Westland 30

30-300

1984








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


Specifications


Engine: 2 x GE CT7-2B 1712shp
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 Westland 30-300


From Organisation with model 30-300
1982
united kingdom Westland
    30 1982/??


Construction Numbers on database of 30-300

130-300




Construction Numbers

Help Us

C/NYearHistory
020 UK G-HAUL : Westland 30-300 TT300; G-17-22; 24jul93 pictured preser+


1 C/N.

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