Equipped with Sperry autopiloting, the H-25 was used for evacuation, utility and SAR.  Passenger capacity is six, including the pilots.

Overview

Data on design, manufacture and status

Design authority: Piasecki Helicopter Corporation

Primary manufacturer: Piasecki Helicopter Corporation

Parent type: No type defined

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Tandem (Fore/aft) (x2)

Crew required: 2

Crew seating: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Continental R-975-46 reciprocating

Engine manufacturer: Continental Motors

Take-off / rated power: 410 kW (550 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 2767 kg (6100 lb)

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Related Public Resources

Resources related to the H-25 Army Mule (HUP-2 Navy), provided by public sources across the internet.

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