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To meet a US Marine Corps requirement for a two-seat
fighter with bombing and observation capability, Curtiss
adapted the airframe of the USAAC's O-1 Falcon.
With a Pratt & Whitney R-1340 Wasp radial engine in
place of the water-cooled Conqueror six examples were
delivered, two as XF8C-1s and four as F8C-1s, in
January 1928. Armament comprised two fixed forwardfiring
7.62mm guns and a weapon of similar
calibre on a Scarff ring in the rear cockpit, and power
was provided by a 432hp R-1340B Wasp. Twenty-one
additional machines (one XF8C-3 and 20 F8C-3s) were
delivered later in 1928, these being essentially similar to the F8C-1s which were redesignated as OC-1s
shortly after entering service, the F8C-3s becoming
OC-2s.
| WEIGHTS |
| Take-off weight | 1901 kg | 4191 lb |
| Empty weight | 1141 kg | 2515 lb |
| DIMENSIONS |
| Wingspan | 11.58 m | 37 ft 12 in |
| Length | 8.51 m | 27 ft 11 in |
| Height | 3.55 m | 11 ft 8 in |
| Wing area | 32.52 m2 | 350.04 sq ft |
| PERFORMANCE |
| Max. speed | 232 km/h | 144 mph |
| Range | 1046 km | 650 miles |
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