142:, was conceived as a more powerful and faster aircraft similar to the LK-4, able to be produced in several versions to carry out different tasks. The three variants tested were intended for military training of pilots and crewmen. Construction was of wood throughout with some fabric covering. Testing at Leningrad was successfully completed by February 1937 when the aircraft was transferred to NII VVS (
146:– scientific test institute of the soviet air force), for further testing, a production order was anticipated but the prototype crashed irreparably, due to pilot error, and no production was authorised.
65:
127:
In 1930 the LIIPS ( - Leningrad institute for sail and communications engineers) formed a UK GVF ( - training centre for civil air fleet), in turn the UK GVF formed the NIAI (
139:
180:
and other biplane fighters: The upper wing centre-section was removed along with the side cabane struts and the rear cockpit was faired over.
364:
131:- scientific test aero-institute) which became the focus of several good design engineers who were given command of individual OKB (
50:
374:
348:
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and other monoplane fighter pilots, the P-3 ON had a cantilever lower wing only and a smaller tailplane.
115:- Leningrad Institute civil air fleet), was a multi-purpose trainer aircraft designed and built in the
369:
343:
Gunston, Bill. “The Osprey
Encyclopaedia of Russian Aircraft 1875–1995”. London, Osprey. 1995.
8:
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Gunston, Bill. "Encyclopaedia of
Russian Aircraft 1875-1995". London:Osprey. 1995.
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1 x 7.62mm ShKAS forward-firing fixed in the forward fuselage.
162:– two-seat sesquiplane) For training pilots and observers for
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Naoochno-Issledovatel'skiy
Institoot Voyenno-Vozdooshnykh Seel
138:
The P-3 was designed by
Anatolii Georgievich Bedunkovich, an
116:
40:
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1 x 7,62mm ShKAS ona flexible mount in the rear cockpit.
113:
Leningradskii
Institoot Grazdahnskovo Vozdooshnovo Flota
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190:– single-seat low-wing monoplane) For training
176:– single-seat biplane) For training pilots of
281:157 km/h (97.5 mph, 84.7 kn)
201:
129:Naoochno-Issledovatel'skiy Aero-Institoot
55:Naoochno-Issledovatel'skiy Aero-Institoot
135:– personal design/construction bureau).
287:850 km (528 mi, 459 nmi)
266:1 × MG-31 , 223.8 kW (300 hp)
357:
299:2.7777 m/s (5,436.8 ft/min)
242:10.6 m (34 ft 9.33 in)
236:7.5 m (24 ft 7.25 in)
365:1930s Soviet civil trainer aircraft
13:
57:- scientific test aero-institute)
14:
386:
66:Anatolii Georgievich Bedunkovich
248:30 m (323 sq ft)
133:Osboye Konstrooktorskoye Byuro
122:
1:
336:
293:3,300 m (10,826 ft)
260:1,560 kg (3,439 lb)
254:1,100 kg (2,425 lb)
375:Aircraft first flown in 1934
7:
319:
149:
10:
391:
18:
221:General characteristics
202:Specifications (P-3DP)
160:Dvukmestnyi Polutoplan
188:Odnomestnyi Nizkoplan
166:and similar aircraft.
27:Multi-purpose trainer
174:Odnomestnyi Biplan
101:
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331:List of aircraft
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291:Service ceiling:
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140:Engineer Colonel
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29:Type of aircraft
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36:National origin
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297:Rate of climb:
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279:Maximum speed:
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91:Developed from
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370:NIAI aircraft
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325:Related lists
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72:First flight
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81:Number built
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272:Performance
264:Powerplant:
123:Development
119:from 1936.
75:early 1934
359:Categories
337:References
246:Wing area:
107:, (a.k.a.
240:Wingspan:
207:Data from
96:NIAI LK-4
62:Designer
320:See also
305:Armament
150:Variants
234:Length:
347:
285:Range:
213:
228:Crew:
184:P-3ON
170:P-3OB
156:P-3DP
109:LIG-5
24:Role
345:ISBN
211:ISBN
192:I-16
178:I-15
117:USSR
103:The
51:NIAI
41:USSR
19:P-3
186:– (
172:– (
164:R-5
158:– (
105:P-3
361::
85:1
230:2
111:(
53:(
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