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  • Chapter 7: Aircraft Systems › Starting System

    starter engages the aircraft flywheel, rotating the engine at a speed that allows the engine to start and maintain operation. Electrical power for starting is usually supplied by an onboard battery, but can also be supplied by external power through ... starter switch draw current from the main bus bar, but the starter will not operate until the starting solenoid is energized by the starter switch being turned to the “start” position. When the starter switch is released from the “start…

  • Chapter 7: Aircraft Systems › Turbine Engines › Foreign Object Damage (FOD)

    deflectors, may also be utilized. Preflight procedures include a visual inspection for any sign of FOD. Turbine Engine Hot/Hung Start When the EGT exceeds the safe limit of an aircraft, it experiences a “hot start.” This is caused ... much fuel entering the combustion chamber or insufficient turbine rpm. Any time an engine has a hot start, refer to the AFM/POH or an appropriate maintenance manual for inspection requirements. If the engine fails to accelerate to the proper speed…

  • Chapter 7: Aircraft Systems › Flameout › Performance Comparison

    purposes only and is not for specific models of engines. The following are the four types of engines: • Reciprocating powerplant • Turbine, propeller combination (turboprop) • Turbine engine incorporating a fan (turbofan) • Turbojet (pure jet) By plotting the performance curve for each ... means of comparison, numerical values for net thrust, aircraft speed, and drag are not included. Comparison of the four powerplants on the basis of net thrust makes certain performance capabilities evident. In the speed range shown to the left…

  • Chapter 3: Aircraft Construction › Alternate Types of Wings › The Powerplant

    Powerplant The powerplant usually includes both the engine and the propeller. The primary function of the engine is to provide the power to turn the propeller. It also generates electrical power, provides a vacuum source for some flight instruments…

  • Chapter 9: Flight Manuals and Other Documents › Powerplant

    Powerplant The Powerplant Limitations portion describes operating limitations on an aircraft’s reciprocating or turbine engine(s). These include limitations for takeoff power, maximum continuous power, and maximum normal operating power, which is the maximum power the engine can produce…

  • Chapter 10: Engine Maintenance & Operation › Engine Troubleshooting

    impractical to list all the malfunctions that could occur in a reciprocating engine, so only the most common malfunctions are discussed. A thorough knowledge of the engine systems, applied with logical reasoning, solves most problems that may occur. Figure ... lists general conditions or troubles that may be encountered on reciprocating engines, such as engine fails to start. They are further divided into the probable causes contributing to such conditions. Corrective actions are indicated in the remedy column. The items…