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St. Louis PT LM 4

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First flight
  
1940

St. Louis PT-LM-4 httpsuploadwikimediaorgwikipediacommonsthu

Manufacturer
  
St. Louis Aircraft Corporation

The St. Louis PT-LM-4 was a primary trainer design for use in the Civilian Pilot Training Program of World War II.

Contents

Design

The PT-LM-4 was a low-wing, open cockpit, tandem seat, trainer with conventional landing gear, powered by a 180 hp (134 kW) Ranger 6-440C-3 engine. The fuselage was constructed of welded steel tubing with aluminum skins. The wings used aluminum construction with aircraft fabric covering. Fairchild won the training contract, with St. Louis Aircraft Company building licensed versions of the PT-19 instead.

Specifications (PT-LM-4)

Data from Skyways

General characteristics

  • Crew: 2
  • Length: 24 ft 9 in (7.54 m)
  • Wingspan: 30 ft (9.1 m)
  • Height: 7 ft 10 in (2.39 m)
  • Wing area: 157 sq ft (14.6 m2)
  • Gross weight: 2,012 lb (913 kg)
  • Powerplant: 1 × Ranger 6-440C-3 inline piston engine, 180 hp (130 kW)

    • Performance

  • Maximum speed: 119 kn; 220 km/h (137 mph)
  • Cruise speed: 109 kn; 201 km/h (125 mph)
  • Service ceiling: 18,000 ft (5,500 m)
  • Rate of climb: 1,000 ft/min (5.1 m/s)

    • References

    St. Louis PT-LM-4 Wikipedia
    (Text) CC BY-SA


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