Aerotécnica AC-14
The pilot sat in front of 2 side-by-side passenger seats. Anti-torque control was provided through a gas ejection outlet at the end of the tail boom with deflectors that could control the direction of thrust.
Source: ”Helicopters & Autogyros of the World”, Paul Lambermont with Anthony Pirie, Second edition 1970, Cassell & Company Ltd, SBN 304 93390 2
Overview
Data on design, manufacture and statusDesign authority: Aerotécnica
Primary manufacturer: Aerotécnica
Parent type: No type defined
Aircraft status: No longer flying
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Thruster
Crew required: 1
Crew seating: Other
Landing gear: Skids
Overall Dimensions
Data on aircraft sizeEngine Details
Aircraft powerplant (lift and/or propulsion)Total number of engines: 1
Engine designation: Turbomeca Artouste II turbine
Engine manufacturer: Turbomeca
Take-off / rated power: 269 kW (360 hp)
Weights and Performance
Data on aircraft weight and flight characteristicsMax Gross Weight (ground): 1200 kg (2646 lb)
