Sud Aviation/Aérospatiale SA-360 Dauphin

Rotorcraft

Aircraft Information

ICAO Code
S360
Manufacturer
Sud Aviation/Aérospatiale
Model
SA-360 Dauphin
Aircraft Type
Rotorcraft
Primary Role
Transport

Technical Data

Engine Type
Turboshaft
Engine Model
Astazou XVIII
Production Years
1974-1975
Units Produced
36
First Flight
1972-06-02
Notable Operators
New York Helicopter, French regional airlines

The Aérospatiale SA-360 Dauphin was a pioneering medium-lift helicopter that introduced the innovative fenestron anti-torque system to commercial aviation. First flown on June 2, 1972, it was a single-engine turboshaft helicopter capable of carrying one pilot plus nine passengers in its distinctively glazed fuselage. Measuring 13.20 meters overall length with an 11.50-meter main rotor diameter, the SA-360 achieved notable speed records before production limitations led to only 36 aircraft being built by Aérospatiale between 1974 and 1975.

Development and Innovation

The SA-360 Dauphin emerged from Sud Aviation's ambitious goal to create a successor to the successful Alouette III helicopter. The design team incorporated several groundbreaking technologies, most notably the fenestron tail rotor system borrowed from the Gazelle helicopter. This shrouded tail rotor configuration reduced noise and improved safety compared to conventional exposed tail rotors.

The prototype initially flew with a Turbomeca Astazou XVI engine, but after 180 test flights, engineers recognized the need for more power. The aircraft was subsequently modified with the more powerful Astazou XVIII turboshaft engine producing 1,050 shaft horsepower, along with composite rotor blades to reduce problematic vibrations and ground resonance issues.

Record-Breaking Performance

Despite its technical challenges, the SA-360 demonstrated impressive performance capabilities. At the 1973 Le Bourget Air Show, test pilot Roland Coffignot established multiple speed records in the E1D helicopter class (1,750-3,000 kg category). The aircraft achieved 299 km/h over a 100-kilometer circuit, reached 312 km/h in straight-line flight over 3 kilometers, and maintained 303 km/h over a 15-kilometer course.

These achievements showcased the potential of the SA-360's aerodynamic design, which featured a fully-glazed forward fuselage providing excellent visibility and a spacious cabin capable of accommodating up to ten occupants in various configurations.

Manufacturing Heritage

Sud Aviation, the original manufacturer, represented a significant consolidation in French aerospace when it formed in 1957 through the merger of Sud-Est and Sud-Ouest companies. By 1970, Sud Aviation itself became part of an even larger nationalization effort, merging with Nord Aviation and SEREB to create Aérospatiale. This company would continue through subsequent transformations, becoming Eurocopter in 1992 and ultimately Airbus Helicopters in 2014.

Limited Production Run

The SA-360's commercial prospects were hampered by its fundamental limitation: insufficient power. Production began in 1974 with the SA-360C variant, but the program concluded quickly with only 34 production aircraft joining the two original prototypes. The single Astazou XVIII engine, while reliable, could not provide adequate performance margins for the helicopter's intended missions, particularly in challenging operating conditions.

Three military variants were explored but never reached full production. The SA-360A naval variant completed its first flight on May 4, 1973, using the modified original prototype. The SA-361H represented a more ambitious upgrade, with three aircraft converted from SA-360C airframes and equipped with the more powerful Astazou XX engine and advanced Starflex rotor system, but this variant also failed to achieve production status.

Operational Service

Despite limited numbers, SA-360 helicopters found service across multiple continents. French operators utilized the aircraft on scheduled passenger routes in southern France, while international customers included operators in Japan and the United States. New York Helicopter operated at least one SA-360 (serial number 1023, registration N8479U), demonstrating the type's capability in demanding urban environments.

The helicopter's spacious cabin and large windows made it particularly suitable for VIP transport and executive missions, where passenger comfort took precedence over maximum efficiency. However, the power limitations restricted operations in hot weather or high-altitude conditions where turbine performance typically degrades.

Technical Legacy

While commercially unsuccessful, the SA-360 proved invaluable as a technology demonstrator. The fenestron tail rotor system, composite rotor blade technology, and various design elements were refined and incorporated into the subsequent SA-365 Dauphin. This twin-engine successor addressed the SA-360's power limitations and became far more successful, with the SA-365N eventually setting its own speed record of 371 km/h over 3 kilometers on November 24, 1989.

The Starflex rotor system, tested on the SA-361H variants, would later become standard equipment on advanced Eurocopter designs, including the EC-155 and other modern helicopters.

Current Status

By 2000, only nine SA-360 helicopters remained in operation worldwide, reflecting the type's transition from active service to historical significance. At least one example has been preserved for posterity: the former New York Helicopter aircraft (N8479U) arrived at the CELAG museum in France on February 17, 2001, where it represents this important stepping stone in helicopter development.

The SA-360 Dauphin's brief production run and rapid replacement should not overshadow its contributions to rotorcraft technology. Its innovations in anti-torque systems, rotor blade design, and aerodynamic efficiency provided crucial foundations for more successful helicopter programs that followed.