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Drzewiecki JD-2

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215: 26: 179:. Flown by Kazimierz Kalina, it won in the 1st Polish Light Aircraft Contest in October 1929, and flown by Worledge it took the 7th place in the 2nd Contest the following year. In 1929 it was bought by a private owner Pawłowski, who crashed it that year. Next it was repaired and bought by Captain 147:
The prototype, with a workshop number SL-4, was built in 1926 and first flown on October 5, 1926 in Warsaw. During landing, a fuel pipe broke and the aircraft burned, injuring the military pilot Kazimierz Kalina. The pilot, however, expressed a good opinion on its handling, so the second modified
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was rectangular in cross-section, plywood-covered. In the JD-2bis, the fuselage was aluminium covered in an engine section. Wings were two-piece, rectangular with straight tips, two-spar, covered with canvas and plywood (in front section), supported with twin struts. Conventional
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The Ministry of Communication planned to build 10 aircraft for regional aero clubs, also Poznań and Cracov Aero Clubs planned to order JD-2bis, but these planes were not realized. JD-2bis was a difficult to fly machine, with low stability, it was however liked by some pilots.
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paramilitary organization. It had changed fuselage front, wing tips and a tail fin (SL-14 and 15, registration numbers: SP-ACD and ACF). In 1930 there was built one more JD-2bis (SL-20, SP-ADP). It was later fitted with a stronger radial engine 80 hp
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Academic Aero Club and it crashed on 18 August 1930 in Lwów, injuring a pilot M. Pakuła. The other one, SP-ACF, built for Warsaw Academic Aero Club, crashed on 16 March 1930, killing pilot K. Trzetrzewiński.
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The second prototype SL-6 was flown on June 26, 1927. Its handling was however not too good, it was also 90 kg heavier, than estimated. It was given a registration P-PSLA, from 1929: SP-ACA.
238:, with individual windshields and twin controls. A safety cage of steel pipes was above the front cockpit (JD-2) or before the front cockpit (JD-2bis). It had a fixed 183:, who used it for touring flying - by 1931 the plane visited 225 airfields, evident from inscriptions on its fuselage. The plane was written off in August 1935. 140:, around an available Anzani engine. It was the only plane of Drzewiecki's individual design and to carry JD designation, as he later worked as a member of the 199: 195: 249:
in front, air-cooled. Two-blade fixed wooden propeller Szomański. A fuel tank was in a fuselage front. Cruise fuel consumption 17 L/h.
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The last JD-2bis, SP-ADP, nicknamed "Adepcia" (a female name created from its registration letters), was built for the aviator
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flying it, took the 3rd place in the 3rd Polish Light Aircraft Contest. It was written off in August 1936.
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The JD-2 was the first aircraft constructed by the Aviation Section of the Mechanic Students' Club of the
141: 129: 495: 239: 475: 164: 327: 180: 8: 234:, covered with plywood (fins) and canvas (elevators and rudder). Two open cockpits in 116:. It was the first sports plane designed in Poland, that was built in a small series. 323: 176: 137: 133: 113: 58: 484: 246: 148:
aircraf(SL-6) t was bui6), and one more airframe for static trials (SL-5).
470: 214: 231: 222: 226: 242:, sprung with a rubber rope, with a common axle and a rear skid. 187: 409: 235: 25: 136:, hence a designation JD. The aircraft was designed in late 159: 154:
In 1929 two more aircraft of an improved variant, the
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were built for aero clubs, with a financial help of
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Aircraft of comparable role, configuration, and era
221:The JD-2 was a wooden construction low-wing braced 482: 225:, conventional in layout, with open cockpits. A 456:(in Polish). Warsaw: WKiŁ. pp. 281–283. 245:45 hp (34 kW) 6-cylinder Anzani 175:The second JD-2 (SP-ACA) was used by the 119: 447: 252: 213: 454:Polskie konstrukcje lotnicze 1893-1939 445: 443: 441: 439: 437: 435: 433: 431: 429: 427: 381:40.5 kg/m (8.3 lb/sq ft) 369:450 km (280 mi, 240 nmi) 357:116 km/h (72 mph, 63 kn) 351:130 km/h (81 mph, 70 kn) 483: 363:68 km/h (42 mph, 37 kn) 260:Polskie konstrukcje lotnicze 1893-1939 170: 451: 424: 132:design team). The main designer was 13: 292:9.7 m (31 ft 10 in) 286:5.95 m (19 ft 6 in) 14: 517: 464: 304:13.5 m (145 sq ft) 186:The JD-2bis SP-ACD was built for 471:Photo and drawing at Ugolok Neba 298:2.8 m (9 ft 2 in) 24: 501:Single-engined tractor aircraft 126:Warsaw University of Technology 48:Warsaw University of Technology 336:2-bladed fixed-pitch propeller 209: 1: 417: 280:1 / 211 kg (465 lb) 112:was a Polish sports plane of 506:Aircraft first flown in 1926 375:2,200 m (7,200 ft) 198:. In September–October 1930 7: 491:1920s Polish sport aircraft 398: 316:546 kg (1,204 lb) 10: 522: 330:, 34 kW (45 hp) 310:335 kg (739 lb) 240:conventional landing gear 23: 18: 394:130 m (427 ft) 165:Armstrong Siddeley Genet 452:Glass, Andrzej (1977). 388:80 m (262 ft) 265:General characteristics 218: 120:Design and development 253:Specifications (JD-2) 217: 128:(later a home of the 328:radial piston engine 171:Operational history 219: 89:Primary user 496:Low-wing aircraft 181:Zbigniew Babiński 106: 105: 513: 458: 457: 449: 373:Service ceiling: 344: 267: 177:Warsaw Aero Club 134:Jerzy Drzewiecki 99: 68:October 5, 1926 59:Jerzy Drzewiecki 38:Type of aircraft 28: 16: 15: 521: 520: 516: 515: 514: 512: 511: 510: 481: 480: 467: 462: 461: 450: 425: 420: 401: 382: 340: 263: 255: 212: 200:Ignacy Giedgowd 173: 122: 97: 39: 12: 11: 5: 519: 509: 508: 503: 498: 493: 479: 478: 473: 466: 465:External links 463: 460: 459: 422: 421: 419: 416: 413: 412: 400: 397: 396: 395: 389: 383: 376: 370: 364: 358: 352: 349:Maximum speed: 338: 337: 331: 317: 311: 305: 299: 293: 287: 281: 275: 254: 251: 211: 208: 196:Witold Rychter 172: 169: 121: 118: 104: 103: 100: 94: 93: 90: 86: 85: 82: 78: 77: 74: 70: 69: 66: 62: 61: 56: 52: 51: 45: 41: 40: 37: 34: 30: 29: 21: 20: 9: 6: 4: 3: 2: 518: 507: 504: 502: 499: 497: 494: 492: 489: 488: 486: 477: 476:Model's photo 474: 472: 469: 468: 455: 448: 446: 444: 442: 440: 438: 436: 434: 432: 430: 428: 423: 415: 411: 408: 407: 406: 405: 393: 390: 387: 386:Take-off run: 384: 380: 379:Wing loading: 377: 374: 371: 368: 365: 362: 359: 356: 355:Cruise speed: 353: 350: 347: 346: 345: 343: 335: 332: 329: 325: 321: 318: 315: 314:Gross weight: 312: 309: 308:Empty weight: 306: 303: 300: 297: 294: 291: 288: 285: 282: 279: 276: 273: 270: 269: 268: 266: 261: 259: 250: 248: 247:radial engine 243: 241: 237: 233: 228: 224: 216: 207: 203: 201: 197: 192: 189: 184: 182: 178: 168: 166: 161: 157: 152: 149: 145: 143: 139: 135: 131: 127: 117: 115: 111: 101: 96: 95: 91: 88: 87: 83: 80: 79: 75: 73:Introduction 72: 71: 67: 65:First flight 64: 63: 60: 57: 54: 53: 49: 46: 44:Manufacturer 43: 42: 35: 32: 31: 27: 22: 17: 453: 414: 403: 402: 392:Landing run: 391: 385: 378: 372: 366: 361:Stall speed: 360: 354: 348: 341: 339: 333: 319: 313: 307: 301: 295: 289: 283: 277: 271: 264: 262: 257: 256: 244: 220: 204: 193: 185: 174: 155: 153: 150: 146: 123: 109: 107: 98:Number built 36:Sports plane 342:Performance 334:Propellers: 326:6-cylinder 320:Powerplant: 210:Description 485:Categories 418:References 302:Wing area: 50:workshops 290:Wingspan: 278:Capacity: 258:Data from 232:empennage 223:monoplane 55:Designer 399:See also 227:fuselage 81:Retired 296:Height: 284:Length: 156:JD-2bis 92:Poland 410:PWS-51 367:Range: 324:Anzani 236:tandem 144:team. 272:Crew: 84:1936 76:1927 33:Role 19:JD-2 322:1 × 188:Lwów 160:LOPP 138:1925 114:1926 110:JD-2 108:The 142:RWD 130:RWD 487:: 426:^ 167:. 102:5 274:1

Index


Warsaw University of Technology
Jerzy Drzewiecki
1926
Warsaw University of Technology
RWD
Jerzy Drzewiecki
1925
RWD
LOPP
Armstrong Siddeley Genet
Warsaw Aero Club
Zbigniew Babiński
Lwów
Witold Rychter
Ignacy Giedgowd

monoplane
fuselage
empennage
tandem
conventional landing gear
radial engine
Anzani
radial piston engine
PWS-51



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