Aérospatiale SA.365 Twin Dauphin
The aircraft was later re-named the Dauphin 2
Overview
Data on design, manufacture and statusDesign authority: Société Nationale Industrielle Aérospatiale
Primary manufacturer: Société Nationale Industrielle Aérospatiale
Parent type: Aérospatiale H155/EC155/AS365/SA.365
Aircraft status: Status unknown
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Fenestron/Shrouded tail rotor
Crew required: 1-2 in Side-by-side arrangement
Landing gear: Wheels (some retractable)
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used
Twin-engined Dauphin set for January deliveries
FLIGHT staff
Flightglobal/Archive, 8 October, 1977 (page 996)
Periodical
Detailed description of the aircraft and its characteristics
Flightglobal/Archive, 8 October, 1977 (page 996)
Periodical
Detailed description of the aircraft and its characteristics
Related VFS Resources
Resources related to the SA.365 Twin Dauphin, provided by the Vertical Flight Society.Forum Proceedings
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.
Images from the VFS Gallery
Enter a search term in the box above.
