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Eurocopter EC135P2+

2006 · Twin-engine light turbine helicopter

History C/N Operators News
Powered by two 463 kW (621 shp) Pratt & Whitney Canada PW206B2 with FADEC, extended component time between overhaul (TBOs) and a change in the main transmission lubricating oil. Aircraft upgraded to this standard ( not built ) are known as EC135P2i.
From 2014 manufactured by Airbus

Specifications

Engine2 x Pratt & Whitney Canada PW206B2 447 shp
Capacity1 + 5
Length (m)12.16
Height (m)3.51
Blades4
Rotor diam. (m)10.2
Disc area (m2)81.7
Weight (kgs)Empty: 1455 Max: 2910
Speed (km/h)Cruise: 254 Max: 285
Range (km)630
Ceiling (m)6100
Rate/Climb (m/min)457
blueprints EC135P2+