217:. Fuselage rectangular in cross-section, built on a steel frame, covered with canvas and aluminum in engine part. Rectangular two-section wings with rounded tips, two-spar, covered with plywood in forward part and canvas in a rear part, supported with upper struts. Crew of two, sitting in tandem in open cockpits with windshields, fitted with dual controls. A luggage compartment behind a cockpit. Conventional fixed
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Later the plane took part in some competitions in Poland, without much success, among others it took the 10th place in the 3rd Polish Light
Aircraft Contest in 1930. In 1931 during repair, a radial engine Genet was replaced with a radial engine
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NZ 5-cylinder radial engine, 85 HP nominal power, and Cirrus III 4-cylinder straight engine, 85 HP nominal and 94 take-off power). Two-blade wooden propeller of a fixed pitch. Fuel tank 100 L before a cockpit. Fuel consumption - 22 L/hour.
179:. It was used then by an Aviation Club of the PWS factory. In June 1933 the plane was damaged. During repair it was fitted with a straight engine Cirrus III (from broken up
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143:. It's noteworthy, that it was only 10 kg heavier, and its maximum speed was 15 km/h higher, than estimated.
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5-cylinder air-cooled radial piston engine, 60 kW (80 hp) to 66 kW (88 hp)
244:
Jane's all the World's
Aircraft 1931, Poser - PWS - Podlaska Wytwórnia Samolotów : PWS-51
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159:. He completed most of a rally over Europe, but had to withdraw after a forced landing near
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was a Polish sports plane of 1930, a single-engine low-wing monoplane, constructed by the
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in front, 80 hp nominal power and 88 hp take-off power (later replaced with
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120 km/h (75 mph, 65 kn) to 140 km/h (87 mph; 76 kn)
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organization and it was first flown in spring of 1930 by
Franciszek Rutkowski in
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The prototype, with markings SP-ADC and contest number O7, took part in the
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398:. London: Sampson Low, Marston & company, ltd. p. 221c.
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in 2–4 February 1934, flown by A. Uszacki, and was broken up.
119:, on factory's initiative, specially to participate in the
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The plane was designed in 1929 by Stanisław Cywiński in
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410:"PWS - Podlaska Wytwórnia Samolotów : PWS-50"
123:international touring aircraft contest (along with
213:Single-engine mixed construction braced low-wing
186:It crashed during the 4th Winter Air Contest of
135:). The plane was built with a financial help of
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155:international contest in July 1930, flown by
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361:1,000 m (3,300 ft) in 10 minutes
445:Polskie konstrukcje lotnicze 1893-1939" (
33:PWS-51 (SP-ADC, on the right) during the
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447:Polish aviation constructions 1893-1939
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343:700 km (430 mi, 380 nmi)
325:155 km/h (96 mph, 84 kn)
163:on July 28, due to an oil pipe damage.
337:70 km/h (43 mph, 38 kn)
15:
376:0.0830 kW/kg (0.0505 hp/lb)
367:40 kg/m (8.2 lb/sq ft)
7:
396:Jane's all the World's Aircraft 1931
224:5-cylinder air-cooled radial engine
416:(in Polish). Warsaw. Archived from
499:Podlaska Wytwórnia Samolotów (PWS)
463:Photos and drawings at Ugolok Neba
270:10.8 m (35 ft 5 in)
107:(PWS), that remained a prototype.
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264:7.7 m (25 ft 3 in)
276:2.2 m (7 ft 3 in)
24:
723:Single-engined tractor aircraft
282:18 m (190 sq ft)
355:2.2 m/s (430 ft/min)
310:2-bladed fixed-pitch propeller
1:
733:Aircraft first flown in 1930
349:2,700 m (8,900 ft)
117:Podlaska Wytwórnia Samolotów
104:Podlaska Wytwórnia Samolotów
713:1930s Polish sport aircraft
294:720 kg (1,587 lb)
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288:440 kg (970 lb)
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394:Grey, C.G., ed. (1931).
302:Armstrong Siddeley Genet
226:Armstrong Siddeley Genet
443:Glass, Andrzej (1977).
249:General characteristics
205:
111:Design and development
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221:, with a rear skid.
147:Operational history
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201:PWS-51 during the
728:Low-wing aircraft
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359:Time to altitude:
175:aircraft) with a
157:Józef Lewoniewski
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347:Service ceiling:
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46:Type of aircraft
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451:. Warsaw: WKiŁ.
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437:Further reading
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420:on 17 May 2003
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353:Rate of climb:
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237:Specifications
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203:Challenge 1930
153:Challenge 1930
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141:Biała Podlaska
121:Challenge 1930
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718:PWS aircraft
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422:. Retrieved
418:the original
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335:Stall speed:
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219:landing gear
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177:Townend ring
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87:Number built
44:Sports plane
316:Performance
308:Propellers:
298:Powerplant:
230:Walter Vega
209:Description
183:aircraft).
169:Walter Vega
707:Categories
665:Avia BH-33
381:References
372:Power/mass
280:Wing area:
81:prototype
268:Wingspan:
242:Data from
215:monoplane
171:NZ (from
667:as PWS-A
507:Aircraft
501:aircraft
192:Podlasie
70:Retired
692:PWS-103
687:PWS-102
682:PWS-101
675:Gliders
274:Height:
262:Length:
78:Status
19:PWS-51
649:PWS-54
644:PWS-52
639:PWS-51
634:PWS-50
629:PWS-40
624:PWS-35
619:PWS-33
614:PWS-26
609:PWS-24
604:PWS-23
599:PWS-22
594:PWS-21
589:PWS-20
584:PWS-19
579:PWS-18
574:PWS-16
569:PWS-15
564:PWS-14
559:PWS-12
554:PWS-11
549:PWS-10
424:21 May
341:Range:
188:Lublin
181:PWS-50
161:Vienna
129:PWS-52
125:PWS-50
99:PWS-51
544:PWS-8
539:PWS-7
534:PWS-6
529:PWS-5
524:PWS-4
519:PWS 3
514:PWS-1
414:Poser
256:Crew:
173:PWS-8
133:PWS-8
73:1934
65:1930
41:Role
426:2019
300:1 ×
190:and
137:LOPP
131:and
97:The
56:PWS
709::
412:.
127:,
91:1
491:e
484:t
477:v
449:)
428:.
374::
258:2
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