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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))
We provide Aircraft Parts, Jig/Fixture. My company is the international sales agent of the manufacturer. The seller in sales and purchase contracts will be the manufacturer, and my company will take commissions as the agent. ** Product Outline Various kinds of aircraft parts, jigs and fixtures. The manufacturer has excellent technique for various types of jigs and fixtures, with Aerospace Standard. Ever since the foundation in 1990, the manufacturer has been renowned with great quality of their products, satisfactory service, and exact delivery for domestic and worldwide customers. Please contact us for further details. ** Country of Origin Republic of Korea(South Korea) ** Port of Loading Busan port or any other port of Korea > Negotiable > Negotiable > Negotiable
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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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Jet aircraft.
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Aircraft, airplane.Transportation
