Hall-Scott A-7
The Hall-Scott A-7 was an early aircraft engine manufactured by the Hall-Scott company of Berkeley, California. Of straight-4 configuration, it developed 100 horsepower (75 kW). These engines suffered from reliability problems and were prone to catch fire while in operation.
Applications
Specifications
General characteristics
- Type: Four-cylinder inline piston engine
Performance
- Power output: 100 hp (75 kW)
See also
- Related lists
References
- Gunston, Bill. (1986). World Encyclopaedia of Aero Engines. Patrick Stephens: Wellingborough. p.73
External links
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- 60 hp
- A-1
- A-2
- A-3
- A-4
- A-5
- A-5A
- A-7
- A7a
- A-8
- L-4
- L-6
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