The most popular uses of this engine were in the Fouga CM.170 Magister and the Morane-Saulnier MS.760 Paris.

It was also licensed for production in the United States as the Teledyne CAE J69.

A typical weight for this series of engines is 140 kg (310 lb).

Fuel consumption is 720 L/h (160 imp gal/h; 190 gal/h) on the Marboré VI at 4,500 m (14,800 ft), as compared to 520 L/h (110 imp gal/h; 140 gal/h) on Marboré II engines (same altitude), as well as an increase of fuel consumption of 27% and a decrease in cruise range capabilities.

[2] Data from FAA TCDS,[4] Aircraft engines of the World 1953[5] Related development