HOWARD DGA-15 Civil Aircraft Model Details

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General Information of HOWARD DGA-15

Designer : Benny Howard

Developed From : Howard DGA-12

Introduction : 1939

Manufacturer : Howard Aircraft Corporation

Number Built : 520

Primary Users : US Navy

Produced : 1939-1944

Role : Civil transport

General characteristics of HOWARD DGA-15

Airfoil : NACA 2R212 (reflexed)

Capacity : 3-4 passengers (NH-1 trainer has additional blind flight student station behind pilot)

Crew : one, pilot

Empty Weight : 2,700 lb (1,225 kg)

Height : 8 ft 5 in (2.57 m)

Length : 25 ft 8 in (7.82 m)

Loaded_Weight : 4,350 lb (USN aircraft : 4,500 lb) (1,973 kg)

Max Takeoff Weight : 4,350 lb (1,973 kg)

Powerplant : 1 × Pratt & Whitney R-985 radial engine, 450 hp (336 kW)

Wing Area : 210 ft² (19.5 m² (Note : the wing span and chord are the same as the earlier DGA-11, but the DGA-15 area is calculated including the area displaced by the fuselage cabin))

Wingspan : 38 ft 0 in (11.58 m)

Performance of HOWARD DGA-15

Maximum Speed : 175 knots (201 mph, 323 km/h)

Never Exceed Speed : 235 knots (270 mph, 437 km/h)

Power/Mass : 0.100 hp/lb (0.165 kW/kg)

Range : 1,095 nm (1,260 mi, 2,028 km)

Rate Of Climb : 1,800 ft/min (550 m/min)

Service Ceiling : 21,000 ft (6,555 m)

Wing Loading : 21.3 lb/ft² (104.7 kg/m²)

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