EASA Part66 Module14 Propulsion
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This document outlines various aircraft systems and components required for different levels of aircraft maintenance licensing. It includes sections on gyroscopic principles, flight instruments, lighting systems, onboard maintenance systems, turbine engines, and engine indicating systems. It also includes a section on fundamentals of gas turbine engines that discusses energy, engine operation, and performance parameters such as thrust and efficiency.
EASA Part66 Module14 Propulsion
- 1. Level A B1 B2 Gyroscopic principles; Artificial horizons; Slip indicators; Directional gyros; Ground Proximity Warning Systems; Compass systems; Flight Data Recording systems; Electronic Flight Instrument Systems; Instrument warning systems including master warning systems and centralised warning panels; Stall warning systems and angle of attack indicating systems; Vibration measurement and indication. 13.9 Lights (ATA 33) — — 3 External: navigation, landing, taxiing, ice; Internal: cabin, cockpit, cargo; Emergency. 13.10 On board Maintenance Systems (ATA 45) — — 2 Central maintenance computers; Data loading system; Electronic library system; Printing; Structure monitoring (damage tolerance monitoring). MODULE 14 PROPULSION Level A B1 B2 14.1 Turbine Engines (a) — — 1 Constructional arrangement and operation of turbojet, turbofan, turboshaft and turbopropeller engines; (b) — — 2 Electronic Engine control and fuel metering systems (FADEC). 28.11.2003 L 315/127Official Journal of the European UnionEN
- 2. Level A B1 B2 14.2 Engine Indicating Systems — — 2 Exhaust gas temperature/Interstage turbine temperature systems; Engine speed; Engine Thrust Indication: Engine Pressure Ratio, engine turbine discharge pressure or jet pipe pressure systems; Oil pressure and temperature; Fuel pressure, temperature and flow; Manifold pressure; Engine torque; Propeller speed. MODULE 15. GAS TURBINE ENGINE Level A B1 B2 15.1 Fundamentals 1 2 — Potential energy, kinetic energy, Newton's laws of motion, Brayton cycle; The relationship between force, work, power, energy, velo- city, acceleration; Constructional arrangement and operation of turbojet, turbofan, turboshaft, turboprop. 15.2 Engine Performance — 2 — Gross thrust, net thrust, choked nozzle thrust, thrust distri- bution, resultant thrust, thrust horsepower, equivalent shaft horsepower, specific fuel consumption; Engine efficiencies; By-pass ratio and engine pressure ratio; Pressure, temperature and velocity of the gas flow; Engine ratings, static thrust, influence of speed, altitude and hot climate, flat rating, limitations. 28.11.2003L 315/128 Official Journal of the European UnionEN