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Welcome to the Dauntless Aviation Glossary!
At Dauntless, our editorial staff maintains the web's largest unified glossary of aviation terms. This glossary is built from a combination of official, quasi-official,
and proprietary sources (including original material that we develop oursselves). Uniquely, we often provide multiple definitions of a given term so that you can find that which best applies
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Light-Sport Aircraft
Light-Sport Aircraft | | Light-sport aircraft means an aircraft, other than a helicopter or powered-lift that, since its original certification, has continued to meet the following: - A maximum takeoff weight of not more than—
- 1,320 pounds (600 kilograms) for aircraft not intended for operation on water; or
- 1,430 pounds (650 kilograms) for an aircraft intended for operation on water.
- A maximum airspeed in level flight with maximum continuous power (VH) of not more than 120 knots CAS under standard atmospheric conditions at sea level.
- A maximum never-exceed speed (VNE) of not more than 120 knots CAS for a glider.
- A maximum stalling speed or minimum steady flight speed without the use of lift-enhancing devices (VS1) of not more than 45 knots CAS at the aircraft's maximum certificated takeoff weight and most critical center of gravity.
- A maximum seating capacity of no more than two persons, including the pilot.
- A single, reciprocating engine, if powered.
- A fixed or ground-adjustable propeller if a powered aircraft other than a powered glider.
- A fixed or feathering propeller system if a powered glider.
- A fixed-pitch, semi-rigid, teetering, two-blade rotor system, if a gyroplane.
- A nonpressurized cabin, if equipped with a cabin.
- Fixed landing gear, except for an aircraft intended for operation on water or a glider.
- Fixed or retractable landing gear, or a hull, for an aircraft intended for operation on water.
- Fixed or retractable landing gear for a glider.
| source: FAA Federal Aviation Regulations (CFR 14 Part 1) |
| | LIGHT-SPORT AIRCRAFT (LSA): (Refer to 14 CFR Part 1, ?1.1.) An FAA-registered aircraft, other than a helicopter or powered-lift, that meets certain weight and performance. Principally it is a single engine aircraft with a maximum of two seats and weighing no more than 1,430 pounds if intended for operation on water, or 1,320 pounds if not. They must be of simple design (fixed landing gear (except if intended for operations on water or a glider) piston powered, non-pressurized, with a fixed or ground adjustable propeller), Performance is also limited to a maximum airspeed in level flight of not more than 120 knots CAS, have a maximum never-exceed speed of not more than 120 knots CAS for a glider, and have a maximum stalling speed, without the use of lift-enhancing devices (VS1 ) of not more than 45 knots CAS. They may be certificated as either Experimental LSA or as a Special LSA aircraft. A minimum of a sport pilot certificate is required to operate light-sport aircraft. | source: FAA Pilot/Controller Glossary |
| | Light-Sport Aircraft (LSA): An aircraft that meets the requirements defined in 14 CFR section 1.1, regardless of airworthiness certification. | source: FAA Weight Shift Control Handbook (FAA-H-8083-5) |
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Disclaimer: While this glossary in most cases is likely to be highly accurate and useful, sometimes, for any number of editorial, transcription, technical, and other reasons, it might not be.
Additionally, as somtimes you may have found yourself brought to this page through an automated term matching system, you may find definitions here that do not match the cotext or application in which
you saw the original term. Please use your good judgement when using this resource.
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