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LAK-17

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is a combination of the LAP92-130/15, at its roots, and the LAP-92-150/15, at its tips. The LAK-17 holds water ballast in tanks in the wing and fin. The LAK-17A was certified in November 1994 by the Lithuanian Civil Aviation Authority. A new variant with an improved wing was designated the LAK-17B.
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engine variant was developed for the LAK-17 by Slovenian engineers at LZ Design. It originally had a 0.9 metre propeller, and the latest versions have a 1.0 metre propeller in the nose driven by an electric motor.
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All variants have a 15.00 m (49.21 ft) wingspan but a wing with span increased to 18.00 m (59.06 ft) is available as an option; powered self-sustaining versions are also produced.
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Improved variant with aerodynamic changes as well as a raised undercarriage to provide increased ground clearance for the folding propeller and increased battery capacity for self launching.
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The LAK-17 is designed to meet the requirements of the utility category of JAR-22. It is a single-seat mid-wing
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EASA Type Certificatie and data Sheet of the LAK-17 (PDF- all variants)
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and flaps, it has a retractable single-wheel main landing gear and has
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EASA.A.083 page for the Sportine Aviacija - LAK-17 (all variants)
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European Aviation Safety Agency Type Certificate Data Sheet A.083
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Powered self-sustaining sailplane variant of the LAK-17B with a
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Powered self-sustaining sailplane variant of the LAK-17A with a
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Improved variant with new wing profile and modified geometry.
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two-cylinder air-cooled two-stroke retractable engine.
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Production flapped 15- or 18-metre wingspan sailplane.
453: 1012: 408: 208:Specifications (LAK-17A with 15 metre wingspan) 90:single-seat sailplane that was designed at the 649: 476: 500:Litovskaya Aviatsionnaya Konstruktsiy (LAK) 656: 642: 483: 469: 419: 197:A LAK-17B with a front electric sustainer. 175:A LAK-17A with a front electric sustainer. 294:275 km/h (171 mph, 149 kn) 109: 399: 397: 371: 369: 367: 365: 363: 351: 349: 113: 1013: 330: 328: 326: 324: 322: 320: 637: 464: 430: 394: 385: 383: 360: 346: 317: 246:15.00 m (49 ft 2 in) 100:Lietuviškos aviacinÄ—s konstrukcijos 13: 380: 240:6.53 m (21 ft 5 in) 14: 1042: 445: 252:1.29 m (4 ft 3 in) 126:of composite construction with a 258:9.06 m (97 sq ft) 102:or LAK), and is manufactured by 24: 306:0.53 m/s (104 ft/min) 134:on the upper wing surface. The 1: 310: 234:188 kg (414 lb) water ballast 118:LAK-17bt fuselage and engine 7: 1021:1990s Lithuanian sailplanes 668:aircraft designation system 279:500 kg (1,102 lb) 150: 10: 1047: 947: 876: 815: 675: 511: 273:245 kg (540 lb) 23: 18: 390:Front Electric Sustainer 144:front electric sustainer 219:General characteristics 119: 110:Design and development 99: 117: 76:In production (2015) 665:Italian Armed Forces 298:Maximum glide ratio: 92:Lithuanian Aero Club 191:retractable engine. 340:2011-07-28 at the 120: 1026:Electric aircraft 1008: 1007: 631: 630: 504:Sportine Aviacija 104:SportinÄ— Aviacija 80: 79: 67:SportinÄ— Aviacija 1038: 658: 651: 644: 635: 634: 485: 478: 471: 462: 461: 457: 456: 454:Official website 439: 434: 428: 423: 417: 412: 406: 401: 392: 387: 378: 373: 358: 353: 344: 332: 287: 221: 53: 45:Type of aircraft 28: 16: 15: 1046: 1045: 1041: 1040: 1039: 1037: 1036: 1035: 1011: 1010: 1009: 1004: 943: 872: 811: 671: 662: 632: 627: 507: 489: 452: 451: 448: 443: 442: 435: 431: 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249: 243: 237: 231: 225: 218: 216: 212: 211: 142:An optional 141: 121: 83: 81: 437:LAK-17C FES 285:Performance 200:LAK-17C FES 194:LAK-17B FES 172:LAK-17A FES 1015:Categories 404:LAK-17 FES 311:References 256:Wing area: 96:Lithuanian 88:Lithuanian 787:C-42/P-42 623:Genesis 2 244:Wingspan: 232:Capacity: 213:Data from 189:Solo 2350 167:Solo 2350 132:airbrakes 124:sailplane 57:Lithuania 43:sailplane 948:401–2006 573:LAK-12DR 506:aircraft 338:Archived 184:LAK-17BT 162:LAK-17AT 151:Variants 980:KC-767B 975:KC-767A 877:201–400 816:101–200 578:LAK-12E 528:LAK T-4 376:LAK-17B 356:LAK-17A 250:Height: 238:Length: 178:LAK-17B 156:LAK-17A 136:airfoil 73:Status 19:LAK-17 1000:T-2006 995:F-2000 990:P-1150 970:KC-707 613:LAK-20 608:LAK-19 603:LAK-17 598:LAK-16 593:LAK-15 588:LAK-14 583:LAK-13 568:LAK-12 563:LAK-11 558:LAK-10 553:LAK-9M 128:T-tail 84:LAK-17 985:C-900 965:E-550 960:H-500 955:H-412 939:T-346 934:T-345 929:T-339 924:C-319 919:T-260 914:H-249 909:C-228 904:C-222 899:H-212 894:U-208 889:H-206 884:H-205 868:A-200 863:C-180 858:H-169 853:U-166 848:H-139 843:C-130 838:H-129 833:H-109 828:G-103 823:H-101 676:1–100 618:SL-2P 548:LAK-9 543:LAK-8 538:LAK-6 533:LAK-5 523:LAK-2 267:24.63 226:Crew: 86:is a 33:Role 807:H-90 802:P-72 797:C-50 792:H-47 782:F-35 777:Q-27 772:C-27 767:Q-26 762:Q-25 757:Q-24 752:G-21 747:G-17 742:F-16 737:Q-12 732:Q-11 727:A-11 722:Q-10 712:AV-8 697:H-3F 693:H-3D 516:BK-7 502:and 496:EZSA 492:ESAG 82:The 39:and 717:Q-9 707:Q-7 702:G-4 688:G-2 683:Q-1 228:one 1017:: 498:, 494:, 396:^ 382:^ 362:^ 348:^ 319:^ 300:45 106:. 98:: 695:/ 657:e 650:t 643:v 484:e 477:t 470:v 265:: 94:(

Index


15 metre-class
18 metre-class
Lithuania
SportinÄ— Aviacija
Lithuanian
Lithuanian Aero Club
Lithuanian
SportinÄ— Aviacija

sailplane
T-tail
airbrakes
airfoil
front electric sustainer
Solo 2350
Solo 2350
Aspect ratio






European Aviation Safety Agency Type Certificate Data Sheet A.083
Archived
Wayback Machine


LAK-17A

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