Aircraft Data Sheet: Widgeon l & ll (1924)

First flight:	24th September 1924
Span:	9.35m/30ft 8ins
Length:	6.4m/21ft 0ins
Max weight:	522kg/1150lb
Max level speed:	95.5knots/177kph
Power plant:	One 35shp/26kW Blackburn Thrush (Widgeon l) One Armstrong Siddeley Genet. (Widgeon ll)
Total built:	2 prototypes

The Widgeon was the second Westland entry in the 1924 competition, built to provide a monoplane response. The trials aircraft was unfortunately damaged in the course of the competition and as a consequence did not proceed in this form.