Alpha 2000
 |
It has been suggested that Robin 2160 be merged into this article or section. (Discuss) Proposed since July 2011. |
| Alpha 2000 | |
|---|---|
 |
|
| ZK-CTR of CTC Aviation Training | |
| Role | Multipurpose civil aircraft |
| Manufacturer | Alpha Aviation |
| First flight | 15 January 1976 |
The Alpha Aviation Alpha 2000 is a two-seat, all-metal training and general aviation aircraft built in Hamilton, New Zealand. It is a development of French Apex Aircraft's Robin R2000 series acquired upon Apex's purchase of the Avions Robin company.
Contents |
[edit] History 1971–1994
The original Avions Robin HR200 was designed by Christophe Heintz,[1] to supplement the earlier Avions Robin designs of Jean Délémontez who also designed the popular post war wooden Jodel. The HR 200 prototype first flew on 19 July 1971, and entered production in 1973. The R2000 Alpha name was applied to a new aircraft which shared the fuselage of the HR 200, but had all new wing and tail surfaces. The prototype R2000 Alpha flew on 15 January 1976 and production followed in 1977 to 1983.
Licensed production was also undertaken in Canada.[2]
[edit] History 1994–2004
The R2160 model was returned to production with minor modifications in 1994 by Apex Aircraft.[3]
[edit] New Zealand Production 2004 – 2008
In 2004 Alpha Aviation of New Zealand bought engineering jigs and equipment and world wide production rights[4] to both the Robin HR200 and Robin R2000 series. Alpha Aviation has recommenced production of the Robin R2120 as the Alpha 2000 120T and of the Robin R2160 as the Alpha 2000 160A and 160Ai. Apex continues to market the aircraft in Europe.
Production of the New Zealand development began in 2006 against orders for nine aircraft and 18 options (including orders from the UK, South Africa and Australia), with capacity to build four aircraft a month. An Alpha 160A, ZK-FXY, was first off the production line, being test flown by Noel Kruse and Steve Lange on 12 April 2006. It will be subsequently used as a company demonstrator. It made its first public appearance at the 2006 Warbirds over Wanaka airshow. The next three aircraft off the production line were ordered by the Waikato Aero Club as training aircraft. The official handover ceremony for these three aircraft took place on 15 April 2007.
A further 12 aircraft have been ordered by CTC Aviation Training Ltd. (New Zealand) for use as a primary trainer in their 'CTC Wings' pilot training scheme.
The 4th and 5th Alpha 160A's to roll off the production line were bought by Southern Wings, and since early 2007 have been operated for both primary training and aerobatic instruction.
In January 2008 production was halted due to the liquidation of Alpha Aviation by parent company Inventis.
[edit] Variants
[edit] Robin/Apex
- R 2100A
- Powered by 81 kW (108 hp) Lycoming O-235 engine.[5] 34 built[6]
- R 2112 Alpha
- Replacement for R 2100 with 83.5 kW (112 hp) Lycoming O-235 engine.[6]
- R 2160 Alpha Sport
- 119 kW (160 hp) Lycoming O-320 engine.[6] Originally named Acrobin.[5]
[edit] Alpha Aviation
As of 2006 three variants are offered. The approximate horsepower of each is indicated by the type number.
- Alpha 120T, the smallest and cheapest, envisaged as a trainer.
- Alpha 160A, a more powerful fully aerobatic trainer.
- Alpha 160Ai, a fuel injected engine and equipped for cross country touring as well as aerobatics.
[edit] Specifications (R2160 Alpha Sport)
Data from Jane's All The World's Aircraft 1982–83[7]
General characteristics
- Crew: 2
- Length: 7.10 m (23 ft 3½ in)
- Wingspan: 8.33 m (27 ft 4 in)
- Height: 2.135 m (7 ft 0 in)
- Wing area: 13.00 m² (140 sq ft)
- Airfoil: NACA 23015
- Aspect ratio: 5.34
- Empty weight: 575 kg (1,268 lb)
- Max. takeoff weight: 1,000 kg (2,205 lb)
- Powerplant: 1 × Avco Lycoming O-320-D2A air-cooled flat-four piston engine, 119 kW (160 hp)
Performance
- Never exceed speed: 333 km/h (180 knots, 207 mph)
- Maximum speed: 257 km/h (138 knots, 160 mph) at sea level
- Cruise speed: 234 km/h (126 knots, 145 mph) at 3,350 m (11,000 ft)(65% power)
- Stall speed: 85 km/h (46 knots, 53 mph) (flaps down)
- Range: 796 km (430 nmi, 495 mi) (max fuel, 65% power)
- Service ceiling: 3,800 m (12,500 ft)
- Rate of climb: 5.2 m/s (1,025 ft/min)
[edit] See also
- Aircraft of comparable role, configuration and era
- Related lists
[edit] References
- ^ Designer CHRIS HEINTZ
- ^ HR200JT
- ^ Robin HR200, R 2000 Alpha aircraft performance and specifications
- ^ Apex Aircraft and Alpha Aviation – A strategic alliance
- ^ a b Donald 1997, p.777.
- ^ a b c Taylor 1982, p.77.
- ^ Taylor 1982, pp. 77–78.
- Donald, David (ed.).The Encyclopedia of World Aircraft Leicester:Blitz, 1997. ISBN 1-856605-375-X.
- Taylor, John W R (ed). Jane's All The World's Aircraft 1982–83. London:Jane's Yearbooks, 1982. ISBN 0-7106-0748-2.
[edit] External links
|
|||||
|
||||||||||||||
