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On 7 March 1925, Curtiss was awarded a contract for 15
production examples of the XPW-8B as the P-1, this
being the first fighter to which the company assigned the name Hawk. Externally similar to the XPW-8B, the
P-1 was of mixed construction with wooden wings and
steel-tube fuselage with fabric skinning, and was
powered by a 435hp Curtiss V-1150-1 12-cylinder
water-cooled engine. The final five aircraft were completed
as P-2s, three of these later being converted to
P-1A standards. Follow-on contracts were placed on 9
September 1925 for 25 P-1As (which had a 7.62cm
longer fuselage); on 17 August 1926 for 25 P-1Bs (with
V-1150-3 engine, larger wheels and modified radiator),
and on 3 October 1928 for 33 P-1Cs (with wheel brakes).
All these sub-types carried an armament of two 7.62mm guns. In the meantime, the USAAC had
ordered advanced trainers utilising the same airframe,
these comprising 35 AT-4s (180hp Wright V-720), five
AT-5s and 31 AT-5As (220hp Wright R-790), and, in
1929, these were re-engined with the V-1150-3, all 35
AT-4s becoming P-1Ds and four AT-5s and 24 AT-5As
becoming P-1Es and P-1Fs respectively. These conversions
were essentially similar to the P-1B apart from
having only one gun. Four P-1s were supplied to Bolivia,
one P-1A went to Japan, and eight P-1As and eight
P-1Bs were supplied to Chile.
| MODEL | P-1B |
| WEIGHTS |
| Take-off weight | 1 330 kg | 2 lb |
| Empty weight | 955 kg | 2105 lb |
| DIMENSIONS |
| Wingspan | 9.63 m | 31 ft 7 in |
| Length | 6.91 m | 22 ft 8 in |
| Height | 2.72 m | 8 ft 11 in |
| Wing area | 23.23 m2 | 250.05 sq ft |
| PERFORMANCE |
| Range | 966 km | 600 miles |
 | A three-view drawing (1280 x 892) |
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