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Information About

North American Na-16




The North American NA-16 was the first trainer aircraft built by North American Aviation, Inc. and was the beginning of a line of North American trainer aircraft that would number more than 17,000 derivatives. The NA-16 was a single engine, low-wing monoplane with tandem seating in open cockpits and fix landing gear. A Wright Whirlwind radial air-cooled engine of 400 hp powered the aircraft. While it was mostly of metal construction, the rear fuselage was fabric covered.

The NA-16 flew for the first time on April 1, 1935 and was submitted to the U.S. Army Air Corps for evaluation as a basic trainer. The Army accepted the trainer for production but with some significant changes. These changes included replacing the Wright engine with a Pratt and Whitney R-1340 engine and enclosing the cockpits as well as fairing the landing gear. The modified NA-16 was re-designated by North American as the NA-18.


SPECIFICATIONS (NA-16)


General characteristics

  • Crew: two

  • Length: 27 ft 7 in (8.41 m)

  • Wingspan: 42 ft (12.80 m)

  • Height: ft ( m)

  • Wing area: ft² ( m²)

  • Empty: 3,078 lb (1399 kg)

  • Loaded: lb ( kg)

  • Maximum takeoff: lb ( kg)

  • Powerplant: 1× Wright Whirlwind 400 shp (298.4 kW) each



Performance

  • Maximum speed: 170 mph (273.7 km/h)

  • Range: 700 miles (1127 km)

  • Service ceiling: ft ( m)

  • Rate of climb: ft/min ( m/min)

  • Wing loading: lb/ft² ( kg/m²)

  • Power/mass: 0. hp/lb (0. kW/kg)



Armament

None


RELATED CONTENT

Related development:
North American NA-18
North American BT-9
North American BC-1
T-6 Texan

Comparable aircraft:

Designation sequence: