Knowledge (XXG)

LWD Zuch

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and carried markings SP-BAG. Because of increased drag, maximum speed was lower - 222 km/h comparing to 244 km/h of Zuch-1. Because there were several Sh 14 engines available, left in the country by retreating Germans, the LWD next built a short series of 5 Zuch-2s in 1950. They carried
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inline engine in a long, slant nose. The prototype flew first on September 1, 1948. The design was quite successful and fit to aerobatics, but it did not enter production because of decision not to produce Walter Minor engines in Poland. The prototype served in aero clubs from 1950 until end of
243:, conventional in layout. Fuselage of a steel frame, covered with canvas, in front with metal sheet. Two-spar wings of wooden construction and trapezoid shape, canvas and plywood covered, fitted with split 648: 46: 33: 653: 576: 585: 215: 194: 101: 534: 658: 569: 38: 75: 263:(118 kW / 160 hp) with a ring cover with individual cowls for cylinders. Two-blade wooden propeller. 367: 353: 339: 96: 643: 562: 554: 255:
with a tail wheel, main gear in massive covers. Engine in front: Zuch-1: 6-cylinder inline engine
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markings SP-BAL - SP-BAP and served in aero clubs until 1955, except SP-BAM, which served until
223:. The design was similar to Junak-1, the main difference was en engine. Unlike Junak, its fixed 530: 220: 617: 296: 291: 276: 210: 190: 186: 158: 140: 323: 248: 244: 228: 231:
and had slightly enlarged rudder (similar improvements were later adapted in Junak-2).
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The aircraft was a development of a military and civilian trainer plane
227:, in massive covers, was lacking struts. It was also fitted with split 433:
7-cylinder air-cooled radial piston engine, 120 kW (160 hp)
316: 558: 529:, Typy Broni i Uzbrojenia #110, Wydawnictwo MON, Warsaw 1986, 259:(118 kW / 160 hp), Zuch-2: 7-cylinder radial engine 247:. Cockpit with two seats in tandem, under a multi-part closed 18: 219:(LWD - Aircraft Experimental Workshops), a main designer was 209:, meant as a civilian aerobatics and trainer plane for the 506:
Aircraft of comparable role, configuration, and era
164: 154: 146: 136: 128: 123: 115: 107: 95: 87: 82: 68: 570: 239:Mixed construction (steel and wood) low-wing 8: 270:was powered by the Czechoslovak 160 hp 577: 563: 555: 65: 466:1,160 km (720 mi, 630 nmi) 454:222 km/h (138 mph, 120 kn) 484:58.3 kg/m (11.9 lb/sq ft) 460:181 km/h (112 mph, 98 kn) 49:of all important aspects of the article. 197:bureau and produced in a small series. 586:Lotnicze Warsztaty Doświadczalne (LWD) 45:Please consider expanding the lead to 7: 649:1940s Polish civil trainer aircraft 405:7.61 m (25 ft 0 in) 14: 423:17.5 m (188 sq ft) 417:2.1 m (6 ft 11 in) 411:10 m (32 ft 10 in) 527:Samolot szkolno-treningowy Junak 309: 286:was fitted with a radial engine 216:Lotnicze Warsztaty Doświadczalne 102:Lotnicze Warsztaty Doświadczalne 74: 23: 654:Single-engined tractor aircraft 478:36 m/s (7,100 ft/min) 37:may be too short to adequately 374:(incomplete and disassembled). 47:provide an accessible overview 1: 472:4,750 m (15,580 ft) 346:(damaged and disassembled). 290:. It was flown on April 1, 91:Trainer/aerobatics aircraft 16:1940s Polish light aircraft 675: 550:Photos at Ugolok Neba site 593: 213:. It was designed in the 73: 279:, with markings SP-BAD. 390:General characteristics 379:Specifications (Zuch 2) 368:Polish Aviation Museum 354:Polish Aviation Museum 340:Polish Aviation Museum 201:Design and development 282:The second prototype 251:. Conventional fixed 525:Kempski, Benedykt, 494:Related development 83:General information 439:2-bladed propeller 272:Walter Minor 6-III 266:The first variant 257:Walter Minor 6-III 659:Low-wing aircraft 631: 630: 366:Preserved in the 352:Preserved in the 338:Preserved in the 175: 174: 137:Introduction date 64: 63: 666: 579: 572: 565: 556: 539: 512:Zlin Z-26 Trener 470:Service ceiling: 447: 392: 315: 313: 312: 211:Polish Aero Club 187:trainer aircraft 150:1 September 1948 78: 66: 59: 56: 50: 27: 19: 674: 673: 669: 668: 667: 665: 664: 663: 634: 633: 632: 627: 589: 583: 546: 537: 522: 491: 443: 388: 381: 363:Zuch-2 (SP-BAO) 360:(disassembled). 349:Zuch-2 (SP-BAM) 335:Zuch-1 (SP-BAD) 332: 324:Aeroklub Polski 310: 308: 305: 237: 203: 60: 54: 51: 44: 32:This article's 28: 17: 12: 11: 5: 672: 670: 662: 661: 656: 651: 646: 636: 635: 629: 628: 626: 625: 620: 615: 610: 605: 600: 594: 591: 590: 584: 582: 581: 574: 567: 559: 553: 552: 545: 544:External links 542: 541: 540: 521: 518: 515: 514: 503: 502: 490: 487: 486: 485: 479: 476:Rate of climb: 473: 467: 461: 455: 452:Maximum speed: 441: 440: 434: 424: 418: 412: 406: 400: 380: 377: 376: 375: 364: 361: 350: 347: 336: 331: 328: 327: 326: 320: 319: 304: 301: 236: 233: 221:Tadeusz Sołtyk 202: 199: 173: 172: 166: 165:Developed from 162: 161: 156: 152: 151: 148: 144: 143: 138: 134: 133: 130: 126: 125: 121: 120: 117: 113: 112: 109: 105: 104: 99: 93: 92: 89: 85: 84: 80: 79: 71: 70: 62: 61: 41:the key points 31: 29: 22: 15: 13: 10: 9: 6: 4: 3: 2: 671: 660: 657: 655: 652: 650: 647: 645: 642: 641: 639: 624: 621: 619: 616: 614: 611: 609: 606: 604: 601: 599: 596: 595: 592: 587: 580: 575: 573: 568: 566: 561: 560: 557: 551: 548: 547: 543: 536: 535:83-11-07341-4 532: 528: 524: 523: 519: 517: 513: 510: 509: 508: 507: 501: 498: 497: 496: 495: 488: 483: 482:Wing loading: 480: 477: 474: 471: 468: 465: 462: 459: 458:Cruise speed: 456: 453: 450: 449: 448: 446: 438: 435: 432: 428: 425: 422: 419: 416: 413: 410: 407: 404: 401: 398: 395: 394: 393: 391: 386: 385: 378: 373: 369: 365: 362: 359: 355: 351: 348: 345: 341: 337: 334: 333: 329: 325: 322: 321: 318: 307: 306: 302: 300: 298: 293: 289: 285: 280: 278: 273: 269: 264: 262: 258: 254: 250: 246: 242: 234: 232: 230: 226: 222: 218: 217: 212: 208: 200: 198: 196: 192: 188: 184: 181:was a Polish 180: 170: 167: 163: 160: 157: 153: 149: 145: 142: 139: 135: 131: 127: 122: 118: 114: 110: 106: 103: 100: 98: 94: 90: 86: 81: 77: 72: 67: 58: 48: 42: 40: 35: 30: 26: 21: 20: 644:LWD aircraft 612: 526: 516: 505: 504: 493: 492: 481: 475: 469: 463: 457: 451: 444: 442: 436: 426: 420: 414: 408: 402: 396: 389: 387: 383: 382: 283: 281: 267: 265: 253:landing gear 238: 225:landing gear 214: 204: 178: 176: 147:First flight 129:Manufactured 116:Number built 108:Primary user 97:Manufacturer 52: 36: 34:lead section 538:(in Polish) 445:Performance 437:Propellers: 431:Bramo Sh 14 427:Powerplant: 288:Bramo Sh 14 261:Bramo Sh 14 235:Description 207:LWD Junak-1 189:, built in 638:Categories 520:References 421:Wing area: 183:aerobatics 500:LWD Junak 409:Wingspan: 384:Data from 330:Survivors 303:Operators 241:monoplane 169:LWD Junak 132:1948-1950 55:July 2024 39:summarize 588:aircraft 489:See also 69:LWD Zuch 415:Height: 403:Length: 193:in the 155:Retired 124:History 533:  464:Range: 372:Kraków 358:Kraków 344:Kraków 317:Poland 314:  284:Zuch-2 268:Zuch-1 249:canopy 111:Poland 623:Żuraw 608:Junak 598:Szpak 397:Crew: 245:flaps 229:flaps 613:Zuch 531:ISBN 429:1 × 297:1963 292:1949 277:1955 191:1948 185:and 179:Zuch 177:The 159:1963 141:1949 88:Type 618:Miś 603:Żak 370:in 356:in 342:in 195:LWD 640:: 299:. 171:-1 578:e 571:t 564:v 399:2 119:7 57:) 53:( 43:.

Index


lead section
summarize
provide an accessible overview

Manufacturer
Lotnicze Warsztaty Doświadczalne
1949
1963
LWD Junak
aerobatics
trainer aircraft
1948
LWD
LWD Junak-1
Polish Aero Club
Lotnicze Warsztaty Doświadczalne
Tadeusz Sołtyk
landing gear
flaps
monoplane
flaps
canopy
landing gear
Walter Minor 6-III
Bramo Sh 14
Walter Minor 6-III
1955
Bramo Sh 14
1949

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