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MAINTENANCE PRACTICE TRAINING MANUALB1 ou B1/B2

DERICHEBOURG Atis aronautique,Parc Algorithmes, Immeuble Thals 17, Avenue Didier Daurat 31700 Blagnac

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TRAINEE

SURNAME: Forename:

Licence number:

Experience on an aircraft with similar technology: YESNO

Signature: Date : / /

ON JOB TRAININGType of training: A318/319/320/321 CFM56

A319/320/321 IAE V2500

Type: B1 B1/B2

Starting date : / / Ending Date : / /

Performed at :

DERICHEBOURG ATISARONAUTIQUE STAMP :

PRACTICAL ASSESSORSLicence

number/StampNAME Signature Date

Validation by Quality Department:

Date: Name: Signature:

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SUBJECTThe aim of this document is to record all the practical tasks performed by engineers within ATIS

Aviation, PART 145 FR.145.107 approved maintenance organisation, in order to comply with therequirements of Appendix III of PART 66 to have the B1 or B1/B2 rating on A318/319/320/321CFM56 or/and 319/320/321 IAE V2500 aircraft.

Any task performed in the frame of this On Job Training (OJT) will have to be signed by thetrainee engineer and validated by assessors. This OJT will be performed under the responsibilityof one or more B1 or B1/B2 qualified engineers. (See PRE-REQUISIT on page 4/38)

After this training, the engineer will be able to:- perform verifications of systems, engines, components and operational functions such as

specified in the maintenance manual,- analyse all information in order to make decisions regarding trouble shooting and corrective

actions as per maintenance manual,- describe the component replacement procedures specific to aircraft type.

DURATION- Engineer with B1 or B1/B2 rating and six month experience on an aircraft with a similartechnology: 70 hours(1),

- Engineer with B1 or B1/B2 rating and less than six month experience on an aircraft with asimilar technology: 140 hours(1),

- Engineer with no B1 or B1/B2 rating on an aircraft with a similar technology: four months.(1)The 70/140 hours do not have to be necessarily performed in a row, but can be extended on a period adapted tooperational configuration (availability of aircraft, trainee and assessors).

CLASSIFICATIONClassifies the importance of a task for the completion of the practical training record.Following classifications are used:- Mandatory (M): This indicates that the related task is required for completion of the

practical training record.

- Optional (O): This indicates that the related task is optional. It is recommended toperform at least 70% of those tasks in each ATA chapter.

TASKS CODES- FOT: Functional Operational Test(*)- LOC: Location and identification of system components- MEL: Minimum Equipment List items requiring a maintenance procedure- RIA: Removal Installation Activation- OPC: Operational Check- SGH: Servicing Ground Handling- TSE: Trouble shooting Exercise- TVC: Carry out Thorough Visual Check

- TPR: Thorough Procedural review(*)If ground power or other applicable systems are unavailable a TPR will be carried out in place of a FOT.

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SIGNING OFF THE TASKSPart 66 Appendix 3 paragraph 2.2 requires that the practical training element must consist of theperformance of representative tasks and their assessment, in order to meet the followingobjectives:

a) Ensure safe performance of maintenance, inspections and routine work according to themaintenance manual and other relevant instructions and tasks as appropriate for the typeof aircraft, for example troubleshooting, repairs, adjustments, replacements, rigging andfunctional checks such as engine run, etc, if required,

b) Correctly use all technical literature and documentation for the aircraft,

c) Correctly use specialist/special tooling and test equipment, perform removal andreplacement of components

The nominated trainer/assessor will sign off each task when satisfied that the trainee hasattained the demonstrable level of understanding that is required.

PRE-REQUISITThe trainee must have participated and succeeded in a PART 147 theoretical type rating training(T1/T2 training).

The assessors must have an experience of five years in the line maintenance and two years inthe qualification of type.For any OJT, the assessors will have to make a request by email at the Quality Department forvalidation of pre-requisit.

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Item Ref. ATA Ref. Subject Class B1/B2TaskCode

DateTrainee'ssignature

Instructor'ssignature

U05-00-00 - TIME LIMITS / MAINTENANCE CHECKS U

05-001 05-00-00 Daily check M TVC

05-002 05-50-00 Weekly check M TVC

05-003 05-51-11 Walk around check M TVC

U09-00-00 - TOWING&TAXINGU

09-001 09-00-00Towing points/steeringangle limitation

M SGH

U10-00-00 - PARKING AND MOORING U

10-001 10-00-00 Landing gear loking pins M SGH

10-002 10-00-00 Engine / airframe blanging O SGH

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U12-00-00 - SERVICINGU

12-001 12-11-28Automatic refuel/defuelprocedures

M SGH

12-001 12-11-28Presure Refuel underManual Control

M FOT

12-003 12-11-28Magnetic Fuel Quantityindicators reading

O SGH

12-004 12-12-29Reservoirs refiling withhand pump

M SGH

12-005 12-13-24Electrical power servicing(IDG)

M SGH

12-006 12-13-49 APU servicing M SGH

12-007 12-13-0 Engine starter servicing O SGH

12-008 12-14-29 Accumulators filing O SGH

12-009 12-14-32

Landing gear gas servicing

procedure using chart O SGH

12-010 12-15-38 Potable water servicing M SGH

12-011 12-16-38 Lavatory servicing M SGH

12-012 12-34-24 Aircraft grounding M SGH

REMARKS :

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U21-00-00 AIR CONDITIONNING U

21-001 21-00-00ECS/Aircon controls I &indications int he cockpit

M LOC

21-002 21-00-00Aircon. System,components

M LOC

21-003 21-00-00Aircon. System - Defectsrectification & TIS

M TSE

21-004 21-21-00Operational test of CabinRecirc Fans

M FOT

21-005 21-21-41 Recirculation filter M LOC

21-006 21-26-00Deact/reactivation ofavionics vent components

O MEL

21-007 21-26-00Avionics smokeconfiguration control circuit

O FOT

21-008 21-26-00Operational test of theAvionics Eqpt Ventilationfrom the MCDU

O FOT

21-009 21-26-00 Avionics Equipt Ventilationsyst Test (No CFDS)

O FOT

21-010 21-26-00 AEVC M RIA

21-011 21-26-43 Avionics vent demister filter M RIA

21-012 21-28-00Cargo compartmentventilation system

O FOT

21-013 21-28-00Deact/reactivation of cargocompt. vent. Isol. valve

O MEL

21-014 21-31-00Manual pressure control &

monitoring system

O FOT

21-015 21-31-00Operational Test of thePressure Control andMonitoring System

M FOT

21-016 21-43-00Test of the AFT CGOcompartement HeatingSystem

M FOT

21-017 21-51-00Pack flow control &indicating

M FOT

21-018 21-51-00Deact. / reactivation of packflow contrl valve

O MEL

21-019 21-55-00 Emergency ram air inlet M FOT

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21-020 21-61-00Operational test of Packtemp. Control. System

M FOT

21-021 21-63-00Deact. / reactivation of trimair & hot air valves

O MEL

21-022 21-63-00Functional test of cockpit /temperature control

M FOT

21-023 21-63-17 Cabin temperature sensors M RIA

REMARKS :

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U22-00-00 AUTO FLIGHT

22-001 22-00-00AFS controls andindications in cockpit

M LOC

22-002 22-00-00AFS controls andindications in cockpit

M LOC

22-003 22-10-00A/P disengagement andlocking devices

O FOT

22-004 22-60-00 Windshear procedure M MEL

22-005 22-61-00Rudder travel limitingfunction

M FOT

22-006 22-62-00Rudder trim function testand reset

M FOT

22-007 22-63-00 Yaw damper function M FOT

22-008 22-66-00 FAC M RIA

22-009 22-70-00FM Navigation databaseloading

O SGH

22-010 22-70-00 FM MCDU menu Data entry M SGH

22-011 22-70-00Flight plan initializationprocedure

M SGH

22-012 22-81-00 FCU M RIA

22-013 22-82-12 MCDU M RIA

22-014 22-91-00 AFS Ground Scanning test M FOT

22-015 22-97-00AFS land CAT3 capabilitytest M FOT

REMARKS :

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U23-00-00 COMMUNICATION

23-001 23-00-00Com. System controls andindic. In the cockpit

M LOC

23-002 23-00-00 Com. System components M LOC

23-003 23-00-00Com. System - Defectrectification & TIS

M TSE

23-004 23-00-00 Com. System components M TSE

23-005 23-12-00VHF communication systemoperation

O FOT

23-006 23-12-00 VHF system BITE test M FOT

23-007 23-13-00 RMP BITE test M FOT

23-008 23-32-00 PRAM M RIA

23-009 23-32-00 PRAM Tape M RIA

23-010 23-32-00 PRAM initialization M SGH

23-011 23-44-00Service interphone /Mechanic call

O FOT

23-012 23-51-00Audio managementoperational test

O FOT

23-013 23-51-00 ACP switching M FOT

23-014 23-51-12 ACP M RIA

23-015 23-51-00 AMU / ACP BITE test O FOT

23-016 23-71-00 CVR Mic Amplifer O RIA

23-017 23-71-00 CVR M RIA

23-018 23-73-00Cabin and flight crewinterphone (CIDS)

O FOT

23-019 23-73-00CIDS energizing / de-energizing & BITE

O FOT

23-020 23-73-00

FAP and PTP general

operation M FOT

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23-021 23-73-00Cabin Layout and zoneprogramming

M SGH

23-022 23-73-00CIDS system test throughMCDU

M FOT

23-023 23-73-00 CIDS Director M RIA

23-024 23-73-00 DEU A / DEU B M RIA

REMARKS :

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U24-00-00 - ELECTRICAL POWER.N.B. : SERVICING tasks p lease refer to ATA 12-00-00 Chapter

24-001 24-00-00Electrical power controls &ind. In the cockpit

M LOC

24-002 24-00-00Electrical power systemcomponents

M LOC

24-003 24-00-00Electrical system defectsrectification & T/S

M TSE

24-004 24-20-00Deact/Reactivation RATextension control

M MEL RIA

24-005 24-20-00Deact / Reactivation Enginedriven generator

M MEL RIA

24-006 24-22-55 GLC-BTC contactors M RIA

24-007 24-24-00Emergency generationsystem

M FOT

24-008 24-24-00 Emergency generator GCU M FOT

24-009 24-26-00Galley manual an automaticshedding O FOT

24-010 24-28-00 Static inverter test M FOT

24-011 24-30-00Deact / Reactivation of aBCL

O MEL

24-012 24-32-00TR reset via CFDS andfrom panel 103 VU

O FOT

24-013 24-38-00 Battery charge limiter M FOT

24-014 24-41-00External powercontrol/GPCU function

M FOT

24-015 24-41-00Energize a/c electricalnetwork form ext. Power

M FOT

24-016 24-41-00De-Energize a/c electricalnetwork from ext. Power

M FOT

24-017 24-41-34 gpcu (or GAPCU) M RIA

24-018 24-42-00Energize the ground servicenetwork

M FOT

24-019 24-56-00Deact./React. Of Galleysupply system

M MEL

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24-020 24-56-00 Galley supply contactors M RIA

REMARKS :

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U25-00-00 EQUIPMENT AND FURNISHING.

25-001 25-00-00Equipment & furnishingcomponents location

M LOC

25-002 25-11-00 Crew seats M FOT

25-003 25-11-00 3rd occupant seat M RIA

25-004 25-21-00Passenger convertibleseats

O SGH

25-005 25-23-00 Ceiling panels M RIA

25-006 25-23-00 Cove light panels M RIA

25-007 25-25-00PSU / PIU / cove lightpanels

M RIA

25-008 25-35-00 Galley equipment O SGH

25-009 25-00-00

Check of pressure at door

escape slides (no CIDS) O TVC

25-010 25-50-00 Cargo loading system O FOT

25-011 25-53-00Drainage cargocompartment

O SGH

25-012 25-62-00 Doors escape slides M RIA

25-013 25-62-00 Over wing escape slide O RIA

REMARKS :

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U26-00-00 FIRE PROTECTION.

26-001 26-12-00Fire protection controls &ind. In the cockpit

M LOC

26-002 26-12-00Fire protection systemcomponents

M LOC

26-003 26-12-00Fire protection systemdefect rectification & T/S

M TSE

26-004 26-12-00Engine fire detectionsystem test

M FOT

26-005 26-13-00APU fire detection systemtest

M FOT

26-006 26-15-00Avionics compartmentsmoke detection

O FOT

26-007 26-16-00LDCC Smoke DetectionTest using PTT

M FOT

26-008 26-17-00Test of Lavatory SmokeDetection System

M FOT

26-009 26-17-00 SDCU M RIA

26-010 26-22-00APU auto fire extinguishing& APU LP fuel valve

M FOT

26-011 26-23-00Cargo compartment fireextinguishing system

M FOT

REMARKS :

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U27-00-200. FLIGHT CONTROL

27-001 27-00-00Flight control componens &ind. In the cockpit

M LOC

27-002 27-00-00 Flight control components M LOC

27-003 27-00-00Flight control systemdefects rectification & T/S

M TSE

27-004 27-14-00Deactivation / reactivationof aileron servo control

M MEL

27-005 27-14-00Aileron servo controlactuation

M FOT

27-006 27-21-00 Rudder centering spring rod M FOT

27-007 27-22-00 Rudder trim reset function M FOT

27-008 27-23-00Operational test of ruddertravel limitation unit

O FOT

27-009 27-24-00

Test of Rudder SC with

individual Hyd System M FOT

27-010 27-34-00 Elevator sytem M FOT

27-011 27-41-00THS system test-using trimwheels

M FOT

27-012 27-44-51THS : check of no-backwear indicator

O TVC

27-013 27-44-51THS : inspection of gearboxmagnetic chip detector

O TVC

27-014 27-50-00Extending / retracting Flaps& Slats

M FOT

27-015 27-51-00Wingtip brake and pressureoff brake : eng & reset

M FOT

27-016 27-51-00SFCC (Flap system) BITEtest

M FOT

27-017 27-51-00Automatic Integrity Test ofSFCC

M FOT

27-018 27-51-00 S/F control lever M RIA

27-019 27-60-00Ground spoilermaintenance device

M SGH

27-020 27-64-00

Deactivation / reactivation

of spoiler actuator M MEL

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27-021 27-81-00SFCC (slat system) BITEtest

M FOT

27-022 27-81-00 Slat WTB and POB test O FOT

27-023 27-94-00 SEC M RIA

27-024 27-96-00EFCS BITE (GroundScanning) test

M FOT

27-025 27-96-00Ability of ELAC and SEC tocontrol Elevators SC M FOT

27-026 27-96-00Test of the Side StickAssembly

O FOT

27-027 27-96-00Test of the DampingMeasurement (Aileron)

M FOT

27-028 27-96-00Test of the DampingMeasurement (Elevator)

M FOT

27-029 27-96-00 FCDC M RIA

REMARKS :

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U28-00-00. FUELN.B. : For SERVICING tasks please refer to ATA 12-00-00 Chapter

28-001 28-00-00Fuel system control &indications in the cockpit

M LOC

28-002 28-00-00 Fuel system components M LOC

28-003 28-00-00Fuel system defectsrectification & T/S

M TSE

28-004 28-11-00 Water drain system M SGH

28-005 28-12-00Tank venting overpressureprotector

M MEL

28-006 28-15-00Transfer Valves IndividualOperational

O FOT

28-007 28-15-00 Transfer Valves actuator M RIA

28-008 28-21-00 Wing-tank fuel control test O FOT

28-009 28-22-00Bleed APU fuel line fromAPU O FOT

28-010 28-24-00Engine LP fuel shut-offvalve

M FOT

28-011 28-25-00 Defuel /Transfer operations O SGH

28-012 28-25-00Deact/reactivation of refuelvalve (Manual refuel)

O MEL

28-013 28-25-00Deact/reactivation oftransfer defuel valve

O MEL

28-014 28-40-00Deact/reactivation of APULP valve & X-feed valve

O MEL

28-015 28-42-00 FQIC Status Report (BITE) O FOT

28-016 28-42-00 FQIC M RIA

28-017 28-43-00Determination of fuel levelusing M.L.I

O SGH

28-018 28-46-00Tank High Level SensingSystem

M FOT

28-019 28-46-00 FLSS Functional (BITE) test M FOT

28-020 /

Fuel Tank Safety / CDCCL

awareness M TPR

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U29-00-00. HYDRAULIC POWERN.B. : For SERVICING tasks please refer to ATA 12-00-00 Chapter

29-001 29-00-00Hydraulic sytem controls &Ind. In the cockpit

M LOC

29-002 29-00-00Hydraulic systemcomponents & servicepanels

M LOC

29-003 29-00-00

Hydraulic power defects

rectification & T/S M TSE

29-004 29-10-00Press/depressurize Bluehydraulic system (usingelectric pump)

M FOT

29-005 29-12-00Blue hyd. Sys. Electricpump phase unbalancedetector

M FOT

29-006 29-14-00 Reservoir pressurization O SGH

29-007 29-17-00Collector tanks seal drainsystem

O SGH

29-008 29-22-00 RAT Auto Deployment Test M FOT

29-009 29-23-00

Pressurize/ depressurisegreen hydraulic systemfrom yellow hydraulicsystem through PTU usingelectric pump

M FOT

29-010 29-23-00PTU isolation couplingdisconnection reconnection

M SGH

29-011 29-31-00Deact./reactivation ofhydraulic fluid quantity ind.

M MEL

29-012 29-34-00Deact./reactivation ofreservoir pressurization ind.

M MEL

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U30-00-00. ICE AND RAIN PROTECTION

30-001 30-00-00Anti-ice system controls &ind. In the cockpit

M LOC

30-002 30-00-00Anti-ice systemcomponents

M LOC

30-003 30-00-00Anti-ice system defectsrectification & T/S

M TSE

30-004 30-11-00Wing ice protection :deact/react of anti-icecontrol valve

M MEL

30-005 30-11-00Wing ice protection groundtest

M FOT

30-006 30-21-00Deact/reactivation of engineanti-ice valve

O MEL

30-007 30-31-00Check of probe heatingchannel

M MEL

30-008 30-31-00 Probe ice protectionoperational test

O FOT

30-009 30-31-00 PHC M RIA

30-010 30-42-00Windshield anti-icing anddefogging operational test

O FOT

30-011 30-42-00 WHC M RIA

30-012 30-71-00Deact/reactivation of Wastewater drain mast heating

O MEL

REMARKS :

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U31-00-00. INDICATING/RECORDING

31-001 31-00-00System controls andindications int he cockpit

M LOC

31-002 31-00-00Indicating/recording systemcomponents

O LOC

31-003 31-00-00Indicating/recording syst,Deects rectification & T/S

M TSE

31-004 31-21-00 Electrical clock M RIA

31-005 31-21-00 Electrical clock setting M SGH

31-006 31-32-00CFDS general operation,TS & Class 3 faults reading

M FOT

31-007 31-32-00 CFDIU Bite Test O FOT

31-008 31-32-00 Uploading of CFDS filter O SGH

31-009 31-32-00

Activation/Deact. Of PFR

filter O SGH

31-010 31-33-00FDIU fault monotoring Testvia MCDU

M FOT

31-011 31-33-00 OAR disk (if installed) M RIA

31-012 31-35-00 Printer operation O SGH

31-013 31-35-22 Printer servicing M SGH

31-014 31-35-00 Printer M RIA

31-015 31-36-00AIDS general operation &parameter call-up menus

M FOT

31-016 31-36-00 Print Out of Stored Report O SGH

31-017 31-36-00 Test of DMU M FOT

31-018 31-36-00Update APU Hours andCycles into DMU

M SGH

31-019 31-36-00 DMU M RIA

31-020 31-60-00

EIS (EFIS/ECAM) start /

stop procedure M FOT

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31-021 31-60-00EFIS/ECAM switchingfunctions

M FOT

31-022 31-60-00 EIS system test/display test O FOT

31-023 31-60-00 EIS input test O FOT

31-024 31-63-00 Display Unit M RIA

REMARKS :

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U32-00-00. LANDING GEARN.B : For SERVICING tasks please refer to ATA 12-00-00 Chapter

32-001 32-00-00Landing gear systemcontrols & Ind. Int thecockpit

M LOC

32-002 32-00-00MLG/NLG/MWS and wheelwell components

M LOC

32-003 32-00-00

Ldg Gear defects

rectification & T/S M TSE

32-004 32-11-00

In-Situ explanation of MLGshock absorber spare sealactivating valve andmaintenance practices

O SGH

32-005 32-12-00Maint landing gear doorsground opening & closing

M SGH

32-006 32-22-00Nose landing gear doorsground opening & closing

M SGH

32-007 32-31-00 LGCIU M RIA

32-008 32-41-00 Main nose wheel removal M RIA

32-009 32-42-00Bleeding o brake system &reset of safety valve

O SGH

32-010 32-42-00Deact/reactivation of mainwheel brakes

M MEL

32-011 32-42-00 Normal brake system test O FOT

32-012 32-42-00 Brake unit removal O RIA

32-013 32-44-00Alternate braking with &without antis kid

M FOT

32-014 32-45-00Parking / ultimateemergency braking

M FOT

32-015 32-45-00Release of parking brakepressure

O SGH

32-016 32-46-00BSCU BITE Test andGNDSCAN selection

M FOT

32-017 32-47-00Deact./reacivation of braketemperature sensor

O MEL

32-018 32-49-00TPIS BITE test CFOSprocedure (if installed)

O FOT

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32-019 32-51-00Nose wheel steeringoperational test (CFOS)

M FOT

32-020 32-61-00 LDG NOT DOWN test O FOT

32-021 32-69-00BITE test of the landinggear

M FOT

32-022 32-69-00Simulation of flight, aircrafton ground

O FOT

REMARKS :

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U33-00-00. LIGHTS

33-001 33-00-00Light controls & ind. In thecockpit

M LOC

33-002 33-00-00Light controls & ind. In thecabin

M LOC

33-003 33-00-00 Light components M LOC

33-004 33-10-00Bulb replacement of pushbutton switches

M RIA

33-005 33-10-00Cockpit general illumination& Integral lighting

M FOT

33-006 33-14-00Annuciator light test &dimming

M FOT

33-007 33-21-00 Cabin general illumination M FOT

33-008 33-21-00 Cabin lights M RIA

33-009 33-24-00 Lavatory lighting O FOT

33-010 33-25-00 Passenger reading lights O FOT

33-011 33-25-00 Passenger reading lights M RIA

33-012 33-26-00 Lavatory lighted signs O FOT

33-013 33-27-00 Cabin attendant work light O FOT

33-014 33-30-00 Cargo and services lights O FOT

33-015 33-35-00Equipment compartmentlighting

O FOT

33-016 33-40-00 Exterior lights M FOT

33-017 33-41-00 Navigation lights O FOT

33-018 33-51-00 Emergency light test M MEL

33-019 33-51-00Emergency lighting throughPTP

O FOT

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33-020 33-51-00EMER LIGHT SVS fromcockpit and FAP

M FOT

33-021 33-51-00EMER escape path markinglights

M FOT

33-022 33-51-00 EPSU M RIA

REMARKS :

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U34-00-00. NAVIGATION

34-001 34-00-00Navigation system controls& ind. In the cockpit

M LOC

34-002 34-00-00Navigation systemcomponents

M LOC

34-003 34-00-00Navigation system - Defectrectification & T/S

M TSE

34-004 34-10-00ADIRS start / stopprocedure

M SGH

34-005 34-10-00 IR alignment procedure M SGH

34-006 34-13-00 ADR BITE / interface test O FOT

34-007 34-14-00 IR BITE / interface test O FOT

34-008 34-11-00 ADM M RIA

34-009 34-13-00

ALTICAS dynamic slew

tests O FOT

34-010 34-36-00 ILS (MMR) BITE test O FOT

34-011 34-41-00Weather radar BITE test(Safety precautions)

M FOT

34-012 34-42-00 Radio altimeter BITE test O FOT

34-013 34-42-00 Radio altimeter ramp test O FOT

34-014 34-43-00 TCAS BITE test (if installed) O FOT

34-015 34-48-00GPWS/EGPWS (asinstalled)

M FOT

34-016 34-48-00 GPWC M RIA

34-017 34-58-00Satellite navigation system(GPS) (if installed)

M FOT

34-018 34-58-00 GPSSU M RIA

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U35-00-00. OXYGEN

35-001 35-00-00Oxigen system controls &ind. In the cockpit

M LOC

35-002 35-10-00Cockpit and cabin oxygensystem components

M LOC

35-003 35-10-00Crew oxygen systempressure indication-check

M FOT

35-004 35-10-00Crew oxygen system FullFace Mask test

M FOT

35-005 35-10-02Pressure check crewoxygen cylinder

M TVC

35-006 35-11-00Crew oxygen storagecylinder

O RIA

35-007 35-21-00Open cabin emergcontainer door with manual

O FOT

35-008 35-21-00 Emergency oxygen cylinder M RIA

35-009 35-21-00

Emergency oxygen

container O RIA

35-010 35-31-00Indicator check of thetamper seasl on smokehood

O TVC

REMARKS :

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U36-00-00. PNEUMATIC

36-001 36-00-00Pneumatic system controls& ind. In the cockpit

M LOC

36-002 36-00-00Pneumatic systemcomponents

M LOC

36-003 36-00-00Bleed air supply system -Defect rectification & T/S

M TSE

36-004 36-00-00Pressurization of pneumaticsystem

M FOT

36-005 36-11-00 BMC BITE test O FOT

36-006 36-11-00Deact/ractivation of bleedpress. Reg. Valve (PRV)

M MEL

36-007 36-11-00Deact/reactivation of HPbleed valve

O MEL

36-008 36-11-00CFDS bleed air supplucurrent status readout

M FOT

REMARKS :

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U38-00-00. WATER:WASTE SYSTEMN.B : For SERVICING tasks please refer to ATA 12-00-00 Chapter

38-001 38-10-00Water /waste systemcomponents

M LOC

38-002 38-10-00Pressurization of potablewater tank

O SGH

38-003 38-10-00 Water filter (Galley) O RIA

38-004 38-12-00Functional test of the watersystem

O FOT

38-005 38-12-00functional test/reset of thewater heater

O FOT

38-006 38-13-00Water quantity indicatingsystem test

M FOT

38-007 38-31-00Vacuum toilet systemBITE/test

O FOT

38-008 38-31-00 VSC M RIA

REMARKS :

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U49-00-00. APUN.B : For SERVICING tasks please refer to ATA 12-00-00 Chapter

49-001 49-00-00APU controls & indicationsin the cockpit

M LOC

49-002 49-00-00APU - Defect rectification &T/S

M TSE

49-003 49-00-00

APU start/shutdown

49.004.49-0-00 ECB selftest

M SGH

49-004 49-00-00 ECB self test M FOT

49-005 49-32-11Fuel filter diff. Press.Indicator check

M TVC

49-006 49-62-00APU emergency shut downtest

O FOT

REMARKS :

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U52-00-00. DOORS

52-001 52-00-00 Door indication on ECAM M LOC

52-002 52-10-00Opening / closing &precautions

M FOT

52-003 52-10-00Escape slide disarmingwhen opening from outside

M FOT

52-004 52-21-00Over wing emergency exitsdisarming (A319/A320)

M FOT

52.005 52-21-00Over wing emergency exits(A319/A320)

M RIA

52-006 52-30-00Cargo doors operation withelectric

M FOT

52-007 52-30-00Cargo doors operation withhand pump

O FOT

52-008 52-30-00Deact/reactivation of cargodoor actuators

O MEL

52-009 52-33-00

Bulk cargo door operation

(if installed) O SGH

REMARKS :

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U53-00-00. FUSELAGE

53-001 53-10-00Opening / closing of theradome

O SGH

53-002 53-10-00Radome inspection fordamage

O TVC

REMARKS :




U54-00-00. NACELLE / PYLONS

54-001 54-50-00 Pylon pressure relief door M LOC

REMARKS :




U56-00-00. WINDOWS

56-001 56-10-00Cleaning of windshield andwindows O SGH

56-002 56-12-00Operation of cockpit slidingwindows

M FOT

REMARKS :

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U71-00-00. POWER CFM 56

71-001 71-00-00 Power Plant components M LOC

71-002 71-00-00Power Plant defectrectification & T/S

M TSE

71-003 71-00-00Opening & closing ofengine cowlings

M SGH

71-004 71-00-00DRY/Wet motoring ofengine

M FOT

71-005 71-00-00 Engine Automatic Start M FOT

71-006 71-00-00 Engine Manual Start M FOT

71-007 71-00-00 Engine Sthutdown M FOT

71-008 71-00-00 Start Abort M FOT

REMARKS :




U72-00-00. ENGINE

72-001 72-00-00 FOD inspection O LOC

72-002 72-31-12

Fan blades : limits,

approved repairs,replacement O SGH

REMARKS :

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U73-00-00. ENGINE FUEL AND CONTROL

73-001 73-00-00Engine fuel and controls /indications in the cockpit

M TVC

73-002 73-00-00Engine fuel and controlscomponents

M TVC

73-003 73-11-00Inspection of the fuelmanifold assy (CFM)

O TVC

73-004 73-11-00 Fuel filter (CFM) O RIA

73-005 73-25-00 EIU BITE test M FOT

73-006 73-29-00FADEC Test on Gmd (EngNON Motoring) (CFM56)

M FOT

73-007 73-29-00FADEC Test on Gmd (EngNON Motoring) (CFM56)

M FOT

REMARKS :




U74-00-00. IGNITION

74-001 74-00-00 Ignition indication on ECAM M LOC

74-002 74-00-00 Ignition system components M TVC

74-003 74-00-00Test of the Ignition Systemwith CFDS M FOT

74-004 74-11-00 Ignito plug O TVC

REMARKS :

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U75-00-00. AIR

75-001 75-00-00 Air system components M TVC

REMARKS :




U76-00-00. ENGINES CONTROLS

76-001 76-00-00Engines systems controls inthe cockpit

M LOC

76-002 76-00-00Engine systems defectrectification & T/S (CFM)

O TSE

REMARKS :




U77-00-00. ENGINE INDICATING

77-001 77-00-00Engine indicating systems

/ECAM panelM TVC

77-002 77-00-00Engine indicating systemscomponents

M TVC

77-003 77-32-00Change configuration ofaccelerometer

M RIA

77-004 77-32-34Operational test of EVMUwith CFDS

M FOT

REMARKS :

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U78-00-00. EXHAUST

78-001 78-00-00Thrust reverser/exhaustcomponents

M TVC

78-002 78-30-00Deact./reactivation of thrustreverser

M MEL

78-003 78-30-00Deactivation of thrustreverser for maintenance

M SGH

78-004 78-31-41Operation of thrust reverserusing CFDS M FOT

REMARKS :




U79-00-00. OIL

79-001 79-00-00 Oil system components M TVC

79-002 79-00-00 Oli filters O SGH

79-003 79-00-00Oil filter clogged indicatorsinspection

M RIA

79-004 79-31-00Oil quantity indication onECAM

M MEL

79-005 79-35-00Oil filter clogged warning onECAM

M MEL

REMARKS :




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U80-00-00. STARTING

80-001 80-00-00starting systemcomponents

M LOC

80-002 80-00-00Starting system - defectrectification & T/S

M TSE

80-003 80-11-00Manual operation of startervalve

M FOT TVC

REMARKS :

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U71-00-00. POWER V2500

71-001 71-00-00 Power Plant components M LOC

71-002 71-00-00Power Plant defectrectification & T/S

M TSE

71-003 71-00-00Opening & closing ofengine cowlings

M SGH

71-004 71-00-00DRY/Wet motoring ofengine

M FOT

71-005 71-00-00 Engine Automatic Start M FOT

71-006 71-00-00 Engine Manual Start M FOT

71-007 71-00-00 Engine Sthutdown M FOT

71-008 71-00-00 Start Abort M FOT

REMARKS :




U72-00-00. ENGINE

72-001 72-00-00 FOD inspection O LOC

72-002 72-31-12

Fan blades : limits,

approved repairs,replacement O SGH

REMARKS :

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U73-00-00. ENGINE FUEL AND CONTROL

73-001 73-00-00Engine fuel and controls /indications in the cockpit

M TVC

73-002 73-00-00Engine fuel and controlscomponents

M TVC

73-003 73-11-00Inspection of the fuelmanifold assy (V2500)

O TVC

73-004 73-11-00 Fuel filter (CFM) O RIA

73-005 73-25-00 EIU BITE test M FOT

73-006 73-29-00FADEC Test on Gmd (EngNON Motoring) (V2500)

M FOT

73-007 73-29-00FADEC Test on Gmd (EngNON Motoring) (V2500)

M FOT

REMARKS :




U74-00-00. IGNITION

74-001 74-00-00 Ignition indication on ECAM M LOC

74-002 74-00-00 Ignition system components M TVC

74-003 74-00-00Test of the Ignition Systemwith CFDS M FOT

74-004 74-11-00 Ignitionplug O TVC

REMARKS :

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U75-00-00. AIR

75-001 75-00-00 Air system components M TVC

REMARKS :




U76-00-00. ENGINES CONTROLS

76-001 76-00-00Engines systems controls inthe cockpit

M LOC

76-002 76-00-00 Engine systems defectrectification & T/S (V2500)

O TSE

REMARKS :




U77-00-00. ENGINE INDICATING

77-001 77-00-00Engine indicating systems/ECAM panel

M TVC

77-002 77-00-00Engine indicating systemscomponents

M TVC

77-003 77-32-00Change configuration ofaccelerometer

M RIA

77-004 77-32-34Operational test of EVMUwith CFDS

M FOT

REMARKS :

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U78-00-00. EXHAUST

78-001 78-00-00Thrust reverser/exhaustcomponents

M TVC

78-002 78-30-00Deact./reactivation of thrustreverser

M MEL

78-003 78-30-00Deactivation of thrustreverser for maintenance

M SGH

78-004 78-31-41Operation of thrust reverserusing CFDS

M FOT

REMARKS :




U79-00-00. OIL

79-001 79-00-00 Oil system components M TVC

79-002 79-00-00 Oli filters O SGH

79-003 79-00-00Oil filter clogged indicatorsinspection

M RIA

79-004 79-31-00Oil quantity indication onECAM M MEL

79-005 79-35-00Oil filter clogged warning onECAM

M MEL

REMARKS :

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U80-00-00. STARTING

80-001 80-00-00starting systemcomponents

M LOC

80-002 80-00-00Starting system - defectrectification & T/S

M TSE

80-003 80-11-00Manual operation of startervalve

M FOT TVC

REMARKS :

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SUPPLEMENT DEXPERIENCE PRATIQUE

ATA reference Work experience DateTraineessignature

Assessorssignature

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Assessorssignature

Documents

Doc for 07 _ojt 320 b1 b2_ Ed4