Search results
Results from the WOW.Com Content Network
The SQ2000 XP has a typical empty weight of 1,200 lb (540 kg) and a gross weight of 2,250 lb (1,020 kg), giving a useful load of 1,050 lb (480 kg). With full fuel of 42 U.S. gallons (160 L; 35 imp gal) the payload for pilot, passengers and baggage is 798 lb (362 kg).
It displaces 11,466 lb (5,201 kg) and carries 4,960 lb (2,250 kg) of lead ballast. [1] [2] The boat has a draft of 5.90 ft (1.80 m) with the standard keel. [1] [2] The boat is fitted with a Swedish Volvo Penta MD-11 diesel engine of 23 hp (17 kW) for docking and manoeuvring. The fuel tank holds 60.8 U.S. gallons (230 L; 50.6 imp gal) and the ...
Data from Jane's All The World's Aircraft 1953-54 General characteristics Crew: 2 Capacity: 4 passengers Length: 8.65 m (28 ft 5 in) Wingspan: 13.0 m (42 ft 8 in) Height: 3.19 m (10 ft 6 in) Wing area: 21.0 m 2 (226 sq ft) Empty weight: 1,490 kg (3,285 lb) Gross weight: 2,250 kg (4,960 lb) Fuel capacity: 400 L (110 US gal; 88 imp gal) Powerplant: 2 × Continental E185 air-cooled flat-six ...
Conversions between units in the metric system are defined by their prefixes (for example, 1 kilogram = 1000 grams, 1 milligram = 0.001 grams) and are thus not listed in this article. Exceptions are made if the unit is commonly known by another name (for example, 1 micron = 10 −6 metre).
Gross weight: 2,250 kg (4,960 lb) (normal max take-off weight) Max takeoff weight: 2,450 kg (5,401 lb) (overload) Fuel capacity: 315 L (83.2 US Gal) in wing tanks
The aircraft has an empty weight of 1,650 lb (750 kg) and a gross weight of 2,250 lb (1,020 kg), giving a useful load of 600 lb (270 kg). With full fuel of 50 U.S. gallons (190 L; 42 imp gal) the payload is 300 lb (140 kg). [2] [3] The aircraft proved to be stall and spin proof. Its standard day, sea level take off run is 1,200 ft (366 m) and ...
The aircraft was to have a typical empty weight of 1,250 lb (570 kg) and a gross weight of 2,250 lb (1,020 kg), giving a useful load of 1,000 lb (450 kg). With full fuel of 60 U.S. gallons (230 L; 50 imp gal) the payload for the pilot, passengers and baggage was to be 640 lb (290 kg). [1]
Max takeoff weight: 2,250 kg (4,960 lb) (external load) Fuel capacity: 700 L (150 imp gal; 180 US gal) Powerplant: 1 × Omsk TVO-100 turboshaft, 530 kW (710 hp)