BOEING 737-300/400/500 GENERAL FAMILIARIZATION COURSE WITH CFM56 POWERPLANTS

ABOUT

Our Boeing 737-300/400/500 General Familiarisation course with CFM56 Powerplants, meets ATA 104 Specification Level I: General Familiarisation; A brief overview of the airframe, systems and powerplant as outlined in the Systems Description Section of the Aircraft Maintenance Manual.

The Boeing 737-300/400/500 General Familiarisation course with CFM56 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 Boeing 737-300/400/500 General Familiarisation course with CFM56 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 GENERAL FAMILIARIZATION COURSES?
Our online Boeing 737-300/400/500 General Familiarisation course with CFM56 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.

WHY BUY FROM US?
Our Boeing 737-300/400/500 General Familiarisation course with CFM56 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

The Boeing 737-300/400/500 General Familiarisation course with CFM56 Powerplants, begins with an aircraft type introduction, then covers each ATA chapter to approximately Part 66 Level 1;

ATA 00 -12 – Lifting and Shoring, Levelling and Weighing, Towing and Taxiing, Parking Mooring, Servicing.

ATA 22 AUTO FLIGHT – Flight Management System – Built -In Test Equipment, Flight Management Computer System Built -In Test Equipment, Digital Flight Control System – Built -In Test Equipment, Autothrottle System – Built -In Test Equipment, Inertial Reference System – Built -In Test Equipment, Flight Management System Sensor – Built -In Test Equipment, Electronic Flight Instrument System, Digital Flight Control System, Yaw Damper System, Mach Trim, Autothrottle System.

ATA 23 COMMUNICATIONS – Speech Communication, HF Communication System, VHF Communication System, Emergency Locator Transmitter, Aircraft Communications Addressing and Reporting System (ACARS), SELCAL System, Passenger Address System, Passenger Entertainment System, Passenger Video System, Cabin Video Information System, Service Interphone System, Flight and Ground Crew Call System, Flight Interphone System, Static Discharger, Voice Recorder System.

ATA 24 ELECTRICAL POWER – Electrical Power Precautions, AC Generator Drive System, AC Generation System, Manual Control (Apply Power), DC Generation System, AC External Power, Electrical Load Distribution, Main 115-Volt AC Power Distribution, 28-Volt AC Power Distribution, Standby Power System, DC Power Distribution.

ATA 25 EQUIPMENT/FURNISHINGS – Equipment Ano Furnishing, Cabin Accommodations, Flight Compartment, Flight Compartment Equipment, Passenger Compartment, Seats – Passenger, Service Units, Galleys, Lavatories, Lavatory Area, Electronic Compartment, Cargo Compartments.

ATA 26 FIRE PROTECTION – Detection, Engine Fire Detection System, Lavatory Smoke Detection System, APU Fire Detection System, Detection System – Cargo Compartment Smoke, Wheel Well Overheat Detection System, Wing and Lower Aft Body Overheat Detection System, Extinguishing, Engine Fire Extinguishing System, APU Fire Extinguishing System, Extinguishing System – Cargo Compartment Fire, Lavatory Fire Extinguishing System, Portable Fire Extinguishers.

ATA 27 FLIGHT CONTROLS – Flight Controls Multiple Use Systems/ Units, Aileron and Aileron Trim Control System, Rudder and Rudder Trim Control System, Elevator and Tab Control System, Stall Warning System, Horizontal Stabilizer Trim Control System, Trailing Edge Flap System, Trailing Edge Flap, Flight Spoiler Control System, Speed Brake Control System, Leading Edge Flap and Slat Control System, Leading Edge Auto-slat System, Position Indicating System – Leading Edge Flap And Slat.

ATA 28 FUEL – Fuel Tanks, Integral Fuel Tanks, Fuel Vent System, Auxiliary Fuel Tank, Centre Tank Fuel Scavenge System, Pressure Fuelling System, Engine Fuel Feed System, Defueling, Fuel Quantity Indicating System, Fuel Feed Low Pressure Indicating System, Fuel Temperature Indicating System.

ATA 29 HYDRAULIC POWER – Hydraulic Reservoir Pressurization System, Hydraulic Systems A, B, and Standby, Ground Servicing System, Power Transfer Unit (PTU) – Hydraulic, Hydraulic Pressure Indicating System, Hydraulic Fluid Overheat System, Hydraulic Fluid Quantity Indicating, Pump Low-Pressure-Warning System.

ATA 30 ICE AND RAIN PROTECTION – Ice and Rain Multiple Use Systems/Components, Wing Thermal Anti-icing System, Inlet Cowl Anti-icing System, Pitot-Static Tubes, Temperature Probe and Alpha Vane Anti-icing System, Control Cabin Window Anti-icing System, Windshield Wiper System, Rain Repellent System, Water and Toilet Drain Anti-icing System.

ATA 31 FLIGHT DATA RECORDER SYSTEM – Clocks, Aural Warning System, Engine Instrument System, Engine Instrument System, Display- EIS Primary, Display- EIS Secondary.

ATA 32 LANDING GEAR – Landing Gear Safety Sensors, Main Gear,  Nose aanding Gear, Nose Gear Doors, Landing Gear Control System, Main Gear Extension and Retraction, Nose Gear Extension And Retraction, Main Gear Manual Extension System, Nose Gear Manual Extension System, Wheels and Brakes, Hydraulic Brake System, Antiskid System, Automatic Braking System, Parking Brake System, Tires and Wheels, Nose Wheel Steering System, Landing Gear Position Indicating And Warning System, Tail Skid.

ATA 33 LIGHTS – Flight Compartment Lighting, Master Warning and Caution Lights, Passenger Compartment Lighting, Passenger Compartment Lights, Reading Lights, Passenger Signs, Call Lights, Lavatory Lights, Galley Lights, Cargo and Service Compartment Lighting, Exterior Lighting, Wing Scanning Lights, Landing, Runway Turnoff and Nose Gear Taxi Lights, Steady Position (Navigation) Lights, Anticollision Lights, Strobe Position Lights, Logo Lights, Emergency Lights.

ATA 34 NAVIGATION SYSTEMS – Pitot-Static System, Air Data System, Mach Airspeed Warning System, Altitude Alerting System, Electronic Flight Instrument System, Magnetic Standby Compass, Standby Horizon System, Inertial Reference System, Instrument Comparator System, VOR/ILS Navigation System, Marker Beacon System, Weather Radar System, GPWS, TCAS, Low Range Radio Altimeter System, ATC System, DME System, Automatic Direction Finder System, Global Positioning System, Flight Management Computer System.

ATA 35 OXYGEN SYSTEMS – Flight Crew Oxygen System, Passenger Oxygen System, Portable Oxygen Equipment.

ATA 36 PNEUMATIC SYSTEM – Engine Bleed Air, Bleed Air, Ducts, Duct Pressure.

ATA 36 WATER AND WASTE – Potable Water System, Waste Water System, Toilet System, Water Tank Pressurization System.

ATA 49 AIRBORNE AUXILIARY POWER, APU Power Plant, Shroud, Mounts, Air Inlet, Shroud Drains, Engine, Fuel System, Ignition and Start System, Cooling Air System, Bleed Air System, Controls, Exhaust Gas Temperature Indicating System, Indicating System, Exhaust System, Lubrication System, Oil Indicating System.

ATA 52 DOORS – Main Entry Doors, Forward Entry Door, Aft Entry Door, Emergency Exits, Emergency Exit Hatch, Cargo Compartment Doors, Galley Service Doors, Access Doors, Miscellaneous Exterior Service Doors, Fixed Interior, Control Cabin Door, Forward Airstair and Door, Door Warning System.

ATA 71 POWERPLANT – Engine, Engine Fuel and Control, Ignition, Air, Engine Controls, Engine Indicating, Exhaust, Oil, Starting.