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Towle TA 2

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First flight
  
November 7, 1929

Designer
  
Thomas Towle

Manufacturer
  
Towle Marine Aircraft Engineering

The Towle TA-2 was an amphibious aircraft based on the T owle WC built for a 1929 round-the world flight.

Contents

Development

Thomas Towle was an engineer that had been involved with many early aircraft designs. Having just co-designed the Eastman E-2 Sea Rover and the Towle WC. Towle found funding to create a new entity, the Towle Aircraft Company to produce the TA-2.

Design

The TA-2 featured an corrugated aluminum hull. The wings were all metal with internal stiffeners, rather than ribs, based loosely on the Ford Trimotor, which Towle worked on previously. The twin Wright R-540 engines sat on small pylons on top of the shoulder mounted wing. Two floats were mounted directly below the engine pylons which incorporated the hydraulically actuated landing gear. The prototype was originally designed for 165 hp Wright 540 engines.

Operational history

The TA-2 was tested in Lake St. Clair on 7 November 1929 by test pilot George Pond and James Bradley. It broke up on takeoff and sank to the bottom of the lake. The aircraft appears to have been rebuilt as a Towle TA-2 was reported to have visited Lympne Airport, Kent, United Kingdom in February 1930. The wing from the prototype was salvaged and used on the next iteration, the Towle TA-3.

Variants

  • Towle WC The basis for the TA-2
  • Specifications

    Data from Flight, 14 February 1930, pp215-16.

    General characteristics

  • Crew: 1
  • Capacity: 5 passengers
  • Length: 33 ft (10 m)
  • Wingspan: 47 ft 9 in (14.55 m)
  • Wing area: 292 sq ft (27.1 m2)
  • Gross weight: 4,420 lb (2,005 kg)
  • Fuel capacity: 90 US gallons (340 l; 75 imp gal)
  • Powerplant: 2 × Wright R-540 radial, 165 hp (123 kW) each
  • Propellers: 2-bladed
  • Performance

  • Maximum speed: 117 kn; 217 km/h (135 mph)
  • Range: 600 nmi (690 mi; 1,111 km)
  • Wing loading: 15.15 lb/sq ft (74.0 kg/m2)
  • References

    Towle TA-2 Wikipedia