AVIATION OCCURRENCE CATEGORIES …
Note: revision 4.1 includes two additional usage notes related to “Abnormal runway contact” and “abrupt Maneuvre” which were suggested by the SISG/4 meeting in …
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FUNDAMENTALS OF GAS TURBINE ENGINES - cast …
www.cast-safety.org1 FUNDAMENTALS OF GAS TURBINE ENGINES INTRODUCTION The gas turbine is an internal combustion engine that uses air as the working fluid. The engine extracts chemical energy from fuel and converts it to mechanical energy
AIRPLANE TURBOPROP ENGINES BASIC …
www.cast-safety.org6 ignored; but, for 10 to 15 compressor stages, it would not be efficient to have all the stages rotate at the same speed. Figure 6 showing 9 stages of an axial compressor …
PROPELLER OPERATION AND MALFUNCTIONS …
www.cast-safety.org1 PROPELLER OPERATION AND MALFUNCTIONS BASIC FAMILIARIZATION FOR FLIGHT CREWS INTRODUCTION The following is basic material to help pilots understand how the propellers on
2 engine types - CAST | Commercial Aviation Safety …
www.cast-safety.org1 INTRODUCTION TO TURBOPROP ENGINE TYPES The turbopropeller engine consists of a gas turbine engine driving a propeller. Most of the energy of the gas flow (air and burned fuel) is used to drive the
ASYMMETRIC FLIGHT - cast-safety.org
www.cast-safety.org1 ASYMMETRIC FLIGHT INTRODUCTION This section provides a discussion of the asymmetric flight of multi-engine airplanes following loss of power from an engine(s) mounted laterally either side of the centerline.
CAST/ICAO Common Taxonomy Team
www.cast-safety.orgObjective Develop common terms, definitions, and taxonomies for aviation accident/incident reporting systems to enable world-wide coordination and focus on common safety
PROPELLER OPERATION AND MALFUNCTIONS BASIC …
www.cast-safety.orgmaintain constant propeller RPM, you must adjust the pitch of the propeller blades as you change airspeed and/or engine power. The pitch is adjusted by rotating the whole blade on a bearing in the hub using an actuator that is linked to the control system. When you change the pitch, you change the "bite" that the blades make with the wind.
FUNDAMENTALS OF GAS TURBINE ENGINES
www.cast-safety.orgengine, the intake, compression, combustion, and exhaust steps occur in the same place (cylinder head) at different times as the piston goes up and down. In the turbine engine, however, these same four steps occur at the same time but in different places. As a result of this fundamental difference, the turbine has engine sections called: 1.
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