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The business was a small supplemental carrier that had two 94-passenger Lockheed L-188 Electra four-engine turbo-prop passenger aircraft. [3] More importantly, it held a supplemental air carrier operating certificate which allowed it to operate as an airline. After significant deliberation, the Civil Aeronautics Board approved the transfer in 1975.
The CoAX 2D/2R was originally known as the FLIP 2 (Fly In Perfection) and is a derivative of the FLIP 1, a conventional helicopter with a main and tail rotor.[1]The CoAX 2D/2R was designed to comply with the European Class 6 microlight helicopter rules, including the category's maximum takeoff weight of 450 kg (992 lb).
Chosen to replace the HH-3F Pelican, the MH-60T is a member of the Sikorsky S-70 family of helicopters and is based on the United States Navy's SH-60 Seahawk helicopter. [1] Development began in September 1986, first flight was achieved on 8 August 1989, and the first HH-60J entered USCG service in June 1990.
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The Helicycle is a single-seat, semi-rigid two-bladed main rotor, helicopter powered by a Solar T62-32 engine. Manufactured by Helicycle Ventures LLC in Mesilla, New Mexico as a kit, the aircraft is intended to be assembled by the owner and is considered a homebuilt aircraft.
The passenger seat on the left can be removed if unnecessary or for greater storage space within the cabin. [23] Various features for personal helicopter usage, such as an externally accessible 200-litre baggage compartment, power sockets within the main cabin, leather seating, and incidental under-seat storage, are also present.
List of single seat helicopters is a list of helicopters with one seat. They may or may not be ultralight aircraft. Some single seat helicopters are evtols. [1] Adams-Wilson Hobbycopter; Airbus A³ Vahana (eVTOL) American Helicopter XH-26 Jet Jeep; Baumgärtl Heliofly III; Chrysler VZ-6; Curtiss-Wright VZ-7; De Lackner HZ-1 Aerocycle; Eagle ...
Sikorsky developed the X2 helicopter on a $50 million budget. The design includes expertise gathered from several earlier design projects. The S-69/XH-59A Advancing Blade Concept Demonstrator had shown that high speed was possible with a coaxial helicopter with auxiliary propulsion supplied using two jet engines, but that vibration and fuel consumption was excessive; [2] [3] [4] the Cypher UAV ...