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In aviation, manufacturer's empty weight (MEW) (also known as manufacturer's weight empty (MWE)) is the weight of the aircraft "as built" and includes the weight of the structure, power plant, furnishings, installations, systems, and other equipment that are considered an integral part of an aircraft before additional operator items are added for operation.
The "Operating empty weight" (OEW) is the sum of the empty weight and the crew plus their baggage. Standard items include all structural modification or configuration orders that may have altered the MEW, including all fluids necessary for operation such as engine oil , engine coolant , water , hydraulic fluid and unusable fuel .
The empty weight of a ... (Regarding aircraft ... Note that weight of oil must be added to Licensed Empty Weight for it to be equivalent to Basic Empty Weight
The aircraft was officially launched at the annual National Business Aviation Association ... Empty weight: 8,600 lb (3,901 kg) Basic Operating; Max takeoff ...
Data from Cirrus SR20 Specifications Webpage General characteristics Crew: 1 Capacity: 3 Length: 26 ft 0 in (7.92 m) Wingspan: 38 ft 4 in (11.68 m) Height: 8 ft 11 in (2.72 m) Empty weight: 2,126 lb (964 kg) Gross weight: 3,050 lb (1,383 kg) Powerplant: 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine, 200 hp (150 kW) Propellers: 3-bladed Performance Cruise ...
The Cessna 182 is an all-metal (mostly aluminum alloy) aircraft, although some parts – such as engine cowling nosebowl and wingtips – are made of fiberglass or thermoplastic material. Its wing has the same planform as the smaller Cessna 172 and the larger 205/206 series; however, some wing details, such as flap and aileron design, are the ...
The aircraft is designed to operate from short and rough airstrips and incorporates an advanced ... Empty weight: 5,244 kg (11,561 lb) Max takeoff weight ...
The maximum zero fuel weight (MZFW) is the maximum weight allowed before usable fuel and other specified usable agents (engine injection fluid, and other consumable propulsion agents) are loaded in defined sections of the aircraft as limited by strength and airworthiness requirements.