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WHITNEY BOOMERANG Civil Aircraft Model Details

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General Information of WHITNEY BOOMERANG
Designer : C.W. Bill Whitney

First Flight : 6 July 2006

Introduction : 2007

Manufacturer : Dean-Wilson Aviation Ltd

National Origin : Australia

Produced : 2007–2011

Role : Training aircraft

Unit_Cost : A$210,000

General characteristics of WHITNEY BOOMERANG
Capacity : 2

Crew : 1

Empty Weight : 600 kg (1323 lbs)

Height : ()

Length : 6.46 m (21 ft 2 in)

Max Takeoff Weight : 825 kg (1819 lbs)

Powerplant : 1 × Textron Lycoming O-235 air-cooled, horizontally opposed, four cylinder reciprocating engine, 88 kW (118 hp)

Propellers : McCauley fixed-pitch two-bladed aluminium propeller, 1 per engine

Useful Load : 225 kg (496 lbs)

Wing Area : 13.72 m2 (147.68 sq ft)

Wingspan : 9.80 m (32 ft 2 in)

Performance of WHITNEY BOOMERANG
Cruise Speed : 176 km/h (95 KIAS)

Never Exceed Speed : 282 km/h (152 KIAS)

Stall Speed : 85 km/h (46 KIAS)

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