RR Trent 700 GE CF6 PW 4000 OJT B1 or B1/B2 de formation... · requirements of Appendix III of PART 66 to have the B1 or B2 or B1/B2 rating on A330 ... Filling of the IDG with Oil

Airbus A330 RR/GE/PW MAINTENANCE PRACTICE TRAINING MANUAL

B1 or 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.49 ed1 Page 1 sur 51

Airbus A330 RR Trent 700

GE CF6 PW 4000

OJT B1 or B1/B2


B1 or B1/B2

Page 2 sur 51 DOC.FOR.49 ed1

TRAINEE NAME: Forename:

Licence number:

Experience on an aircraft with similar technology: YES NO

Signature: Date : / /

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 Date : / / Performed at :

DERICHEBOURG ATIS AÉRONAUTIQUE STAMP :

PRACTICAL ASSESSORS

Licence number/Stamp

NAME Signature Date

Validation by Quality Department: Date: Name: Signature:


B1 or B1/B2


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 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


B1 or B1/B2


- 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 email at the Quality Department for validation of pre-requisit.


B1 or B1/B2


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

signature Instructor's signature

ATA 05 - TIME LIMITS / MAINTENANCE CHECKS 05-001 05-00-00 Daily check M B1 TVC 05-002 05-50-00 Weekly check M B1 TVC 05-003 05-51-11 Walk around check M B1 TVC

05-004 05-51-18 Inspection after lightning strike O B1/B2 TPR

ATA 06 – DIMENSIONS and AREAS

06-001 06-20-00 Identify the major aircraft

zones M B1/B2 LOC

ATA 07 - LIFTING and SHORING

07-001 07-00-00 Main jacking/safety procedures M B1/B2 LOC

ATA 08 – LEVELLING and WEIGHTING 08-001 08-21-00 Perform Quick Leveling M B1/B2 SGH

ATA 09 - TOWING and TAXIING

09-001 09-10-00 Towing points/ Limitation of steering Angle M B1 SGH

ATA 10 – PARKING/STORAGE

10-001 10-11-00 Parking procedures M B1/B2 SGH

10-002 10-20-00 Mooring of aircraft and kit O B&/B2 LOC

ATA 11 – PLACARDS and MARKINGS

11-001 11-21-52 Cabin door emergency placards M B1/B2 LOC


B1 or B1/B2




REMARKS :

ATA 12 - SERVICING

12-001 12-11-28

Pressure Refuel with Automatic Control from the Panel 990VU M B1/B2 LOC

12-002 12-11-28 Pressure Refuel With Manual Control M B1 FOT

12-003 12-11-28

Procedure To Use The Fuel Magnetic Level Indicators M B1 SGH

12-004 12-12-29 Hydraulic power Servicing with a hand pump M B1 SGH

12-005 12-13-24

Filling of the IDG with Oil or Addition of Oil after Level Check O B1/B2 SGH

12-006 12-13-49 Gravity Servicing of the APU Oil Reservoir O B1 SGH

12-007 12-15-38

Fill the potable water system using electrical power O B1 TVC

12-008 12-15-38

Fill the potable water system without electrical power O B1 TVC

12-009 12-24-34 Draining of the Standby Static Pressure-Lines M B2 FOT

12-010 12-34-24 Aircraft grounding M B1/B2 SGH

ATA 20 – STANDARD PRACTICES - Airframe 20-001 20-28-00 Electrical bonding M B1/B2 TPR


B1 or B1/B2




REMARKS :

ATA 21 - AIR CONDITIONNING

21-001 21-00-00

Air conditioning system controls & indication in cockpit O B1/B2 LOC

21-002 21-00-00 Air conditioning general localisation in cockpit M B1/B2 LOC

21-003 21-26-00

Operational Test of the Avionics-Equipment Ventilation System M B1/B2 FOT

21-004 21-26-02

Avionics Equipment Ventilation Overboard Valve M B1/B2 MEL

21-005 21-31-00

Operational Test of the Pressure Control and Monitoring M B1 FOT

21-006 21-52-00 Air-condition pack components O B1/B2 LOC

21-007 21-63-00

System Test of the Cockpit and Cabin Temperature Control O B1/B2 FOT

21-008 21-63-17 Cabin temp sensor M B1/BS TVC 21-009 21-31-66 Safety valve filter M B1 SGH

21-010 21-30-00 Pressure control and

monitoring, Fault Isol(TSM) O B1/B2 TSE


B1 or B1/B2




REMARKS :

ATA 22 - AUTO FLIGHT

22-001 22-00-00 AFS controls and indications M B1/B2 TVC

22-002 22-00-00 AFS components O B1 LOC 22-003 22-00-00 AFS components M B2 LOC

22-004 22-10-00 Operational Test of True North Reference Selection O B2 FOT

22-005 22-10-00

Operational Test of AP Eng and Lock Devices of The Side Stick Controller and Rudder Pedals M B2 FOT

22-006 22-30-00

Operational Test of the Autothrust Isolation from Engine Control M B2 FOT

22-007 22-30-02 Autothrust instinctive disconnect M B1/B2 MEL

22-008 22-70-00 FM MCDU menu data entry M B1/B2 SGH

22-009 22-70-00 Operational Test of BACK-UP NAV Function O B2 FOT

22-010 22-70-00 Crossloading of the FM Data O B2 SGH

22-011 22-70-00 Uploading of the FM Data M B2 TVC


B1 or B1/B2




22-012 22-70-00 Operational Test of the MCDU 3 Transfer O B2 FOT

22-013 22-81-12 Remove/Install FCU O B2 RIA

22-014 22-96-00 BITE Test of the Auto Flight System M B2 FOT

22-015 22-97-00 Test of the LAND CAT III Capability M B2 FOT

22-016 22-81-00 FCU Fault Isolation(TSM) O B2 TSE REMARKS :

ATA 23- COMMUNICATION

23-001 23-00-00

Radio and cockpit communications components O B1 LOC

23-002 23-00-00

Radio and cockpit communications components M B2 LOC

23-003 23-00-00 Cabin communications systems components O B1 LOC

23-004 23-00-00 Cabin communications systems components M B2 LOC

23-005 23-11-00 HF System operational test O B1 FOT 23-006 23-11-00 HF System operational test M B2 FOT

23-007 23-11-00 Operational Test of the HF System O B2 FOT

23-008 23-12-00 VHF System operational test M B1/B2 FOT

23-009 23-12-00 Failure or the VHF 1 reception O B2 TSE

23-010 23-12-00 BITE Test of the VHF System M B2 FOT

23-011 23-12-01 VHF Communication systems O B1/B2 MEL


B1 or B1/B2




23-012 23-28-00 SATCOM System operationnal test O B1/B2 FOT

23-013 23-32-00

Change of the existing Prerecorded Announcement and Boarding Music (PRAM) O B2 SGH

23-014 23-33-34 Remove/Install PES Controller O B1/B2 RIA

23-015 23-33-71 Bite test of PES Music O B1/B2 FOT

23-016 23.36.51 Landscape camera (if installed) M B2 LOC

23-017 23-42-00 Cockpit to GRD crew call system M B2 FOT

23-018 23-43-00 Cockpit to GRD crew call system O B1 LOC

23-019 23-44-00 Service Interphone System operational test O B1/B2 FOT

23-020 23-51-07 Radio PTT Switch O B2 MEL

23-021 23-51-17 Remove/Install Radio PTT switch O B2 RIA

23-022 23-51-00 Operational Test of the Oxygen Mask Microphone O B2 FOT

23-023 23-51-00 BITE Test of the Audio System M B1/B2 FOT

23-024 23-71-00 Operational Test of the CVR O B1 FOT

23-025 23-71-00

Operational Test of the CVR and of the Recording on all Four Channels M B2 FOT

23-026 23-71-00

Operational Test of the CVR Recording Logic, Including Timer Relay O B2 FOT

23-027 23-73-00 PA System presentation M B2 TVC 23-028 23-73-00 PA System operational test M B1 FOT 23-029 23-73-00 Passengers call system O B1/B2 LOC

23-030 23-73-00 Interface and Power - Up Test of the CIDS O B1 FOT

23-031 23-73-00 Interface and Power - Up Test of the CIDS M B2 FOT

23-032 23-73-00

Operational test of Cabin / Flight Crew interphone system O B1/B2 FOT

23-033 23-73-00

Operational test of the Emergency Evacuation Signaling system M B1 FOT


B1 or B1/B2




23-034 23-73-00 Operational test of loudspeakers via MCDU M B1/B2 FOT

23-035 23-73-00 Operational test of cabin SIGNS via MCDU M B1 FOT

23-036 23-73-00 FAP and PIM general presentation M B2 TVC

23-037 23-73-00 Cabin layout and zone programming M B2 SGH

23-038 23-51-00 AMU failure, Fault Isolation(TSM) M B2 TSE

23-039 23-73-00 Operational test of the EVAC function M B2 FOT

23-040 23-73-00 Operational Test of Cabin LED Signs with the MCDU M B2 FOT

23-041 23-73-12 Remove/Install the FAP O B2 TVC 23-042 23-73-19 Remove/Install the CAM O B1/B2 RIA

23-043 23-73-34 Remove/Install the CIDS Director O B2 RIA

23-044 23-73-46 Remove/Install DEU A and/or DEU B M B1/B2 RIA

23-045 23-81-00 Operational Test of the Radio Management M B2 FOT

23-046 23-81-00

Operational Test of the Radio Navigation Back-up Mode M B2 FOT

23-047 23-81-13 Removal /Installation of the RMP M B1/B2 RIA


B1 or B1/B2




REMARKS :

ATA 24 – ELECTRICAL POWER. N.B. : SERVICING tasks please refer to ATA 12

24-001 24-00-00

Main electrical power panels in flight compartment O B1 LOC

24-002 24-00-00

Main electrical power panels in flight compartment M B2 LOC


B1 or B1/B2




24-003 24-00-00 Engine generators and components O B1 LOC

24-004 24-00-00 Engine generators and components M B2 LOC

24-005 24-21-00

Operational Test of the IDG Disconnect and Reconnect Function M B1/B2 TVC

24-006 24-22-00 Operational Test of the Side 1 and Side 2 Isolation M B2 FOT

24-007 24-23-00 APU generator and components O B1/B2 LOC

24-008 24-24-00 Emergency generator components O B1 LOC

24-009 24-24-00 Emergency generator components M B2 LOC

24-010 24-24-00

Operational Test of the Emergency Generation System O B1/B2 FOT

24-011 24-25-00

Operational Test of the AC Essential Generation Switching O B2 FOT

24-012 24-28-00

Operational Test of Static Inverter and DC ESS BUS SUPPLY M B2 FOT

24-013 24-28-00

Operational Test of Static Inverter and DC ESS BUS SUPPLY O B1 FOT

24-014 24-29-00 BITE test or the ECMU M B1/B2 FOT

24-015 24-30-00 DC generation components M B1/B2 LOC

24-016 24-32-00 TR unit reset M B1/B2 LOC

24-017 24-38-00 Batteries and Charge Controllers components O B1 LOC

24-018 24-38-34 BCL M B1/B2 TVC

24-019 24-40-00 External power components M B1 LOC

24-020 24-40-00 External power component M B2 LOC

24-021 24-41-00 GCU/GAPCU or GCU/GPCU system test M B2 FOT

24-022 24-41-00

Energize aircraft electrical circuits from external power M B1/B2 SGH

24-023 24-41-00 Energise aircraft electrical circuits from the APU M B1 FOT


B1 or B1/B2




24-024 24-41-00 Energise aircraft electrical circuits from the APU O B2 FOT

24-025 24-42-00 Energise the ground service network M B1/B2 FOT

24-026 24-22-02 AC Generation IDG Oil circuit O B1/B2 MEL

24-027 24-24-00 Failure of ECP, Fault isolation(TSM) O B1/B2 TSE

24-028 24-21-51 IDG Removal/installation M B1/B2 RIA REMARKS : ATA 25 - EQUIPMENT AND FURNISHING

25-001 25-11-00 Crew seats operational test M B1 FOT 25-002 25-11-00 ATTENDANT seats O B1/B2 LOC

25-003 25-71-00 Operation of the exterior ladder O B1/B2 SGH

25-004 25-21-00 Seats components O B1/B2 LOC


B1 or B1/B2




25-005 25-21-00 Passenger seats O B1 SGH

25-006 25-23-41 Remove /Install Ceiling panels M B1/B2 RIA

25-007 25-23-44 Remove /Install Dado Panel M B1 RIA

25-008 31-18-71 Remove /Install PSU O B1/B2 RIA 25-009 25-34-51 AIR CHILLER O B1/B2 LOC 25-010 25-35-00 Galley equipment M B1/B2 LOC 25-011 25-40-00 Lavatories M B1/B2 LOC

25-012 25-50-00 Cargo loading system components M B1/B2 LOC

25-013 25-62-00 Slide bottle pressure check M B1 LOC

25-014 25-62-41

Removal/Installation of Escape Slide Raft on passenger door O B1 RIA

25-015 25-62-42 E/S slide emergency exit O B1 TVC 25-016 25-65-00 ELT bite test M B2 FOT

25-017 25-65-20 Emergency Locator Transmitter (ELT) M B1/B2 LOC

25-018 25-74-00

Lower deck mobile crew rest room equipment(if fitted) O B1 LOC

25-019 25-27-36 Temperature setting panel O B1/B2 RIA REMARKS :

ATA 26 - FIRE PROTECTION.

26-001 26-00-00

Fire detection/ extinguishing. components cockpit O B1 LOC

26-002 26-00-00

Fire detection/ extinguishing. components cockpit M B2 LOC


B1 or B1/B2




26-003 26-00-00 Engine fire detection loops M B1 LOC 26-004 26-00-00 Engine fire detection loops M B2 LOC

26-005 26-12-00

Engine fire and overheat detection system operational test M B1/B2 FOT

26-006 26-13-00

APU fire and overheat detection system operational test M B1/B2 FOT

26-007 26-13-00 APU fire detection and extinguishing system O B1/B2 LOC

26-008 26-15-00

Avionic compartment smoke detection system components O B1/B2 LOC

26-009 26-15-00

Operational test of the Avionics Compartment Smoke-Detection through the MCDU M B1/B2 FOT

26-010 26-16-00 Cargo compartment fire extinguishing components O B1/B2 LOC

26-011 26-16-15 Removal/Installation of Cargo Smoke Detector M B1/B2 RIA

26-012 26-16-00

Operational check of Cargo Compartment Smoke Detection by PTT M B1/B2 FOT

26-013 26-16-00

Operational test of Lower-Deck Cargo-Compartment Smoke-Detection through the MCDU M B1 FOT

26-014 26-17-00 Lavatory fire extinguishing components O B1 LOC

26-015 26-17-00

Operational check of Lavatory Smoke Detection System by MCDU M B1/B2 FOT

26-016 26-18-03 LDMCR Smoke detection system O B1 MEL

26-017 26-21-41 Engine fire bottle weight check M B1/B2 SGH

26-018 26-13-00 APU fire detection loop ‘A’ fault (TSM) Troubleshoot M B1/B2 TSE

ATA 27 - FLIGHT CONTROLS

27-001 27-00-00 Flight control components in cockpit O B1 LOC

27-002 27-00-00 Flight control components in cockpit M B2 LOC


B1 or B1/B2




27-003 27-14-00 Ailerons and associated systems O B1 LOC

27-004 27-22-00 Operational test rudder trim actuation O B2 FOT

27-005 27-26-00 Operational test of back-up yaw damper (MCDU) O B2 FOT

27-006 27-44-00

Operational Test of the Trimmable Horizontal Stabiliser (THS) Actuator M B1 FOT

27-007 27-44-00

Operational Test of the Trimmable Horizontal Stabiliser (THS) Actuator O B2 FOT

27-008 27-50-00 SFCC /WTB Reset M B1 FOT 27-009 27-50-00 SFCC /WTB Reset O B2 FOT 27-010 27-51-00 SFCC System test M B1 FOT 27-011 27-51-00 SFCC System test M B2 FOT

27-012 27-54-00 Operational test of Flap and Slat System O B1 FOT

27-013 27-54-00 Extending/ retracting slat/flaps O B2 FOT

27-014 27-64-00 Spoiler system components O B1 LOC

27-015 27-64-01 Spoiler M B1 MEL 27-016 27-93-34 Remove/Instal FCPC M B1 RIA 27-017 27-93-34 F C P C O B2 RIA

27-018 27-96-00

Op Test of the Return to Low Speed Config of the Rudder and Pedals Travel-Limitation Units M B1 FOT

27-019 27-96-00

Op Test of the Return to Low Speed Config of the Rudder and Pedals Travel-Limitation Units O B2 FOT

27-020 27-96-00 BITE Test of the EFCS (SYSTEM TEST) M B1/B2 FOT

27-021 27-55-00 Flap position indicating, Fault Isloation (TSM) O B1/B2 TSE

27-022 17-99-00 Electrical backup O B1/B2 SGH


B1 or B1/B2




REMARKS :


B1 or B1/B2




ATA 28 - FUEL N.B. : For SERVICING tasks please refer to ATA 12

28-001 28-00-00 Fuel system components in cockpit O B1 LOC

28-002 28-00-00 Fuel system components in cockpit M B2 LOC

28-003 28-28-00 Pressure Defuel Procedure O B1 SGH 28-004 28-21-00 All fuel boost pumps M B1/B2 LOC

28-005 28-25-00 Ground fuel transfer procedure M B1/B2 FOT

28-006 28-25-00 Ground fuel transfer to the trim tank M B1 FOT

28-007 28-21-51 Removal/Installation of Fuel pump element O B1 TVC

28-008 28-26-53 Removal/Installation of Fuel Inlet Valve Actuator M B1 RIA

28-009 28-25-04 Refuel defuel system -Inlet valve O B1/B2 MEL

28-010 28-31-00 Fuel Jettison fault isolation(TSM) O B1/B2 TSE

28-011 28-42-00- 810-887

Fuel Quantity incorrect, temporarliy (TSM) O B1/B2 TSE

28-012 28-00-00 CDCCL procedures M B1/B2 SGH

28-013 28-42-22 Fuel Quantity indicator, remove/refit. O B1/B2 RIA

REMARKS :


B1 or B1/B2




ATA 29 - HYDRAULIC POWER N.B. : For SERVICING tasks please refer to ATA 12

29-001 29-00-00 Hydraulic power panels cockpit M B1/B2 LOC

29-002 29-00-00 Maintenance panel M B1 SGH 29-003 29-00-00 Maintenance panel M B2 SGH

29-004 29-00-00 Engine Hydraulic Components M B1/B2 LOC

29-005 29-00-00

Pressurise the green (blue ,yellow)hydraulic system with electric pump M B1 SGH

29-006 29-11-00 Green system ground service panel M B1/B2 LOC

29-007 29-12-00 Blue system ground service panel M B1/B2 LOC

29-008 29-13-00 Yellow system ground service panel M B1/B2 LOC

29-009 29-24-00 Operational test of the RAT Extension and retraction O B1 FOT

29-010 29-30-02

Indication reservoir quantity on ECAM Hyd page O B1/B2 MEL

29-011 29-31-11 Hyd tank Air Pressure switch, remove/install M B1/B2 RIA

29-012 29-22-51 Blue system electric pump, remove/install O B1 RIA

29-013 29-11-00- 810-813

Green hydraulic quantity transmitter, (TSM) O B1/B2 TSE

29-014 29-22-00-810-802

Overheat of Blue electric pump, (TSM) O B1 TSE

REMARKS :


B1 or B1/B2




ATA 30 - ICE AND RAIN PROTECTION

30-001 30-00-00 Anti ice system components in cockpit O B1 LOC

30-002 30-00-00 Anti ice system components in cockpit M B2 LOC

30-003 30-11-00 Wing anti ice components on wing M B1/B2 LOC

30-004 30-11-01 Wing ice protection anti ice Control valve M B1 MEL

30-005 30-31-00 Probe heat components O B1 LOC 30-006 30-31-00 Probe heat components M B2 LOC 30-007 30-40-00 Window heat components O B1 LOC 30-008 30-40-00 Window heat components M B2 LOC 30-009 30-42-34 Remove/Install WHC M B1/B2 RIA 30-010 30-21-01 Engine anti ice valve M B1/B2 MEL

30-010 30-11-00- 710-801

Operational test of wing anti-ice system M B1/B2 FOT

30-011 30-11-00-790-801

Leak check, anti-ice ducts and connections O B1 SGH

30-012 30-81-00-830-801

Loss of ice detectors (TSM) fault isolation O B1/B2 TSE

REMARKS :


B1 or B1/B2




ATA 31 - INDICATING/RECORDING

31-001 31-00-00

Indicating/recording System components and indication in cockpit O B1 LOC

31-002 31-00-00

Indicating/recording System components and indication in cockpit M B2 LOC

31-003 31-21-00 Procedure to Set the Clock M B1/B2 SGH 31-004 31-36-00 ACMS general operation M B1/B2 SGH 31-005 31-36-52 DAR Servicing M B2 SGH 31-006 31-50-00 FWS System test M B1/B2 FOT

31-007 31-50-00 Operational Test of the ECAM Control Panel O B2 FOT

31-008 31-60-00 DMC system test M B1/B2 FOT 31-009 31-60-00 EIS start/ stop procedure M B2 SGH

31-010 31-63-22 Removal/Installation of Display Unit M B1/B2 RIA

31-011 31-63-22 DU Cleaning Procedure O B2 SGH

31-012 31-68-01 ECAM DMC switching selector O B1/B2 MEL

31-013 31-56-00-810-804

Loss of ECAM control panel (TSM) M B1/B2 TSE

REMARKS :


B1 or B1/B2




ATA 32 - LANDING GEAR N.B : For SERVICING tasks please refer to ATA 12

32-001 32-00-00 System components and control in the cockpit O B1 LOC

32-002 32-00-00 System components and control in the cockpit M B2 LOC

32-003 32-10-00 MLG and doors components O B1/B2 LOC

32-004 32-20-00 NLG and doors components O B1/B2 LOC

32-005 32-00-00 Gear doors ground opening/ closing M B1 SGH

32-006 32-40-00 Wheels and brakes components O B1/B2 SGH

32-007 32-42-57 Remove/Install Wheel Speed Tachometer M B1/B2 RIA

32-008 32-42-00

Brakes system components (normal, alt, parking) O B1 LOC

32-009 32-46-00 BITE Test of the BSCU and its Related Systems M B1 FOT

32-010 32-69-00

Simulation of flight ,when the aircraft is on the ground M B1/B2 FOT

32-011 32-31-00 Normal Extension and Retraction System test M B1 FOT

32-012 32-42-02 Green brake system O B1 MEL

32-013 32-61-00-810-803

Nose landing gear shows false uplock condition(TSM) O B1/B2 TSE

32-014 32-31-01 LGCIU inop O B1:B2 MEL REMARKS :


B1 or B1/B2




ATA 33 - LIGHTS 33-001 33-10-00 Cockpit light operation O B1/B2 TVC

33-002 33-10-00 Bulb/ LED and push button body M B2 RIA

33-003 33-14-00 Operational test of Lights M B1 FOT 33-004 33-14-00 Annunciator lights test M B2 FOT

33-005 33-14-00 Annunciator lights spare bulbs O B1 LOC

33-006 33-14-00 Annunciator lights spare bulbs M B2 LOC

33-007 33-20-00 Cabin general illumination operation O B1/B2 TVC

33-008 33-21-11 Removal/Instal of Ballast Unit with Lamp-holder M B1/B2 RIA

33-009 33-24-00 Operational test of lavatory lighting O B1/B2 FOT

33-010 33-25-00 Passenger Reading Lights System test M B1 FOT

33-011 33-25-00

Bite test of Passenger reading lights and cabin attendant lights M B1/B2 FOT

33-012 33-25-00

Test of Passenger Reading lights and Cabin Attendant Lights M B2 FOT

33-013 33-30-00 Cargo and services lights operation O B1/B2 TVC

33-014 33-50-00 Emergency lights components M B1/B2 LOC

33-015 33-51-00

Operational check of the Emergency Light via MCDU M B1/B2 FOT

33-016 33-51-00 EMER LIGHT SYS operational test from FAP M B1/B2 FOT

33-017 33-51-00

Localised system test of the Emergency Power Supply Unit M B1/B2 FOT

33-018 33-51-00 EPSU load-programming procedure (teach in) O B1 SGH

33-019 33-51-00 EPSU load-programming procedure (teach in) M B2 SGH

33-020 33-51-38 Removal/Installation of EPSU battery M B1/B2 RIA

33-021 33-42-00-810-801

Left landing light inop (TSM) Fault isolation M B1/B2 TSE


B1 or B1/B2




REMARKS :


B1 or B1/B2




ATA 34- NAVIGATION

34-001 34-00-00 Navigation system components O B1 LOC

34-002 34-00-00 Navigation system components M B2 LOC

34-003 34-10-00 ADIRS start procedure M B1/B2 SGH 34-004 34-10-00 IRS align procedure M B1/B2 SGH 34-005 34-10-01 A D I R S O B1/B2 MEL

34-006 34-11-00

Detection of a discrepancy of the left and right static pressure on ADIRU 1 O B1/B2 TSE

34-007 34-11-00

Draining and Flushing of the Standby Static and Standby Total Pressure Lines O B2 SGH

34-008 34-11-00 ATT/ HDG switching operation M B2 TVC

34-009 34-11-00 Air data switching operation M B2 TVC

34-010 34-12-34 A D I R U M B1 TVC 34-011 34-12-34 A D I R U O B2 RIA 34-012 34-12-34 ADIRS Removal Criteria M B2 TVC

34-013 34-13-00 ALT/CAS dynamic slew test M B2 FOT

34-014 34-13-00 AOA SENSOR TEST O B2 FOT

34-015 34-13-00 VMO/MMO Selector Switch O B2 LOC

34-016 34-13-00 ADR interface test O B2 FOT

34-017 34-22-25 Bite test of the ISIS indicator (if installed) O B2 FOT

34-018 34-36-00 MMR System test M B1/B2 FOT

34-019 34-36-00 Operationnel Test of GPS Function O B1/B2 FOT

34-020 34-36-00 Operational Test of ILS Function O B2 FOT

34-021 34-41-00 Weather radar system test M B1 FOT 34-022 34-41-00 Weather radar system test O B2 FOT 34-023 34-42-00 R.A system test O B1/B2 FOT 34-024 34-42-00 Radio altimeter ramp test M B2 FOT 34-025 34-42-01 Radio altimeter M B2 MEL 34-026 34-43-00 TCAS system test O B1 FOT 34-027 34-43-00 TCAS system test M B2 FOT

34-028 34-48-00 GPWC or EGPWC system test O B1 FOT


B1 or B1/B2




34-029 34-48-00 GPWC or EGPWC system test M B2 FOT

34-030 34-48-00 Uploading of the Enhanced GPWC Data-Base O B2 TVC

34-031 34-48-00 GPWS ground vocabulary test O B2 FOT

34-032 34-51-00 DME System test M B2 FOT 34-033 34-52-00 BITE test of the ATC M B2 FOT 34-034 34-53-00 ADF system test O B1/B2 FOT

34-035 34-53-00 Operational Test of the ADF O B2 FOT

34-036 34-55-00 VOR/MARKER /DME System test O B1 FOT

34-037 34-55-00 VOR/MARKER System test M B2 FOT

34-038 34-41-00-810-803

Failure of weather radar antenna(TSM) fault isolation M B2 TSE

REMARKS :


B1 or B1/B2




ATA 35 OXYGEN

35-001 35-00-00 Flight compartment oxygen system components O B1 LOC

35-002 35-00-00 Flight compartment oxygen system components M B2 LOC

35-003 35-12-00 Crew oxygen system O B1/B2 LOC

35-004 35-21-00 Cabin oxygen system components O B1/B2 LOC

35-005 35-21-42 Remove/Install Generator Emergency Oxygen O B1 RIA

35-006 35-22-00

Check Oxygen Container Opening and Vent Function of Bleed/Vent Valve O B1 FOT

35-007 35-31-52

Visual check of the Tamper Seal/Serviceability Indicator on the Protective Breathing Eqpt M B1 TVC

35-008 35-32-00 Portable oxygen equipment O B1 LOC

35-009 35-13-01 Crew oxygen -control and indicating O B1 MEL

35-010 35-00-00-860-801

Precautions when working with Oxygen M B1/B2 SGH

REMARKS :


B1 or B1/B2




ATA 36 - PNEUMATIC

36-001 36-00-00 System components in cockpit O B1 LOC

36-002 36-00-00 System components in cockpit M B2 LOC

36-003 36-11-00 Engine bleed system components M B1 LOC

36-004 36-11-00 Engine bleed system components O B1 LOC

36-005 36-11-00 BITE Test of the BMC M B1/B2 FOT 36-006 36-11-06 IP Check valve O B1 MEL

36-007 36-11-15 Remove/Install Bleed Pressure Transducer 9HA M B1/B2 RIA

36-008 36-12-00

Operational Test of the APU Bleed-Air Supply and Crossbleed System O B1/B2 FOT

36-009 36-22-00 APU leak detection O B1/B2 TSE

36-010 36-21-00 Pressure and temperature monitoring M B1/B2 SGH

REMARKS :


B1 or B1/B2




ATA 38 - WATER:WASTE SYSTEM N.B : For SERVICING tasks please refer to ATA 12

38-001 38-00-00 CIDS water/ waste page on FAP O B2 LOC

38-002 38-10-00 Potable/waste water system components O B1 LOC

38-003 38-12-00 Potable water heater functional test O B1/B2 FOT

38-004 38-12-00 Isolation Toilet and Water Heater with Shut of Valve M B1 SGH

38-005 38-14-00 Drain water system O B1/B2 LOC

38-006 38-31-00 Operational test of the VSC M B1/B2 FOT

38-007 38-31-00 Functional test of the Toilet Assemblies M B1 FOT

38-008 38-31-41 Potable servicing for normal and ice conditions O B1 SGH

38-009 38-32-00 Potable water drainage O B1/B2 LOC

38-010 38-32-41 Removal/Instalation of Drain Valve O B1 RIA

38-011 38-41-00 Air supply system components O B1/B2 LOC

REMARKS :


B1 or B1/B2




ATA 45 - ONBOARD MAINTENANCE SYSTEMS 45-001 45-00-00 CMS Components O B1 LOC 45-002 45-10-00 CMS Components M B2 LOC 45-003 45-10-00 CMS general operation M B1/B2 TVC 45-004 45-10-00 CMS manual switching M B2 TVC 45-005 45-10-00 CMC System test M B1/B2 FOT

45-006 45-10-00 Operational Test of the Automatic Switching O B2 FOT

45-007 45-20-00 Uploading procedure with MDDU including FMGEC O B1 SGH

45-008 45-41-22 Printer servicing M B1/B2 SGH

ATA 46 - INFORMATION SYSTEMS 46-001 46-21-00 Bite Test ATIMS M B1 FOT 46-002 46-21-00 Bite Test ATSU by CMS M B2 FOT

46-003 46-21-00 VHF 3 Link Test of the ATSU M B2 FOT

46-004 46-21-00 SATCOM Link Test of the ATSU O B2 FOT

46-005 46-21-00 Initialisation Procedure of the ATSU Router M B2 TVC

46-006 46-21-00

Uploading of the ATSU Software with the Multipurpose Disk Drive Unit (MDDU) O B2 TVC

46-007 46-21-00

Procedure to Get Access to the DSP USER-DEFINED Pages M B2 TVC

46-008 46-21-21 DCDU, removal/installation O B2 RIA

46-009 46-21-00 Failure of ATSU(TSM) O B2 TSE REMARKS :


B1 or B1/B2




ATA 49 - APU N.B : For SERVICING tasks please refer to ATA 12

49-001 49-00-00 APU system components in cockpit O B1/B2 LOC

49-002 49-00-00 APU start, operation and shut down procedures O B1 FOT

49-003 49-16-01 Air intake flap O B1 MEL

49-004 49-41-00-810-805 APU ignitor fault(TSM) M B1/B2 TSE

49-005 49-00-00-710-801 Funtional test M B&/B2 SGH

REMARKS :


B1 or B1/B2




ATA 52 - DOORS

52-001 52-10-00 Passengers doors operation M B1/B2 SGH

52-002 52-30-00

FWD/AFT cargo door opening and closing with elec.hyd.pump M B1 SGH

52-003 52-30-00

FWD/AFT cargo door opening and closing with hand pump M B1 FOT

52-004 52-30-00 Cargo door locking mechanism M B1/B2 LOC

52-005 52-71-00 BITE Test of the Proximity Switch Control Unit M B1/B2 FOT

52-006 52-71-01

Door and escape slide control system -Proximity switches O B1/B2 MEL

ATA 53 - FUSELAGE

53-001 53-10-00 Opening / Closing of the Radome O B1/B2 SGH

53-002 53-11-00-210-801

General inspection of NLG stucture O B1 LOC

ATA 54 - NACELLE / PYLONS

54-001 54-50-00 Pylon Pressure relief Doors M B1 LOC

ATA 55- STABILIZERS 55-001 55-41-00 Rudder main structure O B1 LOC

ATA 56 - WINDOWS 56-001 56-10-00 Windshield Panels M B1 LOC

56-002 56-12-00 Cockpit sliding window operating mechanism M B1 SGH

56-003 30-42-00-810-817

Loss of windshield heater monitoring(TSM) M B1/B2 TSE

ATA 57 - WINGS 57-001 57-00-00 Pressure relief Panels O B1 LOC


B1 or B1/B2




REMARKS :


B1 or B1/B2




ATA 71 - POWER PLANT (RR Trent 772B-60)

71-001 71-13-00 Opening /Closing of the Fan Cowls doors M B1/B2 SGH

71-002 78-36-00 Opening /Closing of the Thrust Reverser Doors M B1 SGH

71-003 71-10-00 Visual Inspection of the Air Inlet Cowl O B1 TVC

71-004 71-00-00 Engine Controls and Indications in the Cockpit M B1/B2 LOC

71-005 71-00-00 DRY MOTORING CHECK M B1 FOT 71-006 71-00-00 WET MOTORING CHECK O B1 TVC 71-007 71-71-00 Engine drain module O B1 LOC

ATA 72 – ENGINE (RR Trent 772B-60)

72-001 72-21-00 Visual inspection of Fan Blades and Spinner M B1 TVC

72-002 72-00-00

Visual inspection of visible area of engine inlet/fan outlet O B1 TVC

72-003 72-60-00 Accessory drive gearbox M B1/B2 LOC REMARKS :


B1 or B1/B2




ATA 73- ENGINE FUEL AND CONTROL (RR Trent 772B-60)

73-001 73-00-00 Engine fuel control components M B1/B2 LOC

73-002 73-20-00 ECU components M B2 LOC 73-003 73-21-00 FADEC System Test M B1/B2 FOT

73-004 73-21-00 MCDU FADEC non motoring test M B1 FOT

73-005 73-21-00 MCDU FADEC motoring test M B1 FOT

73-006 73-21-00 FADEC Sensors M B2 LOC

73-008 73-21-00 FADEC Specific data Menu M B2 TVC

73-009 73-21-00 Reading of the Scheduled Maint Report M B2 TVC

73-010 73-21-51

Failure or the HP fuel shut-off valve in OPEN position on engine 1 O B1/B2 TSE

73-011 73-25-00 Engine short time limited dispatch items M B1 MEL

73-012 73-25-02 EIVMU O B2 MEL 73-013 73-25-34 MCDU EIVMU system test M B1 FOT

73-014 73-25-34 EIVMU specific data read out M B1 FOT

73-015 73-25-34 Bite Test of the EIVMU M B2 FOT

73-016 73-25-34 Read the MAX FLIGHT VIBRATION Data O B2 TVC

73-017 73-30-00 Fuel Filter clog indication M B1 MEL

73-018 73-21-13 Fuel temperature thermocouple remve/install O B1/B2 RIA

REMARKS :


B1 or B1/B2




ATA 74 - IGNITION (RR Trent 772B-60)

74-001 74-00-00 Ignition system components M B1/B2 FOT

74-002 74-21-51 Igniter Plug O B1 SGH 74-003 74-31-00 Ignition Indicating System M B1 MEL 74-004 74-11-34 Ignition units M B1/B2 LOC

ATA 75- AIR (RR Trent 772B-60) 75-001 75-00-00 Air system components M B1/B2 LOC

75-002 75-31-00

Adjustement/Test of the Variable Bleed Valve System O B1 TVC

75-003 75-33-00 Variable Stator Vane Actuator/Sensor O B1 RIA

75-004 75-41-00-810-833

High nacelle temp trend on engine(TSM) O B1 TSE

ATA76 – ENGINES CONTROLS (RR Trent 772B-60)

76-001 76-10-00 Engine controls in the cockpit M B1/B2 LOC

76-002 76-11-00 Adjustement and Rigging of the mechanical linkage O B1 SGH

76-003 76-11-19 Throttle Control Unit and Mechanical Box M B1 FOT

76-004 76-11-00-810-864

Engine throttle levers too tight or too loose(TSM) O B1 TSE

ATA 77 - ENGINE INDICATING (RR Trent 772B-60)

77-001 77-00-00 Engine indicating systems/ ECAM, panel M B1/B2 LOC

77-002 77-10-00 Engine indicating systems components on eng M B1/B2 LOC

REMARKS :


B1 or B1/B2




ATA 78 - Exhaust (RR Trent 772B-60)

78-001 78-00-00 Thrust reverser system components O B1/B2 LOC

78-002 78-30-00 Thrust Reverser Deactivate/Reavtivate M B1 MEL

78-003 78-31-00

Operational Test of the Thrust Reverser System Via MCDU M B1 FOT

78-004 78-32-41

Manual Deployment/stowing of the Pivoting Doors M B1 SGH

78-005 78-32-44 Adjustement of the Thrust Reverser Door Latches O B1 TVC

ATA 79 – OIL (RR Trent 772B-60)

79-001 79-00-00 Visual Inspection of the Oil System components M B1/B2 LOC

79-002 79-00-00 Check Master Magnetic Chip Detector for particles O B1 SGH

79-003 79-22-45 Check Scavenge Screens O B1 RIA 79-004 79-31-00 Oil Quantity Indication M B1 LOC

ATA 80– STARTING (RR Trent 772B-60)

80-001 80-00-00 Starting system components O B1 LOC

80-002 80-11-00 Manual operation of the Starter Shut-Off Valve M B1 SGH

80-003 80-11-10

Check Starter Magnetic Chip Detector and Oil Level O B1 TVC

80-004 80-11-01 Manual Start procedure M B1 MEL

80-005 80-11-00-810-841

Starter control valve does not move to the correct position(TSM) O B1 TSE


B1 or B1/B2




REMARKS :


B1 or 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.49 ed1 Page 40 sur 51

ATA 71 - POWER PLANT (GE CF6)

71-001 71-13-41 Opening /Closing of the Fan Cowls doors M B1/B2 SGH



71-004 71-00-00 Engine Controls and Indications in the Cockpit M B1/B2 LOC


ATA 72 – ENGINE (GE CF6)


72-002 72-00-00




B1 or B1/B2


Item ATA Subject Class B1/B2 Task Code Date Trainee’s

signature Instructor’s signature

73-00-00 - ENGINE FUEL AND CONTROL (GE CF6)








73-010 73-21-51

Failure or the HP fuel shut-off valve in OPEN position on engine 1 O B2 TSE







73-018 73-11-11 Fuel temperature thermocoule remove/install O B1/B2 RIA

REMARKS :


B1 or B1/B2




74-00-00 - IGNITION (GE CF6) 74-001 74-00-00 Ignition system components M B1 FOT 74-002 74-21-51 Igniter Plug O B1 SGH 74-003 74-31-00 Ignition Indicating System M B1 MEL 74-004 74-11-51 Ignition Units M B1/B2 LOC

75-00-00 - AIR (GE CF6) 75-001 75-00-00 Air system components M B1 LOC

75-002 75-31-00


75-003 75-32-00 Variable Stator Vane Actuator/Sensor O B1 TVC

75-004 75-41-00-810-819

High nacelle temp trend on engine (TSM) O B1 TSE

76-00-00 - ENGINES CONTROLS (GE CF6)




76-004 76-11-00-810-866


77-00-00 - ENGINE INDICATING (GE CF6)



REMARKS :


B1 or B1/B2




78-00-00 - EXHAUST(GE CF6)

78-001 78-00-00 Thrust reverser system components O B1 LOC


78-003 78-31-00


78-004 78-32-65



79-00-00 - OIL(GE CF6)

79-001 79-00-00 Visual Inspection of the Oil System components O B1 TVC

79-002 79-21-11 Check Master Magnetic Chip Detector for particles O B1 TVC

79-003 79-21-41 Check Scavenge Screens O B1 TVC 79-004 79-31-00 Oil Quantity Indication M B1 LOC

80-00-00 - STARTING(GE CF6)



80-003 80-11-41



80-005 80-11-00-810-813



B1 or B1/B2


REMARKS :


B1 or B1/B2




71-00-00 - POWER PLANT (PW 4000)

71-001 71-13-00 Opening /Closing of the Fan Cowls doors M B1 SGH



71-004 71-00-00 Engine Controls and Indications in the Cockpit M B1 LOC


72-00-00 - ENGINE(PW 4000)


72-002 72-00-00




B1 or B1/B2




73-00-00 - ENGINE FUEL AND CONTROL (PW 4000)








73-010 73-21-51

Failure or the HP fuel shut-off valve in OPEN position on engine 1 O B2 TSE







73-018 73-32-11 Fuel temperature thermocouple remve/install O B1/B2 RIA

REMARKS :


B1 or B1/B2




74-00-00 - IGNITION (PW 4000)

74-001 74-00-00 Ignition system components M B1 FOT

74-002 74-21-00 Igniter Plug O B1 SGH 74-003 74-31-00 Ignition Indicating System M B1 MEL 74-004 74-11-00 Ignition units M B1/B2 LOC

75-00-00 - AIR 75-001 75-00-00 Air system components M B1 LOC

75-002 75-31-00


75-003 75-31-12 Variable Stator Vane Actuator/Sensor O B1 TVC

75-004 75-41-00-810-825

High nacelle temp trend on engine(TSM) O B1 TSE

76-00-00 - ENGINES CONTROLS (PW 4000)




76-004 76-11-00-810-867


77-00-00 - ENGINE INDICATING (PW 4000)



REMARKS :


B1 or B1/B2




78-00-00 - EXHAUST(PW 4000)

78-001 78-00-00 Thrust reverser system components O B1 LOC


78-003 78-31-00


78-004 78-32-00



79-00-00 - OIL(PW 4000)

79-001 79-00-00 Visual Inspection of the Oil System components O B1 TVC

79-002 79-21-11 Check Master Magnetic Chip Detector for particles O B1 TVC

79-003 79-22-00 Check Scavenge Screens O B1 TVC 79-004 79-31-00 Oil Quantity Indication M B1 LOC

80-00-00 - STARTING(PW 4000)



80-003 80-11-18



80-005 80-11-00-810-823



B1 or B1/B2


REMARKS :


B1 or B1/B2


ADDITIONAL PRACTICAL EXPERIENCE ATA

reference Work experience Date Trainee’s signature

Assessor’s signature


B1 or B1/B2


ADDITIONAL PRACTICAL EXPERIENCE ATA

reference Work experience Date Trainee’s signature

Assessor’s signature

Documents

RR Trent 700 GE CF6 PW 4000 OJT B1 or B1/B2 de formation... · requirements of Appendix III of PART 66 to have the B1 or B2 or B1/B2 rating on A330 ... Filling of the IDG with Oil