The Turbomeca Bastan was a turboprop engine developed in France in 1957. Early models developed 650 shp (485 kW), but by 1965 this had been increased to 1,048 shp (780 kW) with the Bastan VII.

Flight tests of some Bastan models were carried out using a Lockheed Constellation flying test bed. The engine's principal applications were the Aérospatiale N 262 (Nord 262) and Nord 260 airliners.

Turbomeca Bastan

The Bastan was also developed into the Turbomeca Aubisque turbofan.

Turbomeca Bastan

Applications

Aérospatiale N 262

FMA IA 50 Guaraní II

Nord 260

Sud Aviation SE.116 Voltigeur

Sud Aviation SE.117 Voltigeur

Variants

Bastan IV

Bastan VI

Bastan VIA1

Bastan VIB1

Bastan VIB2

Bastan VIC

Bastan VIC1

Bastan VII

Bastan 16

Bastafan

Bi-Bastan IV A paired Bastan IV developed for French-modified Sikorsky S-58 helicopters. De-rated to

Turbomeca Bastan

Specifications (Bastan VIC)

See also

References

Bastan

1950s turboprop engines