Auster Adventurer

Auster J/5 Adventurer
J/5 Adventurer at Ardmore airfield, Auckland, New Zealand in February 1992
Role	private owner aircraft
National origin	United Kingdom
Manufacturer	Auster Aircraft Ltd
First flight	15 November 1947
Introduction	1948
Status	several still in operation
Primary user	private owner pilots and agricultural contractors
Number built	59
Developed from	J/1 Autocrat

The Auster J/5 Adventurer is a British-built three-seat light high-wing monoplane of the late 1940s.

Development

The Adventurer three-seat high-wing monoplane was developed from the J/1 Autocrat with extra power provided by the installation of the 130 h.p. Gipsy Major engine, to enable more flexible operations in the hotter climate of Australia and New Zealand, where most examples were sold. Unlike the similarly powered J/1 Aiglet and J/1N Alpha, the Adventurer retained the smaller tail surfaces of the Autocrat, the new engine being set back sufficiently far for the original fin area to remain sufficient.

The prototype Adventurer was converted to the new standard from a J/1 Autocrat c/n 2093 and first flew on 15 November 1947. This was followed by a further 58 production examples delivered between 1948 and 1952.

Operational history

Most J/5s were sold to private pilot owners in Australia and New Zealand where they were given the name Adventurer. Eleven Adventurers were still in service in Australia in 2009 and one in New Zealand (see image). Six Adventurers were sold to the Royal New Zealand Air Force (RNZAF) and four to the Royal Rhodesian Air Force (RRAF). Five examples were completed for agricultural use as the J/5A Cropduster and served in Africa and Pakistan.

Variants

J/5

civil version, also operated by the RNZAF and RRAF (54 aircraft)

J/5A

agricultural version with spray bars, spray tank etc. (5 aircraft)

Operators

New Zealand

• Royal New Zealand Air Force operated six J/5 Aiglets.

Southern Rhodesia

• Southern Rhodesian Air Force operated four.

Specifications (J/5)

Data from Green, 1965, p. 138

General characteristics

• Crew: one
• Capacity: two passengers
• Length: 23 ft 6 in (7.16 m)
• Wingspan: 36 ft 0 in (10.97 m)
• Height: 6 ft 6 in (1.98 m)
• Wing area: 185 sq ft (17.19 m²)
• Empty weight: 1,205 lb (547 kg)
• Gross weight: 2,000 lb (907 kg)
• Powerplant: 1 × de Havilland Gipsy Major I , 130 hp (97 kW)

Performance

• Maximum speed: 125 mph (201 km/h, 109 kn)
• Cruise speed: 106 mph (171 km/h, 92 kn)
• Range: 200 mi (322 km, 170 nmi)
• Rate of climb: 750 ft/min (3.81 m/s)

References

Notes

Bibliography

• Ellison, N.H. (1965). Auster Aircraft Ltd - Aircraft Production list. Air Britain (Historians).
• Green, William (1965). The Aircraft of the World. Macdonald & Co (Publishers). ASIN B001AH4Y0E.
• Hitchman, A.V. (1989). The History of the Auster Aeroplane. International Auster Pilot Club. ASIN B0019BV2YM.
• Jerram, Mike (January 1988). "For Business and Pleasure: Part Six". Aeroplane Monthly. Vol. 16, no. 1. pp. 54–57. ISSN 0143-7240.