Samiksha Jaiswal (Editor)

Daytona Aircraft D 200

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Manufacturer
  
Daytona Aircraft

The Daytona Aircraft D-200 is one of a series of American training aircraft developed in the 1990s by Daytona Aircraft.

Contents

Development

The DA-200 is a two place side-by-side configuration, low wing aircraft with tricycle landing gear and gull wing doors. It features a double tapered wing, similar to a Mooney 201, and a swept tail with dorsal fin similar to a Cessna 172. The aircraft uses all aluminum construction. It was the first demonstrated in a line of aircraft intended to be built in Fargo, North Dakota. The producers hoped to capitalize on the lack of prior manufacturing liability.

Variants

D-160
D-180
D-200
Two seat prototype
D-250
D-270
D-300

Specifications (D-200)

Data from Jane's All The World's Aircraft 1992–93

General characteristics

  • Crew: 1
  • Capacity: 3 passengers
  • Length: 25 ft 11 in (7.90 m)
  • Wingspan: 36 ft 0 in (10.97 m)
  • Height: 7 ft 8 in (2.34 m)
  • Wing area: 162.8 sq ft (15.12 m2)
  • Aspect ratio: 7.96:1
  • Empty weight: 1,250 lb (567 kg)
  • Max takeoff weight: 2,500 lb (1,134 kg)
  • Powerplant: 1 × Lycoming horizontally opposed piston aircraft engine, 200 hp (150 kW)
  • Propellers: 2-bladed

    • Performance

  • Maximum speed: 175 kn (201 mph; 324 km/h)
  • Cruise speed: 165 kn (190 mph; 306 km/h) (75% power)
  • Stall speed: 51 kn (59 mph; 94 km/h) (flaps and undercarriage down)
  • Range: 1,275 nmi (1,467 mi; 2,361 km)
  • Endurance: 7 hr 44 min
  • Service ceiling: 18,000 ft (5,500 m)
  • G limits: +6 -3
  • Rate of climb: 1,000 ft/min (5.1 m/s)
  • Take-off to 50 ft (15 m): 1,319 feet (402 m)
  • Landing from 50 ft (15 m): 1,220 feet (370 m)

    • References

    Daytona Aircraft D-200 Wikipedia
    (Text) CC BY-SA