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Seat maps usually indicate the basic seating layout; the numbering and lettering of the seats; and the locations of the emergency exits, lavatories, galleys, bulkheads and wings. Airlines that allow internet check-in frequently present a seat map indicating free and occupied seats to the passenger so that they select their seat from it.
The jet uses the Citation II's forward fuselage, a new carry-through section, a new laminar flow, supercritical wing developed with NASA and Boeing, and a T-tail. Powered by two 1,900 lbf (8.5 kN) Williams FJ44s , the 10,000 lb (4,500 kg) aircraft has a trailing link undercarriage for smooth landings, and can be flown by a single pilot.
[2] [3] [6] To further reduce drag, the fuselage and engine nacelle pylons were redesigned, and nacelle fairings were added. [ 2 ] [ 6 ] Fuel capacity was increased by 120 US gal (450 L). The result of the improvements was a cruise speed of 403 kn (746 km/h)—exceeding 400 kn, felt to be an important marketing benchmark by Cessna—and a range ...
An airline seat is a seat on an airliner in which passengers are accommodated for the duration of the journey. Such seats are usually arranged in rows running across the airplane's fuselage. A diagram of such seats in an aircraft is called an aircraft seat map. Within the industry, this map is known as a LOPA (Layout-Passenger Accommodation).
The Harrier, informally referred to as the Harrier jump jet, is a family of jet-powered attack aircraft capable of vertical/short takeoff and landing operations (V/STOL). Named after the bird of prey , [ 1 ] it was originally developed by British manufacturer Hawker Siddeley in the 1960s.
Various ejection seats. In aircraft, an ejection seat or ejector seat is a system designed to rescue the pilot or other crew of an aircraft (usually military) in an emergency. . In most designs, the seat is propelled out of the aircraft by an explosive charge or rocket motor, carrying the pilot with
The Gulfstream II is a twin-jet swept wing corporate transport powered by two Rolls-Royce Spey turbofan engines and designed to provide high speed and long range capability without sacrificing the airport performance, reliability, and other operational advantages of its predecessor, the turboprop Gulfstream I. Preliminary design of the wing was ...
Data from Frawley Gulfstream G200 data General characteristics Crew: 2 Capacity: Typical Seating of 8-10, 18 Max / 4,050 lb (1,840 kg) Length: 62 ft 3 in (18.97 m) Wingspan: 58 ft 1 in (17.70 m) Height: 21 ft 5 in (6.53 m) Wing area: 369 sq ft (34.3 m 2) Empty weight: 19,200 lb (8,709 kg) Max takeoff weight: 35,450 lb (16,080 kg) Powerplant: 2 × Pratt & Whitney Canada PW306A turbofans, 6,040 ...
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