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The cirrus sr22 is a single-engine four- or five-seat composite aircraft built from 2001 by cirrus aircraft of duluth, minnesota. It is a development of the cirrus sr20, with a larger wing, higher fuel capacity, and a more powerful, 310-horsepower (231 kw) engine. The sr22 has been the world's best-selling general aviation (ga) airplane every year since 2002. It is the most-produced ga aircraft made from composite material, accounting for over 30% of the entire piston aircraft market General characteristics Crew: one Capacity: four passengers Length: 26 ft 0 in (7.92 m) Wingspan: 38 ft 4 in (11.68 m) Height: 8 ft 11 in (2.72 m) Airfoil: roncz Empty weight: 2, 225 lb (1, 009 kg) Gross weight: 3, 600 lb (1, 633 kg) Fuel capacity: 92 us gallons (348 litres) Powerplant: 1 continental io-550-n six cylinder horizontally opposed aircraft engine, 310 hp (230 kw) Propellers: 3-bladed Performance Cruise speed: 183 kn (211 mph; 339 km/h) Stall speed: 60 kn (69 mph; 111 km/h) flaps down Range: 1, 049 nmi (1, 207 mi; 1, 943 km) with reserves at 65% power Service ceiling: 17, 500 ft (5, 300 m) Rate of climb: 1, 270 ft/min (6.5 m/s)
The cessna citation mustang, model 510, is a very light jet (vlj) class business jet built by cessna aircraft company at their independence, kansas production facility. The mustang, in standard configuration, has four passenger seats in the aft cabin, a toilet, and seating for two in the cockpit. Like most other light jets, the mustang is approved for single-pilot operation. General characteristics Crew: one or two pilots Capacity: 4 to 5 passengers Length: 40 feet 7 inches (12.37 m) Wingspan: 43 feet 2 inches (13.16 m) Height: 13 feet 5 inches (4.09 m) Empty weight: 5600 lb (2540 kg) Useful load: 3130 lb (1420 kg) Max. Takeoff weight: 8645 lb (3930 kg) Powerplant: 2 pratt & whitney canada pw615f turbofans, 1460 lb thrust (6.49 kn) each Performance Maximum speed: mach 0.63 (483 mph, 777 km/h) Cruise speed: 340 ktas (390 mph, 630 km/h) Range: 1167 nmi (at max. Takeoff weight) (1, 343 mi, 2, 161 km) Service ceiling: 41000 ft (12500 m) Rate of climb: 3010 fpm (917 mpm) Thrust/weight: 0.337 (at max. Takeoff weight) Takeoff distance: 3, 110 ft (948 m) Landing distance: 2, 380 ft (729 m)
We have the following aircrafts for sale 2 x A330-200F, Factory Freighters, YOM 2009 - 2 x B747-800F, Factory Freighter, YOM 2013 - 1 x B737-300F, Converted Freighter, YOM 1993 - 1 x B737-300F, Converted Freighter, YOM 1993 - 1 x B737-800SF, Converted Freighter, YOM 2003 - 1 x A320, Factory Passengers, YOM 2001 - 1 x A320, Factory Passengers, YOM 1999 - 1 x B737-300, Factory Passengers, YOM 1997 1 x B737-400, Factory Passengers, YOM 1996 -
Boeing, airbus, fokker, falcon, md, dc transport and cargo aircraft in turboprop and turbofan. Large , medium , small
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The robinson r22 is a two-bladed, single-engine light utility helicopter manufactured by robinson helicopter company. The two-seat r22 was designed in 1973 by frank robinson and has been in production since 1979. General characteristics Crew: 1 Capacity: 2, including pilot Length: 28 ft 8 in (8.74 m) Rotor diameter: 25 ft 2.4 in (7.67 m) Tail rotor diameter: 3 ft 6 in (1.07 m) Height: 8 ft 11 in (2.72 m) Disc area: 497 (46.2 m) Empty weight: 880 lb (399 kg[23]) Loaded weight: 920 lb (417 kg) Max. Takeoff weight: 1, 370 lb (635 kg) Main tank total capacity: 19.8 us gallons (75 liters) Main tank usable capacity: 19.2 us gallons (73 liters) Optional aux tank total capacity: 10.9 us gallons (41 liters) Optional aux tank usable capacity: 10.5 us gallons (40 liters) Powerplant: 1 ã? lycoming o-320-a2b or -a2c flat 4 piston engine, 124 hp (93 kw) Performance Never exceed speed: 117 mph, 188 km/h, 102 kts Cruise speed: 110 mph, 177 km/h, 96 kts Range: 240 mi (386 km) Service ceiling: 14, 000 ft (4, 267 m) Rate of climb: 1, 200 ft/min (6.1 m/s) Disc loading: 2.61 lb/ (13.7 kg/m) Fuel consumption: 8~10 us gal/hr Power/mass: 0.095 hp/lb (0.147 kw/kg) Endurance: approx. 3 hours, with 30-minute reserve
A new ANG 01 aircraft has been designed and manufactured in 2019. ANG 01 is based on the concept of LA-50 aircraft, At the same time, ANG 01 is substantially more perfect than its predecessor. Thus, due the use of new carbon fiber materials, its weight was reduced and its strength characteristics were enhanced. Owing to the usage of specialized computer programs, the company specialists have managed to implement an optimum structure of the fuselage and wing, having achieved hereby their best performance. We have also used the advanced products for computer-based wind-tunnel simulation that allows modeling the characteristics of the airframe and fine-tuning them at the development phase. The development of the aircraft was performed, based on the latest technological achievements, with the use of the up-to-date CAD systems for aircraft design computing, which allowed to carry out the design strength aerodynamics testing, etc. with high precision directly in the computer. Due to the calculations solely in CAD systems, we have obtained the aircraft empty weight of 380-400 kg (maximum configuration), while the maximum take-off weight is of 950 kg. Thus, the payload is 550-570 kg, that is 137%-150% of its own weight. Besides, to enhance the safety of the aircraft, it was equipped with a modern parachute rescue system GRS 6 800-990 SDS manufactured by the Czech company Galaxy GRS s.r.o. Reliability and ease of control is provided by modern electronic SkyView HDX system manufactured by Dynon Avionics. Specifications Number of Seats 5 Engine Rotax 915 iS3A 141 HP fuel Type Avgas A-92, A-95, A-98, 100LL Propeller 3 blade, Variable Pitch Type Landing Gear trycicle type, hydraulically retractable Maximum Takeoff Weight 950 kg empty weight 380 kg The capacityof fuel tanks 245 l wing area 11,3 m2 Wingspan 9,6 m Aircraft Length 7,138 m Height 2,65 m fuselage width MAX 1,35 m cabin height 1,2 m Cabin length MAX 2.3 m Wing loading 84 kg/m2 Landing Gear Tread 1.9 m wheel size 8â?? (420 mm) Luggage Compartment Capacity 780 liters Maximum Lift-to-Drag Ratio 18.6 Max speed 360 km/h Maximum cruising speed 345 km/h Cruising speed 85% 310 km/h landing speed 70 km/h Cruising speed 65% 290 km/h rate of climb 3,5 m/s Takeoff Run 300 m Landing Roll 150 m at an altitude of 4000m Climb rate 8.3m / sec
From the world's most advanced and fuel-efficient single-aisle aircraft family. Choice of two new-generation engines (the PurePower PW1100G-JM from Pratt and Whitney and the LEAP-1A from CFM International) and features large, fuel-saving wingtip devices known as Sharklets. Overall Length: 37.57m. Wing span: 35.80m. Height: 11.76m. Range: 6,300km. Max take-off weight: 79 tonnes. Max fuel capacity: 26,730 litres. Maximum passengers: 194. Offer available: Buy 10 aircrafts for $810 million USD.
Item Specifics Type: Airbus 380 Material: Resin Product Composition: Airplane Model + Metal Bracket + Imitation Mahogany Base Detail: Engine Blade Hollow Design Length: 45cm (1:160) Weight: 1.50kg Package Quantity: 6PCS/CTN Package Size: 90.5cm*47cm*44.5cm Packaging: Color Painting Box + Foam Value: Souvenir/Gift/Collection/Display/Decoration OEM/ODM: Support Customize Process STEP 1: Inquiry Contact our Customer Service Team: Please provide dimensions, quantity and custom patterns of the airplane model, our professional customer service will help you evaluate. STEP 2: Design If you don't have sample drawings, please contact customer service to inform your request, we have professional designers to help you design. STEP 3: Confirm the effect drawing Once the effect drawing is confirmed, we will arrange production. If you want to charge, you need to pay for the proofing again. Please confirm carefully. STEP 4: Arrange production
