MGW is 3850 kg  without the addition of a Service Bulletin

Overview

Data on design, manufacture and status

Latest or last design authority: Airbus Helicopters
Originally designed by Sud-Aviation

Primary manufacturer: Société Nationale Industrielle Aérospatiale

Parent type: Aérospatiale H155/EC155/AS365/SA.365

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Fenestron/Shrouded tail rotor

Crew required: 1 in Side-by-side arrangement

Landing gear: Wheels (all retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

References

References and sources used

The Twin-Engine BO-105
A.C. Ballauer and P. F. Sheridan
VERTIFLITE August 1969, August 1969
Periodical
Good description of the overall vehicle

TypeCertificate Data Sheet No. EASA.R.105 Iss. 03
EASA
EASA TCDS web site, 8 December 2015 (page 14)
Website

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Related Public Resources

Resources related to the SA.365N Dauphin 2, provided by public sources across the internet.

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