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EASA PART 66 MODULE 15 P4- GAS TURBINE ENGINE

EASA PART 66 MODULE 15 GAS TURBINE ENGINE PART 4
(15.12 Air Systems 15.13 Starting and Ignition Systems 15.14 Engine Indication Systems 15.15 Power Augmentation Systems 15.16 Turbo-prop Engines 15.17 Turbo-shaft engines 15.18 Auxiliary Power Units (APUs))


15.12 Air Systems 
Operation of engine air distribution and anti-ice control systems, including internal
cooling, sealing and external air services.



15.13 Starting and Ignition Systems 
Operation of engine start systems and components;
Ignition systems and components;
Maintenance safety requirements.




15.14 Engine Indication Systems
Exhaust Gas Temperature/Interstage Turbine Temperature;
Engine Thrust Indication: Engine Pressure Ratio, engine turbine discharge pressure or jet pipe pressure systems;
Oil pressure and temperature;
Fuel pressure and flow;
Engine speed;
Vibration measurement and indication;
Torque;
Power.

15.15 Power Augmentation Systems
Operation and applications;
Water injection, water methanol;
Afterburner systems.



15.16 Turbo-prop Engines 
Gas coupled/free turbine and gear coupled turbines;
Reduction gears;
Integrated engine and propeller controls;
Overspeed safety devices.

15.17 Turbo-shaft engines 
Arrangements, drive systems, reduction gearing,
couplings, control systems.


15.18 Auxiliary Power Units (APUs)
Purpose, operation, protective systems.

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