Jabiru J170
| J170 | |
|---|---|
 | |
| Role | Ultralight aircraft and Light-sport aircraft |
| National origin | Australia |
| Manufacturer | Jabiru Aircraft |
| Status | In production (2012) |
| Number built | 400 (2011) |
| Unit cost |
US$38,400 (kit only, 2011) |
| Developed from | Jabiru J160 |
The Jabiru J170 is an Australian ultralight and light-sport aircraft, designed and produced by Jabiru Aircraft. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1][2]
Design and development
The J170 was derived from the Jabiru J160, by using the J160 fuselage and the wings from the Jabiru J430 plus a bigger elevator to give it a better rate of climb at higher density altitudes. It was designed to comply with the US light-sport aircraft rules at a gross weight of 600 kg (1,323 lb). The J170 features a strut-braced high-wing with winglets, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.[1][3][4]
The aircraft is made from composites. Its 9.66 m (31.7 ft) span wet wing has an area of 9.56 m2 (102.9 sq ft), a fuel capacity of 135 litres (30 imp gal; 36 US gal) and flaps. The standard engine available is the 85 hp (63 kW) Jabiru 2200 four-stroke powerplant.[1][4][5]
The J170 complies with both the US light-sport rules and United Kingdom BCAR Section "S" requirements.[1] In Canada it qualifies as an Advanced Ultralight at a gross weight of 560 kg (1,235 lb)[6]
Specifications (J170)
Data from Bayerl and Jabiru Aircraft[1][5]
General characteristics
- Crew: one
- Capacity: one passenger
- Length: 5.775 m (18 ft 11 in)
- Wingspan: 9.66 m (31 ft 8 in)
- Height: 2.300 m (7 ft 7 in)
- Wing area: 9.56 m2 (102.9 sq ft)
- Aspect ratio: 9.8:1
- Empty weight: 320 kg (705 lb)
- Gross weight: 600 kg (1,323 lb)
- Fuel capacity: 135 litres (30 imp gal; 36 US gal)
- Powerplant: 1 × Jabiru 2200 four cylinder, air-cooled, four stroke aircraft engine, 63 kW (85 hp)
- Propellers: 2-bladed wood/composite, 1.52 m (5 ft 0 in) diameter
Performance
- Maximum speed: 240 km/h (149 mph; 130 kn)
- Cruising speed: 185 km/h (115 mph; 100 kn)
- Stall speed: 72 km/h (45 mph; 39 kn) full flaps
- Never exceed speed: 259 km/h; 161 mph (140 kn)
- Range: 1,908 km; 1,185 mi (1,030 nmi)
- Service ceiling: 4,572 m (15,000 ft)
- g limits: +4/-2
- Maximum glide ratio: 10:1
- Rate of climb: 2.5 m/s (500 ft/min)
- Wing loading: 62.8 kg/m2 (12.9 lb/sq ft)
References
- ↑ 1.0 1.1 1.2 1.3 1.4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 61. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ Vandermeullen, Richard: 2012 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 56. Belvoir Publications. ISSN 0891-1851
- ↑ Experimental Aircraft Association (2012). "EAA's Listing of Special Light-Sport Aircraft". Retrieved 1 June 2012.
- ↑ 4.0 4.1 Jabiru Aircraft (2005). "Jabiru J170". Retrieved 23 July 2012.
- ↑ 5.0 5.1 Jabiru Aircraft (n.d.). "J170 Specifications". Retrieved 23 July 2012.
- ↑ Transport Canada (27 March 2012). "Listing of Models Eligible to be Registered as Advanced Ultra-Light Aeroplanes (AULA)". Retrieved 15 July 2012.
External links
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Wikimedia Commons has media related to Jabiru Aircraft. |
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