Airbus A319/A320/A321 (IAE PW1100G) Differences from Airbus A319/A320/A321 (CFM LEAP-1A)

2d Theory + 1d Exam/Practical

  • 23 July
    2 day theory + 1 day practical
    Session information
    Sessions
    Theoretical Elements
    Wed 23 Jul 08:00 CEST - Thu 24 Jul 15:00 CEST
    Online
    Practical Elements - Dates are Tentative - TBD
    Thu 14 Aug 08:00 - Thu 14 Aug 15:00
    Ljubljana
    Ljubljana
    • €850.00 excl. VAT
    Register4 places remaining

Description

The theoretical training session will be instructor led and delivered to you in real-time. 

 Please note that Exam will be done online, so please bring your own laptops/ tablets.

Course Details

Part-66 Cat. B1/B2, Line & Base Maintenance

Electrical Systems, Airframe & Powerplant - ATA Spec 104 Level 3

Avionics Systems - ATA Spec 104 Level 3

 

Target Group:

Part-66 Category B1/B2: Line and Base Maintenance Engineers

 

Content:

This course covers Airframe, Engine and Electrical systems in detail to ATA specification 104 Level 3 and Avionics Systems Level 2 (i.a.w. Part 66 Appendix 3).

 

Training includes:

  • Description and operation of airframe, engine, electrical and avionics systems
  • Description and operation of controls and indications
  • Identification and location of the main components
  • Servicing of the airframe, engine and electrical systems in accordance with aircraft maintenance manuals
  • Troubleshooting of the airframe, engine and electrical systems with the use of built-in devices
  • Operational testing of the airframe, engine and electrical systems
  • Servicing and minor troubleshooting of the avionics systems with the use of built-in-test devices

 

Prerequisites:

Participants should have a EASA Part-66 Aircraft Maintenance License Cat. B1, B2 or equivalent.

 

Objectives:

  • Describe aircraft systems and their handling, using correct terminology and nomenclature
  • Identify the location of system components
  • Describe the relevant safety precautions
  • Explain the normal function of the aircraft systems
  • Identify and use appropriate aircraft documentation
  • Describe routine ramp and transit activities
  • Describe procedures for removal / installation unique to the aircraft type
  • Describe system, engine and component functional checks as specified in the maintenance manual
  • Use and interpret on-board diagnostics to a Line Replaceable Unit (LRU)
  • Correlate information for the purpose of making decisions with respect to fault diagnosis and rectification
  • Determine aircraft airworthiness in accordance with MEL/CDL, by using crew reports and/or on-board reporting systems

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