The Airbus A330 CF6 Continuation Training Course is designed to provide a comprehensive overview of the airframe, systems, and powerplant, following ATA 104 standards. The course meets EASA Part 66 Level 1 requirements as per EU Regulation No. 1321/2014. Participants will gain a thorough understanding of key systems, maintenance practices, and the general layout of the aircraft.

This self-paced course is estimated to take approximately 40 hours to complete. A quiz at the end of each ATA chapter ensures participants’ understanding before moving to the next chapter. A completion certificate will be issued upon successful course completion.

Course Objectives:

• Identify safety precautions related to the airframe, systems, and powerplant.
• Define the general layout and characteristics of the aircraft’s major systems.
• Understand the powerplant’s layout and operational characteristics.
• Recognize important maintenance practices and special tooling/equipment for the aircraft.

SYSTEM REQUIREMENTS This course is compatible with PCs, laptops, tablets, Android, and iPhone devices. An internet connection is required for access and completion.

STUDY TIME Estimated completion time: approximately 40 hours. Students have 6 months to finish the course, with progress saved automatically. After completion, students have 90 days to review the material.

SUPPORT For assistance during the course, students can contact us during normal working hours.

WHY USE OUR REFRESHER & CONTINUATION COURSES? Our Airbus A330 CF6 Continuation Training Course offers in-depth aircraft type knowledge through flexible online learning. The course meets EASA Part 145.A.35 and FAA Regulation 145.163 requirements, making it an excellent choice for training engineers and company support staff.

WHY TRUST US WITH YOUR TRAINING? Our courses are developed by EASA and UK CAA B1/B2 Engineers, Type Instructors, and Part 147 Training Managers. Every ATA chapter is covered in detail, ensuring regulatory compliance and delivering comprehensive knowledge of the aircraft.

ATA Chapters Overview:

• ATA 00-12: GENERAL – Aircraft Servicing
  • This chapter covers fundamental aircraft servicing procedures, including handling, service points, and arrangements for jacking, leveling, and weighing. Also included are guidelines for towing, taxiing, parking, and mooring, with special emphasis on safety precautions for engine dangerous areas.
• ATA 31: INDICATING/RECORDING SYSTEM
  • Focuses on cockpit instrumentation, including the Electronic Instrument System (EIS), Electronic Centralized Aircraft Monitoring (ECAM), Flight Data Interface Management Unit (FDIMU), and flight data recorders (DFDRS). Maintenance, control, and test procedures are covered in detail to ensure system integrity.
• ATA 45: ONBOARD MAINTENANCE SYSTEM
  • This section describes the onboard Central Maintenance System (CMS), how data is uploaded and downloaded, report printing capabilities, and controls through the Multifunction Control and Display Unit (MCDU). It includes detailed guidance on maintenance and test facilities.
• ATA 24: ELECTRICAL POWER SYSTEM
  • Covers the electrical power generation and distribution systems, including both AC and DC power, APU start power, and the emergency power system (RAT). It also includes maintenance, troubleshooting, and test procedures for power management systems.
• ATA 34: NAVIGATION SYSTEM
  • Focuses on navigation systems such as the Air Data/Inertial Reference System (ADIRS), GPS, radio altimeter, VOR/DME/ADF, Enhanced Ground Proximity Warning System (EGPWS), and Traffic Collision Avoidance System (TCAS). It includes detailed coverage of standby instruments, maintenance, and test facilities.
• ATA 22: AUTO FLIGHT SYSTEM
  • Describes the aircraft’s automatic flight control systems, including autopilot, autothrottle, and flight director. Panel layout, system controls, fault isolation, and maintenance procedures are detailed to ensure smooth flight operations.
• ATA 23: COMMUNICATION SYSTEMS
  • This chapter explains cockpit communication systems (VHF, HF, SATCOM), the Cabin Intercommunication Data System (CIDS), and Passenger Address Systems. It covers the Solid-State Cockpit Voice Recorder (SSCVR) and data-link systems used for communication between the flight deck and ground.
• ATA 46: INFORMATION SYSTEMS
  • Focuses on the Aircraft Information Management System (AIMS), FlySmart with Airbus (FSA), and the Airline Network Architecture (ALNA). Maintenance and troubleshooting methods for these systems are included.
• ATA 33: LIGHTING SYSTEM
  • This chapter covers both internal and external lighting systems, including cockpit, cabin, and cargo compartment lighting. Emergency lighting systems are also covered, with details on control, indication, and maintenance procedures.
• ATA 29: HYDRAULIC POWER SYSTEM
  • The hydraulic system is essential for operating the aircraft’s primary flight controls, landing gear, and brakes. This chapter explains the layout and functioning of the Green, Yellow, and Blue hydraulic systems, including engine-driven pumps (EDPs), Power Transfer Unit (PTU), and Ram Air Turbine (RAT).
• ATA 32: LANDING GEAR SYSTEM
  • Describes the extension and retraction systems for the landing gear, including braking systems (normal and alternate), steering systems, and brake temperature monitoring. Detailed procedures for maintenance and testing are also provided.
• ATA 27: FLYING CONTROLS SYSTEM
  • This chapter covers the aircraft’s fly-by-wire control system, flight control laws, and mechanical backups. It also explains the functioning of slats, flaps, spoilers, and actuators, along with detailed maintenance and test procedures.
• ATA 51: STRUCTURES
  • Focuses on the structural components of the aircraft, including the fuselage, wings, pylons, stabilizers, and doors. It includes guidelines for maintaining and repairing composite materials used in modern aircraft structures.
• ATA 52: DOORS SYSTEM
  • Covers the operation and maintenance of the aircraft’s passenger, cargo, and emergency doors. It also includes escape slide systems and controls for the Doors and Escape Slides Control System (DSCS).
• ATA 25: EQUIPMENT AND FURNISHINGS
  • This section describes the cockpit and cabin furnishings, emergency equipment, lavatories, and galleys. It also includes information on galley trolley cooling systems and equipment cooling.
• ATA 35: OXYGEN SYSTEMS
  • Covers the oxygen systems used for the cockpit crew and passengers, including portable oxygen units. Procedures for system control, indication, and maintenance are detailed.
• ATA 38: WATER AND WASTE SYSTEM
  • Explains the potable water system and vacuum waste system, covering both waste disposal and water supply systems. Maintenance and control indications are also covered.
• ATA 28: FUEL SYSTEM
  • This chapter provides an overview of the fuel system, including fuel storage, transfer, and refuel/defuel operations. It also covers fuel tank safety, component location, and detailed maintenance procedures.
• ATA 26: FIRE PROTECTION SYSTEM
  • Covers the fire protection systems for engines, auxiliary power units (APU), avionics compartments, and cargo compartments. Smoke detection systems, fire extinguishing procedures, and lavatory fire protection are also included.
• ATA 49: APU SYSTEM
  • Describes the installation, operation, and maintenance of the auxiliary power unit (APU). Procedures for APU testing, control, and indications are detailed.
• ATA 71: POWERPLANT
  • This chapter covers the installation, operation, and maintenance of the aircraft’s engines, including the FADEC system, fuel system, oil system, cooling, and thrust reverser systems. It also provides details on engine preservation and maintenance.
• ATA 36: PNEUMATIC SYSTEM
  • Explains the pneumatic system used for aircraft pressurization and air distribution, covering sources, users, and leak detection. Detailed procedures for maintenance and testing are provided.
• ATA 21: AIR CONDITIONING SYSTEM
  • Covers the air conditioning and pressurization systems, including temperature control, ventilation, and avionics cooling. Maintenance facilities and procedures are also included.
• ATA 47: FUEL TANK INERTING SYSTEM
  • Describes the system used to inert fuel tanks, ensuring safety by reducing the risk of combustion. Maintenance and testing procedures for the system are outlined.
• ATA 30: ICE & RAIN PROTECTION SYSTEM
  • This chapter explains the systems used to protect against ice accumulation and rain, including wing anti-icing, windshield anti-icing, and rain protection systems. Maintenance and testing are also covered.