OJT B1 or B1/B2. Airbus A330 RR Trent 700 GE CF6 PW Airbus A330 RR/GE/PW MAINTENANCE PRACTICE TRAINING MANUAL B1 or B1/B2 - PDF

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Airbus A330 RR Trent 700 GE CF6 PW 4000 OJT DERICHEBOURG Atis aéronautique, Parc Algorithmes, Immeuble Thalès 17, Avenue Didier Daurat Blagnac Tél Page 1 sur 51 TRAINEE
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Airbus A330 RR Trent 700 GE CF6 PW 4000 OJT DERICHEBOURG Atis aéronautique, Parc Algorithmes, Immeuble Thalès 17, Avenue Didier Daurat Blagnac Tél Page 1 sur 51 TRAINEE NAME: Forename: Licence number: Experience on an aircraft with similar technology: YES NO Signature: : / / ON JOB TRAINING Type of training: A 330 (RR Trent 700) A 330 (GE CF6-80) A 330 (PW 4000) Type: B1 B2 B1/B2 Start date : / / End : / / Performed at : DERICHEBOURG ATIS AÉRONAUTIQUE STAMP : Licence number/stamp PRACTICAL ASSESSORS NAME Signature Validation by Quality Department: : Name: Signature: Page 2 sur 51 SUBJECT The aim of this document is to record all the practical tasks performed by engineers within ATIS Aviation, PART 145 FR approved maintenance organisation, in order to comply with the requirements of Appendix III of PART 66 to have the B1 or B2 or B1/B2 rating on A330 (RR/PW/GE) 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 B2 or B1/B2 qualified engineers. (See PRE-REQUISITE on page 4/47) 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 B2 or B1/B2 rating and six month experience on an aircraft with a similar technology: 70 hours (1), - Engineer with B1 or B2 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 B2 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 Page 3 sur 51 - TPR: Thorough Procedural review (*) If ground power or other applicable systems are unavailable a TPR will be carried out in place of a FOT. SIGNING OFF THE TASKS Part 66 Appendix 3 paragraph 2.2 requires that the practical training element must consist in 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-REQUISITE 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 at the Quality Department for validation of pre-requisit. Page 4 sur 51 ATA 05 - TIME LIMITS / MAINTENANCE CHECKS Daily check M B1 TVC Weekly check M B1 TVC Walk around check M B1 TVC Inspection after lightning strike O B1/B2 TPR ATA 06 DIMENSIONS and AREAS Identify the major aircraft zones M B1/B2 LOC ATA 07 - LIFTING and SHORING Main jacking/safety procedures M B1/B2 LOC ATA 08 LEVELLING and WEIGHTING Perform Quick Leveling M B1/B2 SGH ATA 09 - TOWING and TAXIING ATA 10 PARKING/STORAGE Towing points/ Limitation of steering Angle M B1 SGH Parking procedures M B1/B2 SGH Mooring of aircraft and kit O B&/B2 LOC ATA 11 PLACARDS and MARKINGS Cabin door emergency placards M B1/B2 LOC Page 5 sur 51 ATA 12 - SERVICING Pressure Refuel with Automatic Control from the Panel 990VU M B1/B2 LOC Pressure Refuel With Manual Control M B1 FOT Procedure To Use The Fuel Magnetic Level Indicators M B1 SGH Hydraulic power Servicing with a hand pump M B1 SGH Filling of the IDG with Oil or Addition of Oil after Level Check O B1/B2 SGH Gravity Servicing of the APU Oil Reservoir O B1 SGH Fill the potable water system using electrical power O B1 TVC Fill the potable water system without electrical power O B1 TVC Draining of the Standby Static Pressure-Lines M B2 FOT Aircraft grounding M B1/B2 SGH ATA 20 STANDARD PRACTICES - Airframe Electrical bonding M B1/B2 TPR Page 6 sur 51 ATA 21 - AIR CONDITIONNING Air conditioning system controls & indication in cockpit O B1/B2 LOC Air conditioning general localisation in cockpit M B1/B2 LOC Operational Test of the Avionics-Equipment Ventilation System M B1/B2 FOT Avionics Equipment Ventilation Overboard Valve M B1/B2 MEL Operational Test of the Pressure Control and Monitoring M B1 FOT Air-condition pack components O B1/B2 LOC System Test of the Cockpit and Cabin Temperature Control O B1/B2 FOT Cabin temp sensor M B1/BS TVC Safety valve filter M B1 SGH Pressure control and monitoring, Fault Isol(TSM) O B1/B2 TSE Page 7 sur 51 ATA 22 - AUTO FLIGHT AFS controls and indications M B1/B2 TVC AFS components O B1 LOC AFS components M B2 LOC Operational Test of True North Reference Selection O B2 FOT Operational Test of AP Eng and Lock Devices of The Side Stick Controller and Rudder Pedals M B2 FOT Operational Test of the Autothrust Isolation from Engine Control M B2 FOT Autothrust instinctive disconnect M B1/B2 MEL FM MCDU menu data entry M B1/B2 SGH Operational Test of BACK- UP NAV Function O B2 FOT Crossloading of the FM Data O B2 SGH Uploading of the FM Data M B2 TVC Page 8 sur 51 Operational Test of the MCDU 3 Transfer O B2 FOT Remove/Install FCU O B2 RIA BITE Test of the Auto Flight System M B2 FOT Test of the LAND CAT III Capability M B2 FOT FCU Fault Isolation(TSM) O B2 TSE ATA 23- COMMUNICATION Radio and cockpit communications components O B1 LOC Radio and cockpit communications components M B2 LOC Cabin communications systems components O B1 LOC Cabin communications systems components M B2 LOC HF System operational test O B1 FOT HF System operational test M B2 FOT Operational Test of the HF System O B2 FOT VHF System operational test M B1/B2 FOT Failure or the VHF 1 reception O B2 TSE BITE Test of the VHF System M B2 FOT VHF Communication systems O B1/B2 MEL Page 9 sur 51 SATCOM System operationnal test O B1/B2 FOT Change of the existing Prerecorded Announcement and Boarding Music (PRAM) O B2 SGH Remove/Install PES Controller O B1/B2 RIA Bite test of PES Music O B1/B2 FOT Landscape camera (if installed) M B2 LOC Cockpit to GRD crew call system M B2 FOT Cockpit to GRD crew call system O B1 LOC Service Interphone System operational test O B1/B2 FOT Radio PTT Switch O B2 MEL Remove/Install Radio PTT switch O B2 RIA Operational Test of the Oxygen Mask Microphone O B2 FOT BITE Test of the Audio System M B1/B2 FOT Operational Test of the CVR O B1 FOT Operational Test of the CVR and of the Recording on all Four Channels M B2 FOT Operational Test of the CVR Recording Logic, Including Timer Relay O B2 FOT PA System presentation M B2 TVC PA System operational test M B1 FOT Passengers call system O B1/B2 LOC Interface and Power - Up Test of the CIDS O B1 FOT Interface and Power - Up Test of the CIDS M B2 FOT Operational test of Cabin / Flight Crew interphone system O B1/B2 FOT Operational test of the Emergency Evacuation Signaling system M B1 FOT Page 10 sur 51 Operational test of loudspeakers via MCDU M B1/B2 FOT Operational test of cabin SIGNS via MCDU M B1 FOT FAP and PIM general presentation M B2 TVC Cabin layout and zone programming M B2 SGH AMU failure, Fault Isolation(TSM) M B2 TSE Operational test of the EVAC function M B2 FOT Operational Test of Cabin LED Signs with the MCDU M B2 FOT Remove/Install the FAP O B2 TVC Remove/Install the CAM O B1/B2 RIA Remove/Install the CIDS Director O B2 RIA Remove/Install DEU A and/or DEU B M B1/B2 RIA Operational Test of the Radio Management M B2 FOT Operational Test of the Radio Navigation Back-up Mode M B2 FOT Removal /Installation of the RMP M B1/B2 RIA Page 11 sur 51 ATA 24 ELECTRICAL POWER. N.B. : SERVICING tasks please refer to ATA 12 Main electrical power panels in flight compartment O B1 LOC Main electrical power panels in flight compartment M B2 LOC Page 12 sur 51 Engine generators and components O B1 LOC Engine generators and components M B2 LOC Operational Test of the IDG Disconnect and Reconnect Function M B1/B2 TVC Operational Test of the Side 1 and Side 2 Isolation M B2 FOT APU generator and components O B1/B2 LOC Emergency generator components O B1 LOC Emergency generator components M B2 LOC Operational Test of the Emergency Generation System O B1/B2 FOT Operational Test of the AC Essential Generation Switching O B2 FOT Operational Test of Static Inverter and DC ESS BUS SUPPLY M B2 FOT Operational Test of Static Inverter and DC ESS BUS SUPPLY O B1 FOT BITE test or the ECMU M B1/B2 FOT DC generation components M B1/B2 LOC TR unit reset M B1/B2 LOC Batteries and Charge Controllers components O B1 LOC BCL M B1/B2 TVC External power components M B1 LOC External power component M B2 LOC GCU/GAPCU or GCU/GPCU system test M B2 FOT Energize aircraft electrical circuits from external power M B1/B2 SGH Energise aircraft electrical circuits from the APU M B1 FOT Page 13 sur 51 Energise aircraft electrical circuits from the APU O B2 FOT Energise the ground service network M B1/B2 FOT AC Generation IDG Oil circuit O B1/B2 MEL Failure of ECP, Fault isolation(tsm) O B1/B2 TSE IDG Removal/installation M B1/B2 RIA ATA 25 - EQUIPMENT AND FURNISHING Crew seats operational test M B1 FOT ATTENDANT seats O B1/B2 LOC Operation of the exterior ladder O B1/B2 SGH Seats components O B1/B2 LOC Page 14 sur 51 Passenger seats O B1 SGH Remove /Install Ceiling panels M B1/B2 RIA Remove /Install Dado Panel M B1 RIA Remove /Install PSU O B1/B2 RIA AIR CHILLER O B1/B2 LOC Galley equipment M B1/B2 LOC Lavatories M B1/B2 LOC Cargo loading system components M B1/B2 LOC Slide bottle pressure check M B1 LOC Removal/Installation of Escape Slide Raft on passenger door O B1 RIA E/S slide emergency exit O B1 TVC ELT bite test M B2 FOT Emergency Locator Transmitter (ELT) M B1/B2 LOC Lower deck mobile crew rest room equipment(if fitted) O B1 LOC Temperature setting panel O B1/B2 RIA ATA 26 - FIRE PROTECTION. Fire detection/ extinguishing. components cockpit O B1 LOC Fire detection/ extinguishing. components cockpit M B2 LOC Page 15 sur 51 Engine fire detection loops M B1 LOC Engine fire detection loops M B2 LOC Engine fire and overheat detection system operational test M B1/B2 FOT APU fire and overheat detection system operational test M B1/B2 FOT APU fire detection and extinguishing system O B1/B2 LOC Avionic compartment smoke detection system components O B1/B2 LOC Operational test of the Avionics Compartment Smoke-Detection through the MCDU M B1/B2 FOT Cargo compartment fire extinguishing components O B1/B2 LOC Removal/Installation of Cargo Smoke Detector M B1/B2 RIA Operational check of Cargo Compartment Smoke Detection by PTT M B1/B2 FOT Operational test of Lower- Deck Cargo-Compartment Smoke-Detection through the MCDU M B1 FOT Lavatory fire extinguishing components O B1 LOC Operational check of Lavatory Smoke Detection System by MCDU M B1/B2 FOT LDMCR Smoke detection system O B1 MEL Engine fire bottle weight check M B1/B2 SGH APU fire detection loop A fault (TSM) Troubleshoot M B1/B2 TSE ATA 27 - FLIGHT CONTROLS Flight control components in cockpit O B1 LOC Flight control components in cockpit M B2 LOC Page 16 sur 51 Ailerons and associated systems O B1 LOC Operational test rudder trim actuation O B2 FOT Operational test of back-up yaw damper (MCDU) O B2 FOT Operational Test of the Trimmable Horizontal Stabiliser (THS) Actuator M B1 FOT Operational Test of the Trimmable Horizontal Stabiliser (THS) Actuator O B2 FOT SFCC /WTB Reset M B1 FOT SFCC /WTB Reset O B2 FOT SFCC System test M B1 FOT SFCC System test M B2 FOT Operational test of Flap and Slat System O B1 FOT Extending/ retracting slat/flaps O B2 FOT Spoiler system components O B1 LOC Spoiler M B1 MEL Remove/Instal FCPC M B1 RIA F C P C O B2 RIA Op Test of the Return to Low Speed Config of the Rudder and Pedals Travel- Limitation Units M B1 FOT Op Test of the Return to Low Speed Config of the Rudder and Pedals Travel- Limitation Units O B2 FOT BITE Test of the EFCS (SYSTEM TEST) M B1/B2 FOT Flap position indicating, Fault Isloation (TSM) O B1/B2 TSE Electrical backup O B1/B2 SGH Page 17 sur 51 Page 18 sur 51 ATA 28 - FUEL N.B. : For SERVICING tasks please refer to ATA Fuel system components in cockpit O B1 LOC Fuel system components in cockpit M B2 LOC Pressure Defuel Procedure O B1 SGH All fuel boost pumps M B1/B2 LOC Ground fuel transfer procedure M B1/B2 FOT Ground fuel transfer to the trim tank M B1 FOT Removal/Installation of Fuel pump element O B1 TVC Removal/Installation of Fuel Inlet Valve Actuator M B1 RIA Refuel defuel system -Inlet valve O B1/B2 MEL Fuel Jettison fault isolation(tsm) O B1/B2 TSE Fuel Quantity incorrect, temporarliy (TSM) O B1/B2 TSE CDCCL procedures M B1/B2 SGH Fuel Quantity indicator, remove/refit. O B1/B2 RIA Page 19 sur 51 ATA 29 - HYDRAULIC POWER N.B. : For SERVICING tasks please refer to ATA 12 Hydraulic power panels cockpit M B1/B2 LOC Maintenance panel M B1 SGH Maintenance panel M B2 SGH Engine Hydraulic Components M B1/B2 LOC Pressurise the green (blue,yellow)hydraulic system with electric pump M B1 SGH Green system ground service panel M B1/B2 LOC Blue system ground service panel M B1/B2 LOC Yellow system ground service panel M B1/B2 LOC Operational test of the RAT Extension and retraction O B1 FOT Indication reservoir quantity on ECAM Hyd page O B1/B2 MEL Hyd tank Air Pressure switch, remove/install M B1/B2 RIA Blue system electric pump, remove/install O B1 RIA Green hydraulic quantity transmitter, (TSM) O B1/B2 TSE Overheat of Blue electric pump, (TSM) O B1 TSE Page 20 sur 51 ATA 30 - ICE AND RAIN PROTECTION Anti ice system components in cockpit O B1 LOC Anti ice system components in cockpit M B2 LOC Wing anti ice components on wing M B1/B2 LOC Wing ice protection anti ice Control valve M B1 MEL Probe heat components O B1 LOC Probe heat components M B2 LOC Window heat components O B1 LOC Window heat components M B2 LOC Remove/Install WHC M B1/B2 RIA Engine anti ice valve M B1/B2 MEL Operational test of wing anti-ice system M B1/B2 FOT Leak check, anti-ice ducts and connections O B1 SGH Loss of ice detectors (TSM) fault isolation O B1/B2 TSE Page 21 sur 51 ATA 31 - INDICATING/RECORDING Indicating/recording System components and indication in cockpit O B1 LOC Indicating/recording System components and indication in cockpit M B2 LOC Procedure to Set the Clock M B1/B2 SGH ACMS general operation M B1/B2 SGH DAR Servicing M B2 SGH FWS System test M B1/B2 FOT Operational Test of the ECAM Control Panel O B2 FOT DMC system test M B1/B2 FOT EIS start/ stop procedure M B2 SGH Removal/Installation of Display Unit M B1/B2 RIA DU Cleaning Procedure O B2 SGH ECAM DMC switching selector O B1/B2 MEL Loss of ECAM control panel (TSM) M B1/B2 TSE Page 22 sur 51 ATA 32 - LANDING GEAR N.B : For SERVICING tasks please refer to ATA System components and control in the cockpit O B1 LOC System components and control in the cockpit M B2 LOC MLG and doors components O B1/B2 LOC NLG and doors components O B1/B2 LOC Gear doors ground opening/ closing M B1 SGH Wheels and brakes components O B1/B2 SGH Remove/Install Wheel Speed Tachometer M B1/B2 RIA Brakes system components (normal, alt, parking) O B1 LOC BITE Test of the BSCU and its Related Systems M B1 FOT Simulation of flight,when the aircraft is on the ground M B1/B2 FOT Normal Extension and Retraction System test M B1 FOT Green brake system O B1 MEL Nose landing gear shows false uplock condition(tsm) O B1/B2 TSE LGCIU inop O B1:B2 MEL Page 23 sur 51 ATA 33 - LIGHTS Cockpit light operation O B1/B2 TVC Bulb/ LED and push button body M B2 RIA Operational test of Lights M B1 FOT Annunciator lights test M B2 FOT Annunciator lights spare bulbs O B1 LOC Annunciator lights spare bulbs M B2 LOC Cabin general illumination operation O B1/B2 TVC Removal/Instal of Ballast Unit with Lamp-holder M B1/B2 RIA Operational test of lavatory lighting O B1/B2 FOT Passenger Reading Lights System test M B1 FOT Bite test of Passenger reading lights and cabin attendant lights M B1/B2 FOT Test of Passenger Reading lights and Cabin Attendant Lights M B2 FOT Cargo and services lights operation O B1/B2 TVC Emergency lights components M B1/B2 LOC Operational check of the Emergency Light via MCDU M B1/B2 FOT EMER LIGHT SYS operational test from FAP M B1/B2 FOT Localised system test of the Emergency Power Supply Unit M B1/B2 FOT EPSU load-programming procedure (teach in) O B1 SGH EPSU load-programming procedure (teach in) M B2 SGH Removal/Installation of EPSU battery M B1/B2 RIA Left landing light inop (TSM) Fault isolation M B1/B2 TSE Page 24 sur 51 Page 25 sur 51 ATA 34- NAVIGATION Navigation system components O B1 LOC Navigation system components M B2 LOC ADIRS start procedure M B1/B2 SGH IRS align procedure M B1/B2 SGH A D I R S O B1/B2 MEL Detection of a discrepancy of the left and right static pressure on ADIRU 1 O B1/B2 TSE Draining and Flushing of the Standby Static and Standby Total Pressure Lines O B2 SGH ATT/ HDG switching operation M B2 TVC Air data switching operation M B2 TVC A D I R U M B1 TVC A D I R U O B2 RIA ADIRS Removal Criteria M B2 TVC ALT/CAS dynamic slew test M B2 FOT AOA SENSOR TEST O B2 FOT VMO/MMO Selector Switch O B2 LOC ADR interface test O B2 FOT Bite test of the ISIS indicator (if installed) O B2 FOT MMR System test M B1/B2 FOT Operationnel Test of GPS Function O B1/B2 FOT Operational Test of ILS Function O B2 FOT Weather radar system test M B1 FOT Weather radar system test O B2 FOT R.A system test O B1/B2 FOT Radio altimeter ramp test M B2 FOT Radio altimeter M B2 MEL TCAS system test O B1 FOT TCAS system test M B2 FOT GPWC or EGPWC system test O B1 FOT Page 26 sur 51 GPWC or EGPWC system test M B2 FOT Uploading of the Enhanced GPWC Data-Base O B2 TVC GPWS ground vocabulary test O B2 FOT DME System test M B2 FOT BITE test of the ATC M B2 FOT ADF system test O B1/B2 FOT Operational Test of the ADF O B2 FOT VOR/MARKER /DME System test O B1 FOT VOR/MARKER System test M B2 FOT Failure of weather radar antenna(tsm) fault isolation M B2 TSE Page 27 sur 51 ATA 35 OXYGEN Flight compartment oxygen system components O B1 LOC Flight compartment oxygen system components M B2 LOC Crew oxygen system O B1/B2 LOC Cabin oxygen system components O B1/B2 LOC Remove/Install Generator Emergency Oxygen O B1 RIA Check Oxygen Container Opening and Vent Function of Bleed/Vent Valve O B1 FOT Visual check of the Tamper Seal/Serviceability Indicator on the Protective Breathing Eqpt M B1 TV
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