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Boeing T-50-BO-4

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This engine was the result of a development program dating back to 1943. The production engine resulted in a design used by drone anti-submarine helicopters through the mid 1960s.

Technical Specifications
Rated Output 270 hp at 5,950 r.p.m.
Compressor Centrifugal 2 Stage
Turbine Turbine 2 Stage
Commonly Used On QH-50


Location: Hangar 1 North