HALL-SCOTT A-7

Hall-Scott A-7 at Canada Aviation Museum

The 'Hall-Scott A-7' was an early aircraft engine. Of straight-4 configuration, it developed 100 hp (75 kW). These engines suffered from reliability problems and were prone to catch fire while in operation.

Contents
Applications
References

Applications



★ Aeromarine 39

★ Dayton-Wright FS

★ Standard J-1

References



★ Gunston, Bill. (1986). ''World Encyclopaedia of Aero Engines''. Patrick Stephens: Wellingborough. p.73

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