Here are the parameters for your reference. The highest speed (Km/h) : 405 Distance (km) : 1850 Maximum take-off weight (kg) : 1542 Cruising speed (km/h) : 322 Take shortest distance (m) : 295 Length (cm) : 792 Wingspan (cm) : 1168 Height (cm) : 270 Engine type: IO - 550 - N Engine type: piston engine
Cessna 172 r, the united states cessna's classic, accumulative total production was more than 35000 aircraft, safe, comfortable, operating performance is incomparable. The io - 360 engine, horsepower strong and smooth, quiet, under the 2400 r/min can be up to 160 horsepower. The main technical indicators: Dimensions: length: 8204 mm high: 8204 mm wingspan: 11000 mm 2500 meters altitude cruising speed: 226 km/h Sea level on the maximum speed: 228 km/h propeller diameter: 1905 mm Radius of 2500 meters, 1070 km, 4.8 hours radius of 3000 meters, 1270 km, 6.6 hours Climb speed: 220 m/min ceiling: 4110 meters maximum take-off weight: 1110 kg aircraft weight: 744 kg Weight: 371 kg allows the luggage: 54 kilograms fuel tank: 212 liters Rmb 2.39 million Length (cm) : 792 Wingspan (cm) : 1168 Height (cm) : 270 Engine type: io - 550 - n Engine type: piston engine
Description 1.Controled by high precision brushless dc motor 2.No need remove camera when charging sd card. 3.Lightweight 4.Independent imu feedback 5.Full metal making 6.Supported camera:gopro series;xiaoyi;sj4000 and same size camera 7.Supported phone:iphone series , 7 inches below the smart phone Features: 1.Dimensions:323*151*79mm 2.Weight:353g 3.Battery:18650, 18350 4.Endurance time:8h 5.Stationary attitude control accuracy:±0.05° 6.Motion attitude control accuracy:±0.5° 7.Pan axis movement angle:320° 8.Pitch axis movement angle:320° 9.1.3-axis high performance gimbal.
Provide flight control system (support UAV, even hypersonic missile). If you need it, you can contact me. You cannot sell it directly to war-torn areas, for fear of being sanctioned by the United States. can only be transported Flight control system ($1,000-100,000) Only accept wire transfer 100% payment
Item Specifics Type: Boeing 777 Material: Resin Product Composition: Airplane Model + Metal Bracket + Imitation Mahogany Base Detail: Engine Blade Hollow Design Length: 47cm (1:135) Weight: 1.45kg Package Quantity: 6PCS/CTN Package Size: 90.5cm*47cm*44.5cm Packaging: Color Printing Box + Foam Value: Souvenir/Gift/Collection/Display/Decoration OEM/ODM: Support
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
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
Item Specifics Type: Airbus 330 Material: Resin Product Composition: Airplane Model + Metal Bracket + Imitation Mahogany Base Detail: Engine Blade Hollow Design Length: 32cm (1:200) Weight: 0.50kg Package Quantity: 6PCS/CTN Package Size: 60cm*35cm*37.5cm 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 item sizes, quantity and your OEM/ODM plan (airplane model / the stand / packaging box), our professional customer service will make a quotation for you. STEP2: Design If you don't have sample drawings, please contact customer service to inform your request, we have professional designers to help you design. STEP3: Confirm the effect drawing Once the effect drawing is confirmed, we will arrange production. If you want to change, you need to pay for the proofing again. Please confirm carefully. STEP4: Arrange production Why you choose us? 1.Focus on airplane model. Abundant manufacturing experience. 2.We have independent production lines. Provide ONE-STOP production sevice from design, manufacturing to sales. 3.High degree of model simulation. Our airplane models are depended on the size of the original airplane. 4.All airplane types and sizes can be tailored to the client's business and needs. We are in accordance with customerâ??s design concept to strive for each customer satisfied. 5.High flexibility of production process. With a large number of production and micro-production process and management capabilities. Meet the different requirements of customers, provide the most affordable processing price. 6.Professional after-sevice. Our friendly customer service are always standing by for you.
Airbus Standard:ABD 0031 Fire Test to Aircraft Material (Copper clad laminate) 1.ABD 0031 Airbus Fire Test to Demonstrated that Acceptable control of the risk of ignition has been achieved Acceptable control of the rate of and total emission of heat, smoke and toxic fume has been achieved for all major usage materials and surfaces when exposed to a source of ignition. Acceptable resistance to fire has been achieved for all materials and items required to perform as a barrier to fire or which are required to perform some function when exposed to fire. 2.ABD 0031 Fire Test to Aircraft Material-Product Scope Rubber Product, Rubber Seal Plastic Product Fire Coating Fire Adhesive Cable and Wire Textile (Curtain, carpet) 3.Airbus Standard: ABD 0031 - Fire test to Aircraft Material Vertical Flammability Test: ABD 0031- 7.1.2 (AITM 2.0002 B/A) Smoke Density Test: ABD 0031- 7.3.1 (AITM 2.0007) Smoke Toxicity Test: ABD 0031- 7.4 (AITM 3.0005) Heat Release Test: ABD 0031 (AITM 2.0006) Horizontal Test: ABD 0031- 7.1.3 / -7.1.4 (AITM 2.0003) 45�° flammability test: ABD 0031- 7.1.5 4.Far 25.853 Fire test to aircraft material- Test method Vertical flammability test: 14 FAR 25.853 b(4)), Smoke Density Test: 14 FAR 25.853 (d), (App. F to part 25, part V) Heat Release Test: 14 FAR 25.853 (d), Appendix F, Part IV Seat Test: 14 FAR 25.853 (c, App.F to part II) Horizontal Test: 14 FAR 25.853 b(2,3), (App. F to part 25 part I (a),(1) 45 flammability test: 14 FAR 25.853 (b), (App. F to part 25, part I (6))
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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 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
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)
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