Hall-Scott A-7
From Wikipedia, the free encyclopedia
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.
[edit] Applications
- Aeromarine 39
- Dayton-Wright FS
- Standard J-1
[edit] References
- Gunston, Bill. (1986). World Encyclopaedia of Aero Engines. Patrick Stephens: Wellingborough. p.73
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