26:
161:, conventional in layout, with a fixed landing gear and a closed cockpit. Steel framed fuselage, covered with canvas on a wooden frame, aluminum in front engine section. Three-part trapezoid wings with rounded tips, of wooden construction, two-spar, plywood (in front) and canvas covered, fitted with split
192:(registration SP-BPD). In winter it was evaluated by the Aviation Technical Institute in Poland. It was rather difficult to fly. There were no plans of serial production. The plan of beating a record was abandoned, because the German
169:, plywood (fins) and canvas (elevators and rudder) covered. Two seats in tandem, under a canopy, with a fixed panoramic windshield and small side windows. Behind the cockpit was a place for a baggage. Conventional fixed
180:
in front, driving a two-blade tractor wooden propeller SzomaĆski of a fixed pitch. Fuel tanks 180 L in mid-wing section. Cruise fuel consumption 28 L/h.
145:
designed the wing. The aircraft was designed specially in order to beat world records of distance in light aircraft category, under influence of French
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had made it in the meantime. The sole aircraft was probably destroyed during air raids on the DWL factory after the outbreak of World War II.
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4-cylinder inverted air-cooled in-line piston engine, 97 kW (130 hp)
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382:
Biographical
Dictionary of Polish Technicians : Tadeusz ChyliĆski
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Polish aircraft 1893-1939, Polskie konstrukcje lotnicze 1893â1939
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with a rear wheel, the main gear was in covers. 4-cylinder
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258 km/h (160 mph, 139 kn) at sea level
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180 L (48 US gal; 40 imp gal)
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28 L/h (7.4 gal/h; 6.2 imp gal/h)
353:
Aircraft of comparable role, configuration, and era
188:The prototype was built and first flown in October
396:
113:was a Polish two-seat low-wing sports aircraft of
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472:
432:(in Polish). Warsaw: WKiĆ. pp. 327â328.
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479:
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318:217 km/h (135 mph, 117 kn)
331:1,300 km (810 mi, 700 nmi)
297:2-bladed SzomaĆski fixed-pitch propeller
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157:Mixed construction low-wing cantilever
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430:Polskie konstrukcje lotnicze 1893â1939
325:72 km/h (45 mph; 39 kn)
183:
460:
427:
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165:and slats. Conventional cantilever
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447:Photos and drawings at Ugolok Neba
227:9.7 m (31 ft 10 in)
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221:7.4 m (24 ft 3 in)
133:was designed in 1937-1938 in the
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24:
646:Single-engined tractor aircraft
233:12 m (130 sq ft)
137:bureau. The chief designer was
343:4.6 m/s (910 ft/min)
152:
124:
1:
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337:5,000 m (16,000 ft)
651:Aircraft first flown in 1938
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631:1930s Polish sport aircraft
384:. Warsaw: SBTP. p. 24.
347:
245:900 kg (1,984 lb)
239:580 kg (1,279 lb)
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266:de Havilland Gipsy Major I
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399:Polish aircraft 1893-1939
32:
23:
18:
200:Specifications ( RWD 19)
178:de Havilland Gipsy Major
428:Glass, Andrzej (1977).
380:Glass, Andrzej (2003).
212:General characteristics
395:Cynk, Jerzy B (1971).
117:, constructed by the
403:. Putnam. pp.
184:Operational history
641:Low-wing aircraft
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256:Fuel consumption:
149:sports aircraft.
143:Tadeusz ChyliĆski
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73:Tadeusz ChyliĆski
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139:Jerzy Drzewiecki
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43:Type of aircraft
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99:Number built
359:Arado Ar 79
303:Performance
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262:Powerplant:
194:Arado Ar 79
153:Description
141:. Designer
125:Development
625:Categories
367:References
231:Wing area:
93:prototype
225:Wingspan:
205:Data from
167:empennage
159:monoplane
69:Designer
490:aircraft
348:See also
121:bureau.
82:October
405:567-569
219:Length:
147:Caudron
90:Status
54:Poland
19:RWD-19
610:RWD 25
605:RWD 23
600:RWD 22
595:RWD 21
590:RWD 20
585:RWD 19
580:RWD 18
575:RWD 17
570:RWD 16
565:RWD 15
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550:RWD 11
545:RWD 10
452:RWD-19
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329:Range:
131:RWD-19
111:RWD-19
540:RWD 9
535:RWD 8
530:RWD 7
525:RWD 6
520:RWD 5
515:RWD 4
510:RWD 3
505:RWD 2
500:RWD 1
163:flaps
38:Role
409:ISBN
264:1 Ă
190:1938
129:The
115:1938
109:The
84:1938
488:RWD
280:or
135:RWD
119:RWD
63:DWL
627::
407:.
103:1
480:e
473:t
466:v
417:.
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