Hiller Aircraft Corporation was founded in 1994 by Jeffrey Hiller (son of the founder of the original Hiller Aircraft company) and a consortium, to repurchase assets from Rogerson Hiller Corporation. First flight January 1995 of the UH-12E5 five-seat helicopter, and June 1995 for first newly built UH-12E3. Current production is believed to center on the piston-engined UH- 12E3 three-seater and the UH-12E3T turboshaft variant.

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Technical data for Hiller UH-12E5 Engine: Lycoming VO-540-C2A pistone engine, rated at 250kW, main rotor diameter: 10.79m, take-off weight: 1406kg, empty weight: 871kg, max speed: 155km/h, cruising speed: 145km/h, hovering ceiling, OGE: 2070m, service ceiling: 4500m, range: 374km

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