DOC FOR 07 OJT 320 B1 B2 Ed4 - atis-aviation.com de formation... · A318/319/320/321 CFM56 ... - describe the component replacement procedures specific to aircraft type. ... Location

A318/319/320/321 CFM56 A319/320/321 IAE V2500

MAINTENANCE PRACTICE TRAINING MANUAL B1 ou B1/B2

DERICHEBOURG Atis aéronautique, Parc Algorithmes, Immeuble Thalès – 17, Avenue Didier Daurat 31700 Blagnac

Tél. 05 34 60 61 40 - 05 34 60 61 50

DOC.FOR.07 ed4 1/48

A318/319/320/321 CFM56

A319/320/321 IAE V2500

A318/319/320/321 CFM56 A319/320/321 IAE V2500


DOC.FOR.07 ed4 2/48

TRAINEE SURNAME: Forename:

Licence number:

Experience on an aircraft with similar technology: YES NO

Signature: Date : / /

ON JOB TRAINING Type of training: A318/319/320/321 CFM56 A319/320/321 IAE V2500 Type: B1 B1/B2 Starting date : / / Ending Date : / / Performed at :

DERICHEBOURG ATIS AÉRONAUTIQUE STAMP :

PRACTICAL ASSESSORS Licence

number/Stamp NAME Signature Date

Validation by Quality Department:

Date: Name: Signature:

A318/319/320/321 CFM56 A319/320/321 IAE V2500


DOC.FOR.07 ed4 3/48

SUBJECT The 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 the requirements of Appendix III of PART 66 to have the B1 or B1/B2 rating on A318/319/320/321 CFM56 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 the trainee engineer and validated by assessors. This OJT will be performed under the responsibility of 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 similar technology: 70 hours(1),

- Engineer with B1 or B1/B2 rating and less than six month experience on an aircraft with a similar 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 to operational configuration (availability of aircraft, trainee and assessors). CLASSIFICATION Classifies 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 to

perform 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 TASKS Part 66 Appendix 3 paragraph 2.2 requires that the practical training element must consist of the performance of representative tasks and their assessment, in order to meet the following objectives:

a) Ensure safe performance of maintenance, inspections and routine work according to the maintenance manual and other relevant instructions and tasks as appropriate for the type of aircraft, for example troubleshooting, repairs, adjustments, replacements, rigging and functional 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 and

replacement of components The nominated trainer/assessor will sign off each task when satisfied that the trainee has attained the demonstrable level of understanding that is required. PRE-REQUISIT The 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 in the qualification of type. For any OJT, the assessors will have to make a request by email at the Quality Department for validation of pre-requisit.

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Item Ref. ATA Ref. Subject Class B1/B2 Task Code Date Trainee's

signature Instructor's signature

U05-00-00 - TIME LIMITS / MAINTENANCE CHECKSU

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&TAXING U

09-001 09-00-00 Towing points/steering angle 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

REMARKS :

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U12-00-00 - SERVICING U

12-001 12-11-28 Automatic refuel/defuel procedures M SGH

12-001 12-11-28 Presure Refuel under Manual Control M FOT

12-003 12-11-28 Magnetic Fuel Quantity indicators reading O SGH

12-004 12-12-29 Reservoirs refiling with hand pump M SGH

12-005 12-13-24 Electrical 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 21-00-00 ECS/Aircon controls I & indications int he cockpit M LOC

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

21-003 21-00-00 Aircon. System - Defects rectification & TIS M TSE

21-004 21-21-00 Operational test of Cabin Recirc Fans M FOT

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

21-006 21-26-00 Deact/reactivation of avionics vent components O MEL

21-007 21-26-00 Avionics smoke configuration control circuit O FOT

21-008 21-26-00 Operational test of the Avionics Eqpt Ventilation from the MCDU

O FOT

21-009 21-26-00 Avionics Equipt Ventilation syst 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 21-28-00 Cargo compartment ventilation system O FOT

21-013 21-28-00 Deact/reactivation of cargo compt. vent. Isol. valve O MEL

21-014 21-31-00 Manual pressure control & monitoring system O FOT

21-015 21-31-00 Operational Test of the Pressure Control and Monitoring System

M FOT

21-016 21-43-00 Test of the AFT CGO compartement Heating System

M FOT

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

21-018 21-51-00 Deact. / reactivation of pack flow contrl valve O MEL

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

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21-020 21-61-00 Operational test of Pack temp. Control. System M FOT

21-021 21-63-00 Deact. / reactivation of trim air & hot air valves O MEL

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

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

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



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U22-00-00 AUTO FLIGHT

22-001 22-00-00 AFS controls and indications in cockpit M LOC

22-002 22-00-00 AFS controls and indications in cockpit M LOC

22-003 22-10-00 A/P disengagement and locking devices O FOT

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

22-005 22-61-00 Rudder travel limiting function M FOT

22-006 22-62-00 Rudder trim function test and reset M FOT

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

22-008 22-66-00 FAC M RIA

22-009 22-70-00 FM Navigation database loading O SGH

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

22-011 22-70-00 Flight plan initialization procedure 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 22-97-00 AFS land CAT3 capability test M FOT

REMARKS :

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U23-00-00 COMMUNICATION

23-001 23-00-00 Com. System controls and indic. In the cockpit M LOC

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

23-003 23-00-00 Com. System - Defect rectification & TIS M TSE

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

23-005 23-12-00 VHF communication system operation 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 23-44-00 Service interphone / Mechanic call O FOT

23-012 23-51-00 Audio management operational 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 23-73-00 Cabin and flight crew interphone (CIDS) O FOT

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

23-020 23-73-00 FAP and PTP general operation M FOT

A318/319/320/321 CFM56 A319/320/321 IAE V2500





23-021 23-73-00 Cabin Layout and zone programming M SGH

23-022 23-73-00 CIDS system test through MCDU M FOT

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

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

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



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

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

24-002 24-00-00 Electrical power system components M LOC

24-003 24-00-00 Electrical system defects rectification & T/S M TSE

24-004 24-20-00 Deact/Reactivation RAT extension control M MEL RIA

24-005 24-20-00 Deact / Reactivation Engine driven generator M MEL RIA

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

24-007 24-24-00 Emergency generation system M FOT

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

24-009 24-26-00 Galley manual an automatic shedding O FOT

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

24-011 24-30-00 Deact / Reactivation of a BCL O MEL

24-012 24-32-00 TR reset via CFDS and from panel 103 VU O FOT

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

24-014 24-41-00 External power control/GPCU function M FOT

24-015 24-41-00 Energize a/c electrical network form ext. Power M FOT

24-016 24-41-00 De-Energize a/c electrical network from ext. Power M FOT

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

24-018 24-42-00 Energize the ground service network M FOT

24-019 24-56-00 Deact./React. Of Galley supply system M MEL

A318/319/320/321 CFM56 A319/320/321 IAE V2500





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

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U25-00-00 – EQUIPMENT AND FURNISHING.

25-001 25-00-00 Equipment & furnishing components location M LOC

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

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

25-004 25-21-00 Passenger convertible seats O SGH

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

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

25-007 25-25-00 PSU / PIU / cove light panels 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 25-53-00 Drainage cargo compartment O SGH

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

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

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U26-00-00 – FIRE PROTECTION.

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

26-002 26-12-00 Fire protection system components M LOC

26-003 26-12-00 Fire protection system defect rectification & T/S M TSE

26-004 26-12-00 Engine fire detection system test M FOT

26-005 26-13-00 APU fire detection system test M FOT

26-006 26-15-00 Avionics compartment smoke detection O FOT

26-007 26-16-00 LDCC Smoke Detection Test using PTT M FOT

26-008 26-17-00 Test of Lavatory Smoke Detection System M FOT

26-009 26-17-00 SDCU M RIA

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

26-011 26-23-00 Cargo compartment fire extinguishing system M FOT

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U27-00-200. FLIGHT CONTROL

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

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

27-003 27-00-00 Flight control system defects rectification & T/S M TSE

27-004 27-14-00 Deactivation / reactivation of aileron servo control M MEL

27-005 27-14-00 Aileron servo control actuation 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 27-23-00 Operational test of rudder travel 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 27-41-00 THS system test-using trim wheels M FOT

27-012 27-44-51 THS : check of no-back wear indicator O TVC

27-013 27-44-51 THS : inspection of gearbox magnetic chip detector O TVC

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

27-015 27-51-00 Wingtip brake and pressure off brake : eng & reset M FOT

27-016 27-51-00 SFCC (Flap system) BITE test M FOT

27-017 27-51-00 Automatic Integrity Test of SFCC M FOT

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

27-019 27-60-00 Ground spoiler maintenance device M SGH

27-020 27-64-00 Deactivation / reactivation of spoiler actuator M MEL

A318/319/320/321 CFM56 A319/320/321 IAE V2500





27-021 27-81-00 SFCC (slat system) BITE test M FOT

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

27-023 27-94-00 SEC M RIA

27-024 27-96-00 EFCS BITE (Ground Scanning) test M FOT

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

27-026 27-96-00 Test of the Side Stick Assembly O FOT

27-027 27-96-00 Test of the Damping Measurement (Aileron) M FOT

27-028 27-96-00 Test of the Damping Measurement (Elevator) M FOT

27-029 27-96-00 FCDC M RIA

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





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

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

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

28-003 28-00-00 Fuel system defects rectification & T/S M TSE

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

28-005 28-12-00 Tank venting overpressure protector M MEL

28-006 28-15-00 Transfer Valves Individual Operational 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 28-22-00 Bleed APU fuel line from APU O FOT

28-010 28-24-00 Engine LP fuel shut-off valve M FOT

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

28-012 28-25-00 Deact/reactivation of refuel valve (Manual refuel) O MEL

28-013 28-25-00 Deact/reactivation of transfer defuel valve O MEL

28-014 28-40-00 Deact/reactivation of APU LP 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 28-43-00 Determination of fuel level using M.L.I O SGH

28-018 28-46-00 Tank High Level Sensing System M FOT

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

28-020 / Fuel Tank Safety / CDCCL awareness M TPR

A318/319/320/321 CFM56 A319/320/321 IAE V2500



REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



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

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

29-002 29-00-00 Hydraulic system components & service panels

M LOC

29-003 29-00-00 Hydraulic power defects rectification & T/S M TSE

29-004 29-10-00 Press/depressurize Blue hydraulic system (using electric pump)

M FOT

29-005 29-12-00 Blue hyd. Sys. Electric pump phase unbalance detector

M FOT

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

29-007 29-17-00 Collector tanks seal drain system O SGH

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

29-009 29-23-00

Pressurize/ depressurise green hydraulic system from yellow hydraulic system through PTU using electric pump

M FOT

29-010 29-23-00 PTU isolation coupling disconnection reconnection M SGH

29-011 29-31-00 Deact./reactivation of hydraulic fluid quantity ind. M MEL

29-012 29-34-00 Deact./reactivation of reservoir pressurization ind. M MEL

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U30-00-00. ICE AND RAIN PROTECTION

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

30-002 30-00-00 Anti-ice system components M LOC

30-003 30-00-00 Anti-ice system defects rectification & T/S M TSE

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

M MEL

30-005 30-11-00 Wing ice protection ground test M FOT

30-006 30-21-00 Deact/reactivation of engine anti-ice valve O MEL

30-007 30-31-00 Check of probe heating channel M MEL

30-008 30-31-00 Probe ice protection operational test O FOT

30-009 30-31-00 PHC M RIA

30-010 30-42-00 Windshield anti-icing and defogging operational test O FOT

30-011 30-42-00 WHC M RIA

30-012 30-71-00 Deact/reactivation of Waste water drain mast heating O MEL

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U31-00-00. INDICATING/RECORDING

31-001 31-00-00 System controls and indications int he cockpit M LOC

31-002 31-00-00 Indicating/recording system components O LOC

31-003 31-00-00 Indicating/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 31-32-00 CFDS 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 31-33-00 FDIU fault monotoring Test via 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 31-36-00 AIDS 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 31-36-00 Update APU Hours and Cycles 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

A318/319/320/321 CFM56 A319/320/321 IAE V2500





31-021 31-60-00 EFIS/ECAM switching functions 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 :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



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

32-001 32-00-00 Landing gear system controls & Ind. Int the cockpit

M LOC

32-002 32-00-00 MLG/NLG/MWS and wheel well 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 MLG shock absorber spare seal activating valve and maintenance practices

O SGH

32-005 32-12-00 Maint landing gear doors ground opening & closing M SGH

32-006 32-22-00 Nose landing gear doors ground 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 32-42-00 Bleeding o brake system & reset of safety valve O SGH

32-010 32-42-00 Deact/reactivation of main wheel 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 32-44-00 Alternate braking with & without antis kid M FOT

32-014 32-45-00 Parking / ultimate emergency braking M FOT

32-015 32-45-00 Release of parking brake pressure O SGH

32-016 32-46-00 BSCU BITE Test and GNDSCAN selection M FOT

32-017 32-47-00 Deact./reacivation of brake temperature sensor O MEL

32-018 32-49-00 TPIS BITE test CFOS procedure (if installed) O FOT

A318/319/320/321 CFM56 A319/320/321 IAE V2500





32-019 32-51-00 Nose wheel steering operational test (CFOS) M FOT

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

32-021 32-69-00 BITE test of the landing gear M FOT

32-022 32-69-00 Simulation of flight, aircraft on ground O FOT

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



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U33-00-00. LIGHTS

33-001 33-00-00 Light controls & ind. In the cockpit M LOC

33-002 33-00-00 Light controls & ind. In the cabin M LOC

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

33-004 33-10-00 Bulb replacement of push button switches M RIA

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

33-006 33-14-00 Annuciator 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 33-35-00 Equipment compartment lighting 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 33-51-00 Emergency lighting through PTP O FOT

A318/319/320/321 CFM56 A319/320/321 IAE V2500





33-020 33-51-00 EMER LIGHT SVS from cockpit and FAP M FOT

33-021 33-51-00 EMER escape path marking lights M FOT

33-022 33-51-00 EPSU M RIA

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U34-00-00. NAVIGATION

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

34-002 34-00-00 Navigation system components M LOC

34-003 34-00-00 Navigation system - Defect rectification & T/S M TSE

34-004 34-10-00 ADIRS start / stop procedure 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 34-41-00 Weather 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 34-48-00 GPWS/EGPWS (as installed) M FOT

34-016 34-48-00 GPWC M RIA

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

34-018 34-58-00 GPSSU M RIA

A318/319/320/321 CFM56 A319/320/321 IAE V2500



Tél. 05 34 60 61 40 - 05 34 60 61 50


REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U35-00-00. OXYGEN

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

35-002 35-10-00 Cockpit and cabin oxygen system components M LOC

35-003 35-10-00 Crew oxygen system pressure indication-check M FOT

35-004 35-10-00 Crew oxygen system Full Face Mask test M FOT

35-005 35-10-02 Pressure check crew oxygen cylinder M TVC

35-006 35-11-00 Crew oxygen storage cylinder O RIA

35-007 35-21-00 Open cabin emerg container 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 35-31-00 Indicator check of the tamper seasl on smoke hood

O TVC

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U36-00-00. PNEUMATIC

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

36-002 36-00-00 Pneumatic system components M LOC

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

36-004 36-00-00 Pressurization of pneumatic system M FOT

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

36-006 36-11-00 Deact/ractivation of bleed press. Reg. Valve (PRV) M MEL

36-007 36-11-00 Deact/reactivation of HP bleed valve O MEL

36-008 36-11-00 CFDS bleed air supplu current status readout M FOT

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





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

38-001 38-10-00 Water /waste system components M LOC

38-002 38-10-00 Pressurization of potable water tank O SGH

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

38-004 38-12-00 Functional test of the water system O FOT

38-005 38-12-00 functional test/reset of the water heater O FOT

38-006 38-13-00 Water quantity indicating system test M FOT

38-007 38-31-00 Vacuum toilet system BITE/test O FOT

38-008 38-31-00 VSC M RIA

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





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

49-001 49-00-00 APU controls & indications in the cockpit M LOC

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

49-003 49-00-00 APU start/shutdown 49.004.49-0-00 ECB self test

M SGH

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

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

49-006 49-62-00 APU emergency shut down test O FOT

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



Tél. 05 34 60 61 40 - 05 34 60 61 50




U52-00-00. DOORS

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

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

52-003 52-10-00 Escape slide disarming when opening from outside M FOT

52-004 52-21-00 Over wing emergency exits disarming (A319/A320) M FOT

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

52-006 52-30-00 Cargo doors operation with electric M FOT

52-007 52-30-00 Cargo doors operation with hand pump O FOT

52-008 52-30-00 Deact/reactivation of cargo door actuators O MEL

52-009 52-33-00 Bulk cargo door operation (if installed) O SGH

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



Tél. 05 34 60 61 40 - 05 34 60 61 50




U53-00-00. FUSELAGE

53-001 53-10-00 Opening / closing of the radome O SGH

53-002 53-10-00 Radome inspection for damage 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 56-10-00 Cleaning of windshield and windows O SGH

56-002 56-12-00 Operation of cockpit sliding windows M FOT

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



Tél. 05 34 60 61 40 - 05 34 60 61 50




U71-00-00. POWER CFM 56

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

71-002 71-00-00 Power Plant defect rectification & T/S M TSE

71-003 71-00-00 Opening & closing of engine cowlings M SGH

71-004 71-00-00 DRY/Wet motoring of engine 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 :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U73-00-00. ENGINE FUEL AND CONTROL

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

73-002 73-00-00 Engine fuel and controls components M TVC

73-003 73-11-00 Inspection of the fuel manifold 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 73-29-00 FADEC Test on Gmd (Eng NON Motoring) (CFM56) M FOT

73-007 73-29-00 FADEC Test on Gmd (Eng NON 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 74-00-00 Test of the Ignition System with CFDS M FOT

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

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U75-00-00. AIR

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

REMARKS :



U76-00-00. ENGINES CONTROLS

76-001 76-00-00 Engines systems controls in the cockpit M LOC

76-002 76-00-00 Engine systems defect rectification & T/S (CFM) O TSE

REMARKS :



U77-00-00. ENGINE INDICATING

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

77-002 77-00-00 Engine indicating systems components M TVC

77-003 77-32-00 Change configuration of accelerometer M RIA

77-004 77-32-34 Operational test of EVMU with CFDS M FOT

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U78-00-00. EXHAUST

78-001 78-00-00 Thrust reverser/exhaust components M TVC

78-002 78-30-00 Deact./reactivation of thrust reverser M MEL

78-003 78-30-00 Deactivation of thrust reverser for maintenance M SGH

78-004 78-31-41 Operation of thrust reverser using 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 79-00-00 Oil filter clogged indicators inspection M RIA

79-004 79-31-00 Oil quantity indication on ECAM M MEL

79-005 79-35-00 Oil filter clogged warning on ECAM M MEL

REMARKS :



A318/319/320/321 CFM56 A319/320/321 IAE V2500



U80-00-00. STARTING

80-001 80-00-00 starting system components M LOC

80-002 80-00-00 Starting system - defect rectification & T/S M TSE

80-003 80-11-00 Manual operation of starter valve M FOT TVC

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



Tél. 05 34 60 61 40 - 05 34 60 61 50




U71-00-00. POWER V2500

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

71-002 71-00-00 Power Plant defect rectification & T/S M TSE

71-003 71-00-00 Opening & closing of engine cowlings M SGH

71-004 71-00-00 DRY/Wet motoring of engine 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 :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U73-00-00. ENGINE FUEL AND CONTROL

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

73-002 73-00-00 Engine fuel and controls components M TVC

73-003 73-11-00 Inspection of the fuel manifold 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 73-29-00 FADEC Test on Gmd (Eng NON Motoring) (V2500) M FOT

73-007 73-29-00 FADEC Test on Gmd (Eng NON 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 74-00-00 Test of the Ignition System with CFDS M FOT

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

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U75-00-00. AIR

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

REMARKS :



U76-00-00. ENGINES CONTROLS

76-001 76-00-00 Engines systems controls in the cockpit M LOC

76-002 76-00-00 Engine systems defect rectification & T/S (V2500) O TSE

REMARKS :



U77-00-00. ENGINE INDICATING

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

77-002 77-00-00 Engine indicating systems components M TVC

77-003 77-32-00 Change configuration of accelerometer M RIA

77-004 77-32-34 Operational test of EVMU with CFDS M FOT

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U78-00-00. EXHAUST

78-001 78-00-00 Thrust reverser/exhaust components M TVC

78-002 78-30-00 Deact./reactivation of thrust reverser M MEL

78-003 78-30-00 Deactivation of thrust reverser for maintenance M SGH

78-004 78-31-41 Operation of thrust reverser using 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 79-00-00 Oil filter clogged indicators inspection M RIA

79-004 79-31-00 Oil quantity indication on ECAM M MEL

79-005 79-35-00 Oil filter clogged warning on ECAM M MEL

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500





U80-00-00. STARTING

80-001 80-00-00 starting system components M LOC

80-002 80-00-00 Starting system - defect rectification & T/S M TSE

80-003 80-11-00 Manual operation of starter valve M FOT TVC

REMARKS :

A318/319/320/321 CFM56 A319/320/321 IAE V2500



SUPPLEMENT D’EXPERIENCE PRATIQUE

ATA reference Work experience Date Trainee’s signature

Assessor’s signature

A318/319/320/321 CFM56 A319/320/321 IAE V2500






A318/319/320/321 CFM56 A319/320/321 IAE V2500






Documents

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