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definition
LSA as defined in 14 CFR part 1, section 1.1, “means an aircraft, other than a helicopter or powered-lift that, since its original certification, has continued to meet the following:
(1)
A maximum takeoff weight of not more than—
(i)
1,320 pounds (600 kilograms) for aircraft not intended for operation on water; or
(ii)
1,430 pounds (650 kilograms) for an aircraft intended for operation on water.
(2)
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.
(3)
A maximum never-exceed speed (VNE) of not more than 120 knots CAS for a glider.
(4) 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.
(5)
A maximum seating capacity of no more than two persons, including the pilot.
(6)
A single, reciprocating engine, if powered.
(7)
A fixed or ground-adjustable propeller if a powered aircraft other than a powered glider.
(8)
A fixed or autofeathering propeller system if a powered glider.
(9)
A fixed-pitch, semi-rigid, teetering, two-blade rotor system, if a gyroplane.
(10)
A nonpressurized cabin, if equipped with a cabin.
(11)
Fixed landing gear, except for an aircraft intended for operation on water or a glider.
(12)
Fixed or retractable landing gear, or a hull, for an aircraft intended for operation
on water.
(13)
Fixed or retractable landing gear for a glider.”
lsA Certification
Several different kinds of aircraft may be certificated as LSA. Airplanes (both powered and
gliders), rotorcraft (gyroplanes only, not true for helicopters), powered parachutes, weight-shift
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