CURTISS JN-4 Civil Aircraft Model Details

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General Information of CURTISS JN-4

Designer : Benjamin D. Thomas

Introduction : 1915

Manufacturer : Curtiss

Number Built : 6813

Primary Users : U.S. Army Air Service; Royal Flying Corps

Role : Trainer

Unit_Cost : 5465

Variants : Curtiss N-9; Curtiss JN-6H

General characteristics of CURTISS JN-4

Crew : two

Empty Weight : 1,390 lb (630 kg)

Height : 9 ft 10½ in (3.01 m)

Length : 27 ft 4 in (8.33 m)

Max Takeoff Weight : 1,920 lb (871 kg)

Powerplant : 1 × Curtiss OX-5 V8 piston, 90 hp (67 kW)

Wing Area : 352 ft2 (32.7 m2)

Wingspan : 43 ft 7¾ in (13.3 m)

Performance of CURTISS JN-4

Cruise Speed : 60 mph (52 kn, 97 km/h)

Endurance : 2h

Maximum Speed : 75 mph (65 kn, 121 km/h)

Service Ceiling : 6,500 ft (2,000 m)

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