Category: Uncategorized

  • Embraer 135

    Embraer 135

    Information and specifications Role Regional jet First Flight August 11, 1995 Introduction December 1996 Origin Brazil Company Embraer Status In service Produced 1989-present Number built 890 (2012 survey) Capacity 37 Competitors Bombardier CRJ Variants R-99 P-99

  • Cessna T-50

    Cessna T-50

    Information and specifications Role Twin engine trainer, five seat light transport Country of Origin United States of America Manufacturer Cessna Aircraft Company First Flight 26 March, 1939 Total production(units) Over 5400 Primary users Royal Canadian Air Force United States Navy United States Army Air Force Status Restored as antiques Variants AT-8, AT-17, JRC-1 Length 32…

  • Cessna 560

    Cessna 560

    Specification Variants UC-35D, Encore+ UC-35B, Citation Encore, UC-35C, UC-35A, Citation Ultra Crew 2 Passenger 11 maximum Engine 2 turbofan engine Pratt & Whitney Canada PW535A Power 15.1 kN Speed 793 kilometres per hour Service Ceiling 137.16 metres Range 3297 kilometres Weight 4627 kilograms (empty)/7543 kilograms (maximum at takeoff) Wingspan 16.49 metres Wing area 29.9 metres²…

  • Cessna 441 Conquest II

    Cessna 441 Conquest II

    Specifications Crew 2 pilots (maximum) Seats 7 Length 11.89 m Wing Area 23.5 m² Wingspan 15.04 m Height 4.1 m Weight 2,489 kg (empty)/4,611 kg (gross) Engine Garrett TPE331 turboprops; 474 KW/636 hp Propeller 4 bladed Power/Mass 0.21 KW/kg , 8.0 lb/hp Landing Gear Retractable tricycle Takeoff 544 m Climb-Rate 12.37 m/s Speed 480 km/hr…

  • Cessna 350

    Cessna 350

    Information and specification Role Four seat light touring aircraft Manufacturer Cessna Aircraft Company Country of Origin USA First Flight 1998 Top Speed 219 miles per hour Variants Columbia 300, 400 Status Out of production Length 25 ft 2 inches Height 9ft Wingspan 36ft 1 inches

  • Cessna 205

    Cessna 205

    Information and specifications Role Six seat utility light aircraft Country of Origin United States Manufacturer Cessna First Flight 1962 Total Production 577 Primary users United States Air Force Status Remodelled Variants P-206, 207A, Length 8.62 m Height 2.92 m Wingspan 10.92 m

  • Antonov-An-124 Ruslan

    Antonov-An-124 Ruslan

    Information and Specifications Role Large cargo transport aircraft Country of Origin Russia Manufacturer Aviant State Aviation Plant Total Production (units) 60 Primary users Russian Air Force United Kingdom Russian State Transport Company Status Out of operation Cruising speed 800 Km/hr Length 69.10 meter Height 21.80 meter First Flight December 1982

  • Antonov An-225 Mriya

    Antonov An-225 Mriya

    Specification Role Cargo airlifter National origin Soviet Union-Ukraine Manufacturer Antonov Introduced  1988 First Flight 21 December 1988 Primary User Antonov Status In service Primary User Antonov Airlines Designed 1980 (Antonov Design Bureau) Wingspan 88m Length 84m 

  • Antonov An-70

    Antonov An-70

    Specification Crew 4 (2 pilots, 1 navigator, 1 flight engineer) Capacity 300 troops/206 stretcher cases Weight 66.23 tonnes (empty)/145 tonnes (maximum at takeoff) Payload 47 tonnes (cargo) Length 40.7 metres Height 16.38 metres Wingspan 44.6 metres Engine 4 Progress D-27 with SV-27 counter-rotating turboprop fans  Power 13,880 hp/10,350 kW per unit Rate of Climb 24.9…

  • Antonov An-12

    Antonov An-12

    Specification Origin Ukraine Developer Antonov Design Bureau Crew 6 Passengers 130 Weight 30.5 tonnes (empty), 61 tonnes (maximum at take-off) Load 18 tonnes (maximum) Length 37 m Height 10.5 m Usable Volume 90 m³ Cargo Volume 13.5 x 2.95 x 2.47 m³ Wingspan 38 m Wing-area 121.7 m² Fuel Capacity 22,066 kl Engine 4 x…

  • Antonov An-2

    Antonov An-2

    Specification Designer Oleg Antonov Manufacturer Antonov Hongdu Aviation Industry Group First Flight 31 August 1947 Produced 1947-2002 Fleet 18000 and up Primary Users Soviet Union, China, North Korea Role Agriculture and utility biplane Variants Antonov An-3 Length 2m Wingspan 18.2 m(upper), 14.2m (lower) Top Speed 258 km/h

  • Lockheed C-5 Galaxy

    Lockheed C-5 Galaxy

    Specification Developer Lockheed Martin Founded 1947 Variants C-5A, C-5B, C-5C, C-5M Super Galaxy, C-5 RERP, Number Produced 131 Status Operational; production discontinued Engine 4 GE CF-80C2 turbofans Fuel-Capacity 150,819 kl Length 75.53 m Height 19.84 m Speed (normal) 817 km/hr Wingspan 67.91 m Stabiliser Span 20.95 m Operating Weight 181,437 kg Maximum Payload 129,274 kg…