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A220 Continuation Training

£375.00

Our Courses Scale Perfectly To Any Device

 

About our Online Self-Study Course

The A220 Continuation Training course with PW1500G powerplants, has been designed to give you a complete technical refresher of all aircraft systems and meets ATA 104 Specification Level 1 and EASA Part 66 Level 1 as a minimum. The A220 Continuation Training course with PW1500G powerplants, covers all mechanical and avionics systems. We also include links to any relevant incidents, Airworthiness Directives and maintenance incidents. The final chapter covers new relevant aviation technology. This self–study online A220 Continuation Training course with PW1500G powerplants, will take approximately 40 hours of study. Students must pass the multi-choice question at the end of each ATA chapter before the next ATA chapter is unlocked. A completion certificate is issued on successful completion of the course.

 

You have 12 months from enrollment to begin the course and after starting, 6 months to complete the course. You have a further 90 days to review the course after completion.

 

Click on the DESCRIPTION below for course syllabus and more details. Please click here to view our sample course.

 

When checking out, please ensure you use the student’s name. To enroll multiple students in the same course, please make separate transactions or contact us for team discounts.

Description

A220 CONTINUATION TRAINING COURSE WITH PW1500G POWERPLANTS

 

ABOUT

The A220 Continuation Training course with PW1500G powerplants, meets a minimum of ATA 104 Specification Level I; A brief overview of the airframe, systems and powerplant as outlined in the Systems Description Section of the Aircraft Maintenance Manual.

The A220 Continuation Training course with PW1500G powerplants, also complies with EASA’s knowledge LEVEL 1 definition as contained in Regulation EU No. 1321/2014, Part 66, Appendix III Basic Knowledge Requirements;
A familiarization with the principal elements of the subject, with the objective;
(a) The applicant should be familiar with the basic elements of the subject.
(b) The applicant should be able to give a simple description of the whole subject, using common words and examples.
(c) The applicant should be able to use typical terms

This self-study online A220 Continuation Training course with PW1500G powerplants, will take approximately 40 hours of study. Students must pass a quiz at the end of each ATA chapter before the following ATA chapter is unlocked. A completion certificate is issued on successful completion of the course.

Course objectives: upon completion of the course, the student will be able to identify safety precautions related to the airframe, it’s systems and powerplant.
Identify maintenance practices important to the airframe, it’s systems and powerplant
Define the general layout of the aircraft’s major systems.
Define the general layout and characteristics of the powerplant.
Identify special tooling and test equipment used with the aircraft.

 

SYSTEM REQUIREMENTS
Our courses scale perfectly to PC, Laptop, tablet, android and iPhone. You must have an internet connection to use our courses.

 

STUDY TIME
Course completion time varies with the individual; however, we estimate approximately 40 hours will be required. You have 6 months to complete the course and can stop and restart at the same position with your progress saved. Once completed you will have a further 90 days to review the course.

 

SUPPORT
Should you require any assistance during your course, please contact us and we will assist you during normal working hours.

 

WHY USE OUR REFRESHER & CONTINUATION COURSES?
Our online A220 Continuation Training course with PW1500G powerplants, provides an excellent solution for training engineers or company support staff, giving the required in-depth aircraft type knowledge with the advantage of distance learning. Our courses are designed to provide a method for maintenance companies to comply with National Aviation Authority continuation training requirements such as EASA’s part 145.A.35 and the FAA’s Federal Reglation 145.163.

 

WHY BUY FROM US?
Our A220 Continuation Training course with PW1500G powerplants, is designed and produced by EASA and UK CAA B1/B2 Engineers, Type instructors and Part 147 Training Managers. We ensure each course covers all relevant ATA chapters.

 

DETAILED COURSE SYLLABUS

 

ATA 01-00 – AIRCRAFT GENERAL.

 

ATA 00-00 – DOCUMENTATION.

 

ATA 05-00 – SCHEDULED/UNSCHEDULED MAINTENANCE.

 

ATA 06-00 – DIMENSIONS/AREAS.

 

ATA 07-00 – LIFTING, SHORING, RECOVERING, AND TRANSPORTING.

 

ATA 08-00 – LEVELLING AND WEIGHING

ATA 09-00 HANDLING AND MANOEUVRING -Towing, Landing Gear Downlock Safety Pins, Taxiing, A220-100 Turning Radius, A220-300 Turning Radius, Hazard Areas, Engine lntake and Exhaust Hazard Areas, Parking, Mooring, Storing, and Return to Service, Covers and Plugs, Exterior Plugs, Grounding, Landing Gear Grounding Studs.

 

ATA 11 -00 PLACARDS AND MARKINGS – External Placards and Markings, lnterior Placards.

 

ATA 12-00 SERVICING – Servicing Panels and Doors, Ground Support Equipment Placement.

 

ATA 21 AIR CONDITIONING – Control System, Air Conditioning Pack, Recirculation Air Distribution System, Trim Air, Temperature Control System, Cabin Air Distribution, Heating, Flight Crew Floor Heating, Galley Heating System, Equipment Cooling Overview, Air lnlet Cooling System, Air Extraction System, Backup Exhaust System, Cabin Pressure Control System, Controls and lndications, Controls, lndications.

 

ATA 22 AUTOFLIGHT – Flight Guidance, Autopilot, Autoland, Autothrottle, Controls and lndications, Flight Control Panel, Primary Flight Displays.

 

ATA 23 COMMUNICATION – Communication Management, Tuning and Controls, Radio Management System, Audio lntegrating System, Audio lntegrating System, Voice Communication, VHF and HF (Optional) Communication System, Data Communication, Selective Calling System, Airborne Data link System, Flight Deck Printer, Cockpit Voice Recorder, Static Discharging.

 

ATA 24 ELECTRICAL POWER – Electrical Power Generation System, AC Electrical Power Generation System, DC Power Generation, Power Distribution System, Emergency Electrical Generation System, Ram Air Turbine, Controls and lndications, Electrical Panel, Electrical Service Panel, Electrical Synoptic Page, Circuit Breaker Application, Special Tools, Safety.

 

ATA 25 EQUIPMENT AND FURNISHING – Flight Deck, Passenger Cabin, Galleys, Lavatories, Emergency Equipment, Emergency Locator Transmitter, Escape Slides.

 

ATA 26 FIRE PROTECTION – Fire Detection Areas, Fire Extinguishing Areas, FIDEX Control Unit, Engine Fire Detection and Extinguishing, Auxiliary Power Unit Fire Detection and Extinguishing, Main Wheel Weil Overheat Detection, Avionics and Electrical Bay Smoke Detection, Cargo Smoke Detection and Fire Extinguishing, Lavatory Smoke Detection and Fire Extinguishing, Portable Fire Extinguishers.

 

ATA 27 FLIGHT CONTROLS – Fly-By-Wire, Electronic Flight Control System Controls, Sidestick Controllers, Primary Flight Controls Panel, Flight Controls lndications, Electronic Flight Control System, Normal Mode, EFCS – Alternate Flight Control Unit Direct Mode, Electronic Flight Control System Surface Actuation, Non-Electronic Flight Control System, High Lift System, High Lift System Control, Lift System Architecture.

 

ATA 28 FUEL – Fuel Quantity Computer, Fuel Storage, Vent System, Refuel/Defuel System, Refuelling, Defueling, Engine Fuel Feed, APU Fuel Feed, Fuel Transfer System, Fuel lndicating, Controls and lndications, Safety.

 

ATA 29 HYDRAULICS – Hydraulic System No. 1, No. 2 and No. 3, Controls and lndications, Hydraulic Panel, Hydraulic Synoptic Page, Servicing, Safety.

 

ATA 30 ICE AND RAIN PROTECTION – Ice Detection System, Wing Anti-lce System, Cowl Anti-lce System, Probe Heat System, Windshield and Side Window Heating System, Windshield Wiper System, Controls and lndications, lndications.

 

ATA 31 INDICATING/ RECORDING SYSTEMS – Instruments and Control Panels, Controls and lndications, introduction to AFDX, lntegrated Avionics Processing, Electronic Flight Instrument System, Controls and lndications, Engine Indication and Crew Alerting System, Controls and Indications, Flight Data Recorder.

 

 ATA 32 LANDING GEAR – Landing Gear, Extension and Retraction, Extension and Retraction – Uplock Actuators, landing Gear Indicating System, Wheels and Brakes l Wheels, Brakes, Nosewheel Steering System, Controls and Indications, Flight Deck Controls, External Controls, Indications.

 

ATA 33 LIGHTING SYSTEM – Flight Deck Lighting, Passenger Cabin lighting, General Cabin lights, Emergency Lighting, Emergency Power Supply Units, Controls and lndications, Exterior lights, Cargo Compartment lights, Service and Maintenance lighting.

 

ATA 34 NAVIGATION – Air Data System, lnertial Reference System, Standby Flight Instrument System, Standby Compass, Navigation Tuning l Manual Tuning, Autotuning, VHF Navigation System, Instrument landing System and Marker Beacon, Distance Measuring Equipment System, Global Navigation Satellite System, Radio Altimeter System, Weather Radar System, Terrain Awareness and Warning System, Traffic Surveillance System, Flight Management System.

 

ATA 35 OXYGEN – Crew Oxygen, Passenger Oxygen, Portable Oxygen.

 

ATA 36 PNEUMATIC – lntegrated Air Management System, Pneumatics, Bleed Air Sources, Engine Bleed Air, APU Bleed Air, High-Pressure Ground Connection, Bleed Air Leak and Overheat Detection System, Controls and Indications.

 

ATA 38 WATER AND WASTE – Potable Water System, Gray Water Drains, Vacuum Waste System, Controls and Indications.

 

ATA 44 CABIN SYSTEMS – Cabin Management System, Aircraft Systems, Cabin and Passenger Functions, Onboard Communication, Emergency Evacuation System, ln-flight Entertainment and Connectivity System.

 

ATA 45 CENTRAL MAINTENANCE SYSTEM – A220 Series Maintenance Philosophy, Onboard Maintenance System, Onboard Diagnostics, Aircraft Condition Monitoring, Configuration and Reporting.

 

ATA 46 INFORMATION SYSTEMS – Information Management System, Aircraft Health Management System, Health Management Unit, Aircraft Network Switch.

 

ATA 47 FUEL TANK LNERTING SYSTEM – Fuel Tank lnerting System Concept, System Generation, Distribution.

 

ATA 49 AIRBORNE AUXILIARY POWER – APU Construction, General Description, Power Section, Load Compressor Section, Accessory Gearbox, Installation, APU Oil System, APU Fuel System, APU Starting and lgnition, APU Air System, Controls and lndications, EICAS and Status Pages.

 

ATA 50 CARGO COMPARTMENTS – Forward Cargo Compartment, AFT Cargo Compartment, Compartment Nets.

 

ATA 51 STANDARD PRACTICES STRUCTURES – Aircraft Structure Repair Publication, Standard Practices – Structures, AMM 51-10-00 lnvestigation, Clean-up, and Aerodynamic Smoothness, Damage Assessment, Permitted Damage, Repairable Damage, Composite Damage Assessment.

 

ATA 52 DOORS PASSENGER AND SERVICE DOORS – Overwing Emergency Exit Doors, Cargo Compartment Doors, Equipment Bay Doors, Flight Crew, Flight Deck Remote Access System, Controls and lndications.

 

ATA 71 POWER PLANT – Power Plant Subsystems, Nacelle Systems, Power Door Operating System, Engine Mounts and Pylons, Engine Fuel and Control, Fuel Distribution System, FADEC Control System, Fuel lndicating, lgnition and Starting, Engine Cooling, Turbine Active Clearance Control, Engine Controls, Engine lndicating System, Exhaust, Thrust Reverser Actuation System, Thrust Reverser Control, Thrust Reverser lndicating, Oil, Starting.

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