3I Sky Arrow
| Sky Arrow | |
|---|---|
 | |
| Role | Recreational aircraft |
| Manufacturer | Magnaghi Aeronautica, 3I |
| First flight | 13 July 1992 |
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The Sky Arrow is a tandem-seat, pusher configuration, high-wing carbon fibre light aircraft that was manufactured by 3I (Iniziative Industriali Italiane). With only 16½ inches of hip room, the aircraft is considered open due to a large amount of unobstructed view from the large canopy, rear engine, and seating positions ahead of the wing.[1]
3I entered bankruptcy proceedings in 2008 and in 2012 the design was purchased by Magnaghi Aeronautica, of Naples, Italy.[2][3]
Design and development
Magnaghi Aeronautica, the new owners of the design in 2012, announced that it will be upgraded with larger wing tanks, improved aerodynamics and stability, stengthened structural elements and a new avionics package. The Sky Arrow will be available as a completed certified aircraft for light sport or as a kit. A four-seat version is also planned. Magnaghi Aeronautica also intendeds to market it for government utility roles, such as border patrol, pollution monitoring and aerial surveillance, with belly and nose mounted sensors.[3]
Variants
- Sky Arrow LSA
- Sky Arrow 650 TCN
- General aviation - out of production
- Sky Arrow 650 TC
- Sky Arrow 650 TCN
- Sky Arrow 650 TCNS
- General aviation - in production
- Sky Arrow 650TCS:
- (100 hp engine), VFR and Sky Arrow 650 TCNS for VFR Night - Maximum Takeoff Weight (MTOW) of 650 kg (1,433 lb)
- Sky Arrow 710RG:
- 100 hp engine, C for VFR and CN for VFR Night with an increased MTOW of 710 kg (1,565 lb) and retractable landing gear
- Sky Arrow 710 PLUS:
- 100 hp engine, C and CN with an increased MTOW of 710 kg (1,565 lb) and the fixed landing gear
- Sky Arrow 650 ERA:
- fitted with RAWAS instrumentation by the Atmospheric Turbulence Diffusion Division of the National Oceanic Atmospheric Administration and Iniziative Industriali Italiane, for use in territory control environmental monitoring and for scientific research purposes.[4]
- Light aircraft
- Sky Arrow 450TS (100 hp)
- Sky Arrow 480TS (100 hp)
- Sky Arrow 500TF (80 hp)
- Light sport - in production
- Sky Arrow Sport (100 hp)
- Meets ATSM requirements for the FAA Light-Sport category of aircraft.
- Assembly kit
- Sky Arrow 1450L (100 hp/115 hp)
- Homebuilt package consists of ten subkits. Meets the FAA 51 percent builder rule.[5]
Specifications (650)
Data from Giotto Air[6]
General characteristics
- Crew: two
- Length: 7.60 m (24 ft 11 in)
- Wingspan: 9.68 m (31 ft 9 in)
- Height: 2.56 m (8 ft 5 in)
- Wing area: 13.5 m2 (145 sq ft)
- Gross weight: 650 kg (1,433 lb)
- Useful load: 250kg (556 lbs)
- Powerplant: 1 × Rotax 912 F2 , 73.5 kW (98.6 hp)
Performance
- Maximum speed: 194 km/h (121 mph; 105 kn)
- Cruising speed: 187 km/h (116 mph; 101 kn)
- Service ceiling: 4,100 m (13,451 ft)
- Rate of climb: 4.3 m/s (850 ft/min)
References
- ↑ Ed Kolano (May 1996). "Flying Qualities Report Sky Arrow". Sport Aviation.
- ↑ Marsh, Alton K. "AOPA Online: Sky Arrow builder struggling to revive". Aopa.org. Retrieved 2012-04-01.
- 1 2 Grady, Mary (28 March 2012). "New Owners Aim To Enhance Sky Arrow Airplane". AVweb. Retrieved 1 April 2012.
- ↑ National Oceanic Atmospheric Administration (1 October 2008). "The Sky Arrow 650 ERA". Archived from the original on 31 January 2009. Retrieved 31 March 2012.
- ↑ "Sky Arrow". Aircraft Spruce. Retrieved 2012-04-01.
- ↑ Giotto Air (undated), Sky Arrow 650 Series, retrieved 1 April 2012
- World Aircraft Information Files. London: Bright Star Publishing.
External links
 |
Wikimedia Commons has media related to 3I Sky Arrow. |
- Sky Arrow 650 ERA at the National Oceanic and Atmospheric Administration website.
- European Aviation Safety Agency Type Certificate Data Sheet