1984


Westland 30

30-300





Improved version with 5 bladed BERP main rotor and crash hardened landing gear. Single airframe produced first flew on 5 Feb 1986.


Specifications 30-300


Engine 2 x GE CT7-2B 1712 shp
Capacity 2
Length (m) 15.9
Height (m) 4.39
Blades 5
Rotor diam. (m) 13.31
Disc area (m2)
Weight (kgs) Empty: 3765
Speed (km/h)     Max: 277
Range (km) 270
Ceiling (m)
Rate/Climb (m/min)
blueprints


  List of Operators of 30-300


Years Model Org
1982/?? 30 united kingdom Westland



  Global Distribution of 30-300



130-300


Construction Numbers


C/N Year History
020 UK G-HAUL








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