Derived from the Model 107 and also known as the UH-46A under the US Navy.  Developed in 1960, the Model 107-2 is a commercial passenger-transport helicopter with a capacity of 25; weight fully loaded is 21400 lb (9707 kg).  Two of the organizations to first order the aircraft are New York Airways (replacing the Vertol 44) and the Royal Swedish Navy [Ref. 312, 316]

Overview

Data on design, manufacture and status

Design authority: Vertol Aircraft Corporation

Primary manufacturer: Vertol Aircraft Corporation

Parent type: Vertol Model 107/CH-46

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

Overall Height: 5.13 m (16.8 ft)

Overall Length: 25.40 m (83.3 ft)

Overall Width: 14.73 m (48.3 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: GE T58-GE-8 turbine

Engine manufacturer: GE Aviation

Take-off / rated power: 932 kW (1249 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 7734 kg (17050 lb)

Max Range: 431 km (233 nm)

Related VFS Resources

Resources related to the CH-46A (HRB-1) Sea Knight, provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
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Web files from vtol.org
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Related Public Resources

Resources related to the CH-46A (HRB-1) Sea Knight, provided by public sources across the internet.

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