Westland Widgeon (helicopter) Rotorcraft

Compare…

All rotorcrafts

Manufacturer
Westland Aircraft
Description
The Westland Widgeon is a helicopter that was developed by Westland Aircraft as a private venture improvement on the Westland WS-51 Dragonfly.
First Flight
1955-08-23
Designer
Westland Aircraft
Type
Helicopter
Length (m)
12.192
Height (m)
3.9624
Cockpit Crew
1
Max Seating
4
Max Speed (km/h)
167.3718
Cruise Speed (km/h)
130.3569
Max Ceiling (m)
3200.4
Rate of Climb (m/s)
3.556
Capacity Description
4 pax
National Origin
United Kingdom
Number Built
12
Powerplant Description
1 × Alvis Leonides 521/1 9-cylinder air-cooled radial piston engine (6lb boost), 388 kW (520 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Westland_Widgeon_%28helicopter%29
Number of Engines
1
Number of main rotor blades
1
45 empty fields

Family, Model, Variant, Code Name, IATA Code, ICAO Code, EASA TCDSN, Program Launch, Roll Out, Certification, Entry Into service, Launch Customer, Production End, Service End, Category, Width, Line Logo, White Logo, One Class Typical Seating, Two Class Typical Seating, Three Class Typical Seating, Cargo Volume, Unit Load Devices, Min Speed, Optimum Ceiling, List Price, Armament, Endurance, Max Mach, Primary Users, Status, Aircraft Engine, APU, Variable Cost Per Hour, EASA Noise Chapter, Lateral Noise Level, Flyover Noise Level, Approac hNoise Level, Cumulative Noise Level, Number of Rotors, Rotor, Number of tail rotor, Number of tail rotor blades, Tail Propeller, Main Rotor Diameter