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EASA Part 66 Module 11 PDF
Turbine Aeroplane, Structure and .
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Module 11: Turbine Aeroplane Aerodynamics, Structures and Systems
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EASA Part 66 Module 11 PDF Content:
11.1 Theory of Flight
airplane aerodynamics and flight controls; high speed flight.
11.2 Airframe Structures – General
airworthiness requirements and structural strength; construction methods; structural assembly techniques; methods of surface protection; surface cleaning; airframe symmetry.
11.3 Airframe Structures – Aeroplanes; ATA 52-57
fuselage; wings; stabilizers; flight control surfaces; nacelles and pylons.
11.4 Air Conditioning and Cabin Pressure; ATA 21
air supply; air conditioning; pressurization; safety and warning devices.
11.5 Instruments and Avionics Systems; ATA 31
pitot static system, gyroscopic instruments; compasses; angle of attack indication; glass cockpit; avionics systems including autoflight, communications, navigation.
11.6 Electrical Power; ATA 24
Batteries; DC and AC power generation; emergency power generation; voltage regulation; power distribution; inverters, transformers, rectifiers; circuit protection; external ground power.
11.7 Equipment and Furnishings; ATA 25
emergency equipment requirements; cabin layout; cabin entertainment; galley installation; cargo handling; airstairs.
11.8 Fire Protection; ATA 26
fire and smoke detection; fire extinguishing systems; portable fire extinguisher.
11.9 Flight Controls; ATA 27
Primary controls – aileron, elevator, rudder, spoiler; trim control; active load control; high lift devices; lift dump and speed brakes; system operation – manual, hydraulic, pneumatic, electrical, fly-by-wire; artificial feel – yaw damper, Mach trim, rudder limiter, gust lock systems; balance and rigging; stall protection.
11.10 Fuel Systems; ATA 28
system layout; fuel tanks; supply systems; dumping, venting, draining; cross feed and transfer; indications and warning; refueling and defueling; longitudinal balance.
11.11 Hydraulic Power; ATA 29
system layout; hydraulic fluids; reservoirs and accumulators; pressure generation; emergency pressure generation; filters; pressure control; power distribution; indication systems; interface with other systems.
11.12 Ice and Rain Protection; ATA 30
ice formation, classification and detection; anti-icing systems – electrical, hot air, and chemical; rain repellent; probe and drain heating; wiper systems.
11.13 Landing Gear; ATA 32
construction; shock absorbing; extension and retraction systems; indications and warning; wheels, brakes, antiskid, and autobraking; tires; steering; air-ground sensing.
11.14 Lights; ATA 33
external navigation, anti-collision, landing, taxiing, ice; internal cabin, cockpit, cargo; emergency.
11.15 Oxygen; ATA 35
system layout – cockpit and cabin; sources, storage, charging, and distribution; supply regulation; indication and warning.
11.16 Pneumatic/Vacuum; ATA 36
system layout; sources – engine/APU, compressors, reservoirs, ground supply; pressure control; distribution; indications and warning.
11.17 Water/Waste; ATA 38
system layout, supply, distribution, servicing and draining; toilet system layout, flushing and servicing; corrosion aspects.
11.18 On Board Maintenance System; ATA 45
central maintenance computers, data loading system; electronic library system; printing; structure monitoring.
11.19 Integrated Modular Avionics; ATA 42
integrated modular avionic (IMA) modules including bleed management, air pressure control, ventilation control, temperature control, air traffic communications, avionics communication router, electrical load management, electrical system BITE, fuel management, braking control, oleo pressure, gear retraction, etc; core system network components.
11.20 Cabin Systems; ATA 44
cabin core systems; in-flight entertainment; external communications; cabin mass memory system; cabin monitoring systems; miscellaneous cabin systems.
11.21 Information Systems; ATA 46
aircraft general information system; flight deck information system; maintenance information system; cabin information system; miscellaneous information systems
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