00 PB 601

A/C Reg.: ALL


Included)

AMM TASK: 72-00-00-200-006 72-00-00 PB 601

3. Job Set-up

Subtask 72-00-00-941-067-A

A. Safety Precautions

(1) On the center pedestal, on the ENG panei 115VU:

(a) Put a WARNING NOTICE(S) to tell persons not to start the engine.

(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.

(3) On the overhead maintenance panei 50VU:

(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.

(b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).

Subtask 72-00-00-010-074-A

B. Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-040):

(1) FOR TÒ00EM1 (ENGINE-1) 437AL, 438AR

(2) FOR 1000EM2 (ENGINE-2) 447AL, 448AR

Subtask 72-00-00-040-059-A

C. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041) .

Subtask 72-00-00-010-079-A

D. Open the thrust reverser doors (Ref. AMM TASK 78-36-00-010-040) :

(1) FOR 1000EM1 (ENGINE-1) 451AL, 452AR

(2) FOR 1000EM2 (ENGINE-2) 461 AL, 462AR ,

4. Procedure

Subtask 72-00-00-210-062-A

A. Visual Inspection

NOTE: Visual inspection must be done without part renovai. Refer to the hereafter referenced tasks to find the inspection criteria and apply these criteria only on the visible parts.

(1) Possible damage to the spinner front and rear cones (Ref. AMM TASK 72-21-00-210-005).

(2) General condition of the fan rotor blades (Ref. AMM TASK 72-21-00-210-009).

(3) Wearof abradable material in fan inletcase (Ref. AMM TASK 72-23-00-210-004) .

(4) Condition of acoustical paneis that may have been damaged as a result of interference with blade tip (Ref. AMM TASK 72-23-00-210-004) .

(5) Condition of splitter fairing and booster inlet guide vanes (IGV) (Ref. AMM TASK 72-23-00-210-004) and (Ref. AMM TASK 72-21-00-210-005) .

EFF : of 11 DATABASE REV DATE : February 1, 2014 PRINT DATE : March 21, 2014 Local Time

AIRBUS

JOB CARD MPD-TASK :

AIRBUS WRt - A318/A319/A320/A321 AMM TASK :

72-00-00-200-006 72-00-00 PB 601 AIRBUS


Included)

AMM TASK : 72-00-00-200-006 72-00-00 PB 601

A/C Reg.: ALL


Included)

AMM TASK : 72-00-00-200-006 72-00-00 PB 601

(6) Condition of fan outiet guide vanes (OGV) and seals of fan OGV inner shroud (Ref. AMM TASK 72-23-00-210-004) .

(7) Damage to T12 sensor probe (Ref. AMM TASK 73-21-40-210-002) .

Subtask 72-00-00-220-172-A

B. Condition of Exhaust and Stage 4 Low Pressure Turbine (LPT) Blades

(1) Do a visual inspection thru the exhaust nozzle of the LPT stage 4 blades for shingling or damage.

(a) If stage 4 LPT blades unlatch condition or other indication is found, do a borescope inspection of the stage 4 LPT blades (Ref. AMM TASK 72-54-00-290-006) .

Subtask 72-00-00-280-057-A

C. Gaspath Inspection

(1) FOD associated with normal engine parameters.

NOTE: The borescope inspection may be delayed 25 flight hours or 10 flight cycles (whichever ** comes first) provided FOD did not result in missing material to the fan blades. Service

extension is only permitted on one engine in the event of a dual engine FOD.

(a) Do the step that follows if one or more of these conditions apply: - FOD event has resulted in fan blade missing material/fan blade damage beyond serviceable

limits. - FOD event struck fan blades radially inwaid of mid span shroud. - Evidènce of debris has entered the booster inlet ie: damage or debris on spinner front and

rear cones, stage 1 booster vane or splitter fairinq.

1 Do a borescope inspection of the HPC stages 1, 3 and 8 (Ref AMM TASK 72-31-00-290-002) .

2 If damage is found inspect the other stages (Ref. AMM TASK 72-31-00-290-002).

3 Do a borescope of the combustion chamber dome assembly after a bird strike/ingestion event (Ref. AMM TASK 72-42-Ç0-290-005) .

4 If the engine is PRE C F M S B 72-0418, do a borescope inspection of the stage 5 booster blades (Ref. AMM TASK 72-21-00-290-003) . Examine carefully the concave and convex sides of stage 5 booster blades in area E.

** ON A/C 201-299, 451-599, 601-650

(Ref. Fig. PS3 Line SHEET 1) (Ref. Fig. PS3 Line SHEET 1 SHEET 2) (Ref. Fig. PS3 Line SHEET 1 SHEET 2 SHEET 3) (Ref Fig. PS3 Line SHEET 1 SHEET 2 SHEET 3 SHEET 4) (Ref. Fig. PS3 Line SHEET 1 SHEET 2. SHEET 3 SHEET 4 SHEET 5)

** ONA/C 201-299, 451-599, 601-650

Examine carefully blades around blade locks area.

(2) FOD associated with abnormal engine parameters.

EFF : o f11 DATABASE REV DATE : February 1, 2014 PRINT DATE : March 21, 2014 Local Time

AIRBUS

JOB CARD MPD-TASK:

AIRBUS W* - A318/A319/A320/A321 AMM TASK:

72-00-00-200-006 72-00-00 PB 601 AIRBUS TITLE:

72-00-00-200-006-A - Inspection/Check of Foreign Object Damage (FOD) (Bird Strike

Included)

AMM TASK: 72-00-00-200-006 72-00-00 PB 601

A/C Reg.: ALL


Included)

AMM TASK: 72-00-00-200-006 72-00-00 PB 601

(a) If ECAM warnings "FAN VIB HIGHER THAN OR EQUAL TO 6 UNITS AND LOWER THAN 8 UNITS" or "FAN VIB HIGHER THAN OR EQUAL TO 8 UNITS" are displayed TSM 77-00-00-810-864.

(b) If FOD event was associated with abnormal parameters or with surge, or stall or flameout, do the steps which follow:

NOTE: Abnormal engine parameters mean a mismatch or significant shift on N2, WF, or EGT as well as abnormal accel and decel.

1 Do a borescope inspection of the booster (Ref. AMM TASK 72-21-00-290-003). - If the engine is PRE CFM SB 72-0418, do a borescope inspection of the stage 5 examine

carefully the concave and convex sides of stage 5 booster blades in area E ** ON A/C 201-299, 451-599, 601-650

(Ref. Fig. PS3 Line SHEET 1) (Ref. Fig. PS3 Line SHEET 1 SHEET 2) (Ref. Fig. PS3 Line SHEET 1 SHEET 2 SHEET 3) (Ref. Fig. PS3 Line SHEET 1 SHEET 2 SHEET 3 SHEET 4) (Ref. Fig. PS3 Line SHEET 1 SHEET 2 SHEET 3 SHEET 4 SHEET 5)

** ON A/C 201-299, 451-599, 601-6M and blades around blade locks area.

2 Do a borescope inspection of the HPC stages 1, 3 and 8 (Ref. AMM TASK 72-31-00-290-002) .

3 If damage is found inspect the other stages (Ref. AMM TASK 72-31-00-290-002).

4 Do a borescope inspection of the combusfion chamber dome area (Ref. AMM TASK 72-42-00-290-005) .

5 D o a Maximum Power Assurance check [Rei AMM TASK 71-00-00-710-008) .

Subtask 72-00-00-210-063-A

D. FOD (Included Birdstrike) Inspection

NOTE: Before this inspection, perform steps 4.A 4.B and 4.C.

(1) Examine the externai portions of tfre nacelle inlet at the point of impact and look for:

(a) Cracks.

(b) Signs of distortion.

(c) Loose or missing fasteners.

(2) Examine the inlet cowl structure for secondary damage and look for:

(a) Cracks.

(b) Signs of distortion.

(c) Delamination.

(d) Loose or missing fasteners.

(3) Examine all open ports in the inlet and look for:

(a) Blockage. (4) If the FOD went through the inlet cowl structure, look for:

o f11 SE R B V D A T E F e b r u a r y 1. 2 0 1 4 .

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