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A typical light aircraft: the Cessna 172 With a maximum gross takeoff weight of 12,500 lbs, the DHC-6 Twin Otter is an example of the upper limit of the light aircraft category. A Robinson R44 light helicopter. A light aircraft is an aircraft that has a maximum gross takeoff weight of 12,500 lb (5,670 kg) or less. [1]
Jets with 10 or more passenger seats or maximum takeoff weights greater than 12,500 lb (5700 kg); or; Modern propeller-driven airplanes with more than 19 passenger seats or a MTOW greater than 19,000 lb (8618 kg); or; Older propeller-driven airplanes with MTOW greater than 12,500 lb (e.g. Boeing 247 13,650 lb, CASA C-212 Aviocar 17,000 lb)
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The pound or pound-mass is a unit of mass used in both the British imperial and United States customary systems of measurement.Various definitions have been used; the most common today is the international avoirdupois pound, which is legally defined as exactly 0.453 592 37 kilograms, and which is divided into 16 avoirdupois ounces. [1]
The Learjet 24 was designed as an improved version of the Learjet 23, which was limited to 12,500 pounds (5,700 kg) gross weight. Engineers designed the model 24 to accept up to the full 13,500 pounds (6,100 kg) gross weight permitted by FAR-25 standards. Other improvements introduced in the Learjet 24 included:
The American Federal Aviation Administration defines a large aircraft as any aircraft of more than 12,500 pounds (5.7 tonnes) maximum certificated takeoff weight. [ 1 ] The European Aviation Safety Agency (EASA) defines a large aircraft as either "an aeroplane with a maximum take-off mass of more than 5,700 kilograms (12,600 pounds), a multi ...
The slug is a derived unit of mass in a weight-based system of measures, most notably within the British Imperial measurement system and the United States customary measures system. Systems of measure either define mass and derive a force unit or define a base force and derive a mass unit [ 1 ] (cf. poundal , a derived unit of force in a mass ...
Jets with 10 or more seats or a maximum takeoff weight (MTOW) greater than 12,500 pounds (5,670 kg); or; Propeller-driven airplanes with greater than 19 seats or a MTOW greater than 19,000 pounds (8,618 kg). This Part is organized into six subparts, to specify design criteria for each of A – General; B – Flight; C – Structure