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Avionics Systems – ATA Spec 104 Level 2
Duration: 30 days / 210 lessons theoretical training
14 days / 98 hours practical training
Target Group: Part-66 Category B1: Line and Base Maintenance Technician - mechanical
Content: This course covers Airframe, Engine and Electrical elements in detail to ATA specification
104 Level 3 and Avionics Systems Level 2.
Training includes:
• Description and operation of airframe, engine, electrical and avionics systems.
• Description and operation of controls and indicators.
• 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 with the use of built-in-test devices
Number of Theoretical Minimum: 8 Practical Minimum: 4
Participants: Maximum: 15 Maximum: 6
Recommended: 10 Recommended: 5
Prerequisites: JAR/EASA Part-66 Aircraft Maintenance License Cat. B1 or equivalent.
Objectives: Upon completion of the course, the participants will be able to do the following tasks:
• Describe aircraft systems and their handling, using proper 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 procedure 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 in respect to fault diagnosis
and rectification
• Determine aircraft airworthiness in accordance with MEL/CDL, by using crew report
and/or on-board reporting systems
General: Closed book examinations will be conducted throughout the course.
The minimum passing mark for the exam paper is 75 %.
Participants will receive a Part-147 certificate upon successful completion of the
course.
Further
Information: For further information about this course contact:
Commercial Services, Group Technical Training
Tel. +41 43 813 1720 Fax. +41 43 812 9807
Email: technical.training@srtechnics.com
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Course Descriptions A340 (CFM56)
A340 (CFM56), T2: Part-66 Cat. B2, Line & Base Maintenance
Electrical and Avionics Systems – ATA Spec 104 Level 3
Duration: 25 days / 175 lessons theoretical training
10 days / 70 hours practical training
Target Group: Part-66 Category B2: Line and Base Maintenance Technician - avionics
Content: This course covers Avionics and Electrical elements in detail according to ATA specification
104 Level 3. The Airframe and Engine elements are covered according to ATA
Spec 104 Level 2 except FADEC and engine indication which are taught on Level 3.
Training includes:
• Description and operation of the avionics and electrical systems as well as airframe
and engine.
• Identification and location of the main components
• Servicing of the avionics and electrical systems in accordance with aircraft maintenance
manuals
• Troubleshooting of the avionics and electrical systems with the use of built-in devices
• Operational testing of the avionics and electrical systems
Number of Theoretical Minimum: 8 Practical Minimum: 4
Participants: Maximum: 15 Maximum: 6
Recommended: 10 Recommended: 5
Prerequisites: JAR/EASA Part-66 Aircraft Maintenance License Cat. B2 or equivalent.
Objectives: Upon completion of the course, the participants will be able to do the following tasks:
• Describe aircraft systems and their handling, using proper 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 procedure for removal / installation unique to the aircraft type
• Describe system 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 in respect to fault diagnosis
　
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