Jabiru Aircraft
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| Jabiru Aircraft Company Pty Ltd | |
 |
|
| Type | PTY Ltd. |
|---|---|
| Founded | 1988 |
| Headquarters | Bundaberg, Australia |
| Key people | Rodney Stiff Phil Ainsworth |
| Industry | Light aircraft Manufacturers |
| Website | http://www.jabiru.net.au |
This article is about the plane. For the stork see Jabiru.
The Jabiru Aircraft Company Pty Ltd produces a range of small civil utility aircraft designed and manufactured in Bundaberg, Australia. They also design and manufacture a range of engines, specifically designed for light aircraft use. The aircraft are available as kit and ready-built versions. Types include Microlight (Ultralight or ULM), commonly called the Calypso and light aircraft of up to four (but typically two) seats.
The aircraft are built largely of composite materials and are conventional high-wing monoplanes with typically tricycle undercarriage, although taildragger versions are available as well. The wings can be removed for ease of storage or transportation.
Use of modern composite techniques has resulted in a strong, light structure. The aircraft are designed around the pilot and passengers, being spacious and comfortable for touring, yet with a small footprint and frontal profile. Controls include a centrally mounted control column, brake and trim lever.
[edit] Brief History
The company was formed in 1988 by Rodney Stiff and Phil Ainsworth to manufacture affordable light aircraft in Kit and certified forms. In October 1991, the first aircraft (Jabiru LSA 55/2k, was certified by the Australian Civil Aviation Authority
Due to the original engine manufacturer ceasing production of aero engines, the company started development of their own engines, and by 1995 the Jabiru 2200 was available for delivery. Since then the Jabiru 3300 and Jabiru 5100 engines have been added to the range. In the same year, 1995, it was decided to offer these aircraft as amateur build or Experimental self build Kits.
[edit] Aircraft
[edit] Factory-built
- LSA - configured to meet ultralight regulations
- ST3 - configured to meet general aviation regulations
- UL-D - configured to meet UK Microlight regulations
- J160C - Certified with 2200 Engine
- J230C - Certified with 3300 Engine
[edit] Kitplanes
- J200 - 2-seat aircraft
- J400 - 4-seat aircraft
- SP - Light aircraft version
- SP-T - Taildragger version of SP
- UL - export version to meet European microlight regulations (Calypso)
- UL-T - taildragger version of UL
[edit] Specifications (Jabiru J200)
General characteristics
- Crew: 1
- Capacity: 1 passenger
- Length: 6.55 m (21 ft 6 in)
- Wingspan: 8.10 m (26 ft 7 in)
- Height: 2.20 m (7 ft 3 in)
- Wing area: 8 m² (86 ft²)
- Empty weight: 310 kg (682 lb)
- Max takeoff weight: 700 kg (1,540 lb)
- Powerplant: 1× Jabiru 3300 , 90 kW (120 hp)
Performance
- Maximum speed: 220 km/h (137 mph)
- Range: 893 km (555 mi)
- Service ceiling: 4,600 m (15,000 ft)
- Rate of climb: 460 m/min (1,500 ft/min)
[edit] Specifications (Calypso)
Calypso Microlight (ULM) aircraft
- Crew: 1
- Capacity: 1 passenger
- Length: 5.64 m (18 ft 6 in)
- Wingspan: 9.4 m (30 ft 10 in)
- Height: 2.01 m (6 ft 7in)
- Wing area: 9.31 m² (100 ft²)
- Empty: 260 kg (572 lb)
- Maximum takeoff: 450 kg (990 lb)
- Powerplant: 1x Jabiru 2200, 85 hp
[edit] Performance
- Maximum speed: 211 km/h (130 mph)
- Range: 745 km (460 miles)
- Service ceiling: 15,000 ft (4,600 m)
- Rate of climb: 460 m/min (1,500 ft/min)
[edit] Engines
Jabiru produce their own range of lightweight 4-stroke horizontally opposed aircooled engines, specifically designed and engineered for use in aircraft. All engines are direct drive and are fitted with alternators, silencers, vacuum pump drives and dual ignition systems as standard. Over 2000 4-cylinder engines and over 750 of the 6-cylinder engines have been produced. The basic design is now so mature that only minor design changes have been made in the last 1000 engines or so.
[edit] Available Engines
- Jabiru 2200; 4-cylinder at 85 bhp (64 kW)
- Jabiru 3300; 6-cylinder at 120 bhp (89 kW)
- Jabiru 5100; 8-cylinder at 180 bhp (134 kW)
[edit] External links
[edit] Related content
Related development:
Comparable aircraft: 3Xtrim 3X55 Trener
Designation sequence:
