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Howard DGA 18

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First flight
  
1941

Howard DGA-18 wwwhowardaircraftorgimagesslideshowsaircraft

Manufacturer
  
Howard Aircraft Corporation

The Howard DGA-18 was an American two-seat basic training aircraft designed and built by the Howard Aircraft Corporation for the United States Civil Pilot Training Program.

Contents

Design

The DGA-18 was a low-wing cantilever monoplane with two tandem open cockpits and a fixed conventional landing gear. The aircraft was built in three variants with different engines fitted.

Variants

DGA-18 (or DGA-125)
Variant powered by a 125 hp (93 kW) Warner Scarab 50 radial engine.
DGA-18K (or DGA-160)
Variant powered by a 160 hp (119 kW) Kinner R-5 radial engine.
DGA-18W (or DGA-145)
Variant powered by a 145 hp (108 kW) Warner Super Scarab radial engine.

Specifications (DGA-18)

Data from Some Damn Good Airplanes

General characteristics

  • Crew: 2
  • Length: 26 ft 6 in (8.08 m)
  • Wingspan: 34 ft 0 in (10.36 m)
  • Height: 7 ft 3 in (2.21 m)
  • Wing area: 179.5 sq ft (16.68 m2)
  • Empty weight: 1,350 lb (612 kg)
  • Max takeoff weight: 1,950 lb (885 kg)
  • Fuel capacity: 31 US Gal (117 L)
  • Powerplant: 1 × Warner Scarab 50 7-cylinder air-cooled radial engine, 125 hp (93 kW)
  • Performance

  • Maximum speed: 118 mph (190 km/h; 103 kn) at sea level
  • Cruise speed: 108 mph (174 km/h; 94 kn)
  • Range: 380 mi (330 nmi; 612 km)
  • Endurance: 3.5 hr
  • Service ceiling: 13,500 ft (4,100 m)
  • Rate of climb: 800 ft/min (4.1 m/s)
  • References

    Howard DGA-18 Wikipedia


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