Atlantic Aircraft Corporation
/ Atlantic Fokker F-14 / C-14
Atlantic Fokker F-14 / C-14
The F-14 was a typical Fokker designed single-engine transport but unusually it had a parasol-type high wing carried on struts above the fuselage.
It had a fixed tail wheel landing gear.
The pilot had a cockpit behind the passenger cabin.
Civil production version with a 525 hp (391 kW) Wright R-1750-3 radial engine.
Civilian aircraft with 575 hp (429 kW) Pratt & Whitney R-1690 Hornet radial and wing mounted directly on fuselage.
Designation for 20 Hornet-powered examples bought for the United States Army Air Corps in 1931, later became the C-14.
Last of the 20 Y1C-14s re-engine with a 575 hp (429 kW) Wright R-1820-7 Cyclone.
Re-engine with a 525 hp (391 kW) Pratt & Whitney R-1690-5 Hornet.
Conversion of the ninth Y1C-14 as an air ambulance.
F-14 re-engine with a 575 hp (429 kW) Wright R-1820 Cyclone, later C-15A.
43 ft 3 in (13.18 m)
59 ft 5 in (18.11 m)
12 ft 4 in (3.76 m)
551 sq ft (51.19 m2)
4,346 lb (1,971 kg)
7,200 lb (3,266 kg)
1 × Wright R-1750-3 9-cylinder radial , 525 hp (391 kW)
137 mph (220 km/h, 119 kn)
690 mi (1,100 km, 600 nmi)
14,500 ft (4,420 m).
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