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Waco N series
Waco AVN-8 in 1938
Role	Four-seat tricycle undercarriage cabin biplaneType of aircraft
National origin	United States
Manufacturer	Waco Aircraft Company
First flight	1937
Status	a few still airworthy in 2009
Primary user	private owner pilots
Number built	approx 20
Developed from	Waco C series

The Waco N series is a range of 1930s American-built cabin biplanes with a fixed tricycle undercarriage produced by the Waco Aircraft Company.

Design and development

Waco introduced the luxury N-series biplane in 1937. It was based on the Waco C-series five-seat custom-cabin Waco with that model's curved pointed wings, but with an unusual fixed tricycle undercarriage and a modified tail with a lower rudder extension to give increased side area. The Waco N was fitted with flaps on all four wings to improve the aircraft's landing characteristics.

Operational history

The prototype, was designated ZVN-7, with the '7' indicating its year of manufacture (1937), and was powered by the 285 hp (213 kW) Jacobs L-5 engine. Only around 20 examples of the N series were completed, as the AVN-8, and ZVN-8. A few were impressed by the USAAC during the Second World War as the UC-72J and UC-72L. One AVN-8 was used by the Royal Aircraft Establishment at Farnborough, Hampshire, for trials with tricycle landing gear.

An example of the AVN-8 is maintained in airworthy condition by the Historic Aircraft Restoration Museum at Creve Coeur Airport near St Louis Missouri.

Variants

ZVN-7 and ZVN-8

285 hp (213 kW) Jacobs L-5

AVN-8

330 hp (246 kW) Jacobs L-6 engine

Specifications (AVN-8)

Data from Green, 1965, p. 306

General characteristics

• Crew: 1
• Capacity: 3 passengers
• Length: 27 ft 7 in (8.41 m)
• Wingspan: 34 ft 9 in (10.59 m)
• Height: 8 ft 6 in (2.59 m)
• Wing area: 246 sq ft (22.9 m)
• Empty weight: 2,493 lb (1,131 kg)
• Gross weight: 3,800 lb (1,724 kg)
• Powerplant: 1 × Jacobs L-6 seven-cylinder radial air-cooled , 330 hp (250 kW)

Performance

• Maximum speed: 161 mph (259 km/h, 140 kn)
• Cruise speed: 151 mph (243 km/h, 131 kn)
• Service ceiling: 14,200 ft (4,300 m)
• Rate of climb: 900 ft/min (4.6 m/s)

References

Notes

1. Simpson, 2001, p. 575
2. Green, 1965, p. 306

Bibliography

• Green, William (1965). The Aircraft of the World. Macdonald & Co. (Publishers) Ltd.
• Simpson, Rod (2001). Airlife's World Aircraft. Airlife Publishing Ltd. ISBN 1-84037-115-3.

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