A320 Series (CFM56 & V2500) B1/B2 Theory & Practical Training

Course Info

Course Syllabus is provided upon your request.

This course is in compliance with EASA Part-66, Appendix III "Type Training and Examination Standard".

Detailed description, operation, component location, removal/installation BITE and troubleshooting procedures to maintenance manual level.


Course Features

Theory: 33 days

Practical: 10 days

Objectives

After completing the Type Training Course;

The technician will acquire knowledge necessary to perform and certify maintenance tasks permitted to be carried out as certifying staff of the specified category stated in the course title.

The other technical staff will acquire detailed knowledge about A/C systems.


Prerequisites

Basic technical English and basic technical aircraft knowledge.


Target Groups

Technical personnel associated with aircraft maintenance or engineering activities.


Completion Standart

The minimum required attendance to the theoretical training is 75% of each phase and 90% of the total course duration.

If the minimum participation time is not met, a certificate of recognition will not be issued.  


Examination

Phase examinations are closed book and multiple-choice. 

Pass mark per phase: %75 


Certificate

After the successful completion of Type Training Theoretical and Practical Elements courses and examinations/assessments, trainees become entitled to receive the Certificate of Recognition with Reference to EASA Part 147 approval.


A320 Series (CFM56 & V2500) B1/B2 Theory & Practical Training

Application Form



Course Info

Introduction module:

05 Time limits/maintenance checks

06 Dimensions/Areas (MTOM, etc.)

07 Lifting and Shoring

08 Levelling and weighing

09 Towing and taxiing

10 Parking/mooring, Storing and Return to Service

11 Placards and Markings

12 Servicing

20 Standard practices — only type particular

Airframe structures

51 Standard practices and structures (damage classification, assessment and repair)

53 Fuselage

54 Nacelles/Pylons

55 Stabilisers

56 Windows

57 Wings

27A Flight Control Surfaces (All)

52 Doors

Zonal and Station Identification Systems.

Airframe systems:


21 Air Conditioning

21A Air Supply

21B Pressurisation

21C Safety and Warning Devices

22 Autoflight

23 Communications

24 Electrical Power

25 Equipment and Furnishings

25A Electronic Equipment including emergency equipment

26 Fire Protection

27 Flight Controls

27A Sys. Operation: Electrical/Fly-by-Wire

28 Fuel Systems

28A Fuel Systems — Monitoring and indicating

29 Hydraulic Power

29A Hydraulic Power — Monitoring and indicating

30 Ice and Rain Protection

31 Indicating/Recording Systems

31A Instrument Systems

32 Landing Gear

32A Landing Gear — Monitoring and indicating

33 Lights

34 Navigation

35 Oxygen

36 Pneumatic

36A Pneumatic — Monitoring and indicating

37 Vacuum

38 Water/Waste

41 Water Ballast

42 Integrated modular avionics

44 Cabin Systems

45 On-Board Maintenance System (or covered in 31)

46 Information Systems

50 Cargo and Accessory Compartments

Turbine Engine

70 Standard Practices — Engines,

70A Constructional arrangement and operation (Installation Inlet, Compressors, Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems).

70B Engine Performance

71 Powerplant

72 Engine Turbine/Turbo Prop/Ducted Fan/Unducted fan

73 Engine Fuel and Control

75 Air

76 Engine controls

78 Exhaust

79 Oil

80 Starting

82 Water Injections

83 Accessory Gear Boxes

84 Propulsion Augmentation

73A FADEC

74 Ignition

77 Engine Indicating Systems

49 Auxiliary Power Units (APUs)

 


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