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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