Knowledge (XXG)

HKS 700E

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WARNING! This is a non-certified aircraft engine, the possibility of engine failure exists at all times. Do not operate this engine over densely populated areas. Do not operate this engine over terrain where a safe, power off landing cannot be performed. The operating and maintenance instructions
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version with a 62.5 mm (2.5 in) stroke and a compression ratio of 8.8:1, that produces 80 hp (60 kW) at 5300 rpm for three minutes for take-off and 77 hp (57 kW) at 4900 rpm continuously. The engine's dry weight is 57.5 kg (127 lb) equipped with electrical
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Coupe (facelift)HKS 700E engines from serial number 101105 and above meet ASTM standard 2339-05, which governs the design and manufacture of reciprocating engines for light-sport aircraft. Compliance with the ASTM standard means the aircraft is applicable for use on special or experimental
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The reduction drive is a choice of two integral gearboxes: the A-type gearbox has a 2.58:1 ratio and can accommodate propellers of up to 4,000 kg/cm2 inertial load; the B-type gearbox has a 3.47:1 ratio and can accommodate propellers of up to 6,000 kg/cm2.
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Producing 60 hp (45 kW) at 6,200 rpm for three minutes for take-off and 56 hp (42 kW) at 5,800 rpm continuously, the 700E was designed as a fuel efficient four stroke alternative to the high fuel consumption two stroke engines, such as the
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system, electric starter, fuel injectors, gearbox, exhaust system and turbocharger. The initial time between overhauls is recommended as 500 hours, but this is expected to rise with operational experience.
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supplied with this engine must be followed at all times. Flying any aircraft involves the risk of injury or death, building and maintaining your own aircraft requires great personal responsibility.
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Initial version, normally aspirated and producing 60 hp (45 kW) at 6200 rpm for three minutes for take-off and 56 hp (42 kW) at 5800 rpm continuously.
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A-type gearbox with 2.58:1 ratio, limit of 4,000kg/cm2 inertial load. The B-type gearbox with 3.47:1 ratio, limit of 6,000kg/cm2 inertial load
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55 kg (121 lb) equipped with electrical system, electric starter, carburetors, gearbox, exhaust system, oil tank and cooler
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60 hp (45 kW) at 6200 rpm for three minutes for take-off and 56 hp (42 kW) at 5800 rpm continuous
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The 700E burns 9 L (2.4 US gal) per hour in cruise flight at 4,750 rpm. The recommended
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engine has four valves per cylinder, and nickel-ceramic coated cylinder bores. Lubrication is
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is 1000 hours, although this is expected to be increased as experience is gained.
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8th Edition, page G-9 Cybair Limited Publishing, 2001.
583:free air cylinders, with oil-cooled cylinder heads 125:company noted for its automotive racing engines. 222:The company's owner's manual disclaimer states: 224: 560:two intake and two exhaust valves per cylinder 8: 144:and electric start. The engine is mainly 750: 748: 746: 744: 742: 740: 738: 736: 508:Two cylinder, four-stroke aircraft engine 672: 670: 668: 666: 664: 662: 658: 219:light-sport aircraft (S-LSA or E-LSA). 718: 26: 105:aircraft engine, designed for use on 7: 678:Ultralight Aircraft Shopper's Guide 797:"HKS 700T four stroke turbo power" 25: 191: 182: 117:. The engine is manufactured by 35: 397:Green Sky Adventures Micro Mong 782:Compliance Statement July,2006 1: 870:2000s aircraft piston engines 362:Excalibur Aircraft Excalibur 297:Aviation Products Star Trike 138:capacitor discharge ignition 307:BB Microlight BB-two seater 272:Aéro Services Guépard Guépe 886: 477:TechProAviation Merlin 100 822:"HKS 700T Specifications" 760:"HKS 700E Specifications" 43: 34: 29: 526:60 mm (2.4 in) 517:85 mm (3.3 in) 342:Club ULM Rotor Ptenets-2 500:General characteristics 437:RagWing RW22 Tiger Moth 402:Hy-Tek Hurricane Hauler 447:SlipStream Ultra Sport 357:Earthstar Thunder Gull 229: 173:time between overhauls 44:HKS 700E mounted on a 855:Distributor's website 489:Specifications (700E) 382:Flying Machines FM301 725:: CS1 maint: year ( 535:680 cc (41.49 cu in) 427:Quad City Challenger 392:Garland Vampire GA-3 387:Harmening High Flyer 277:Air Creation Skypper 152:cylinder heads. The 95:horizontally opposed 93:is a twin-cylinder, 467:Summit Steel Breeze 422:Phoenix Air Phoenix 417:North Wing Sport X2 377:Flying K Sky Raider 322:ASAP Chinook Plus 2 267:Aeros del Sur Manta 107:ultralight aircraft 567:unleaded auto fuel 457:Sport Flight Talon 452:Solo Wings Aquilla 111:powered parachutes 610:Compression ratio 472:Sundog Two-Seater 442:Rainbow Aerotrike 432:Quicksilver GT400 367:Fletcher Hercules 317:Bede BD-17 Nugget 282:Air Creation Trek 262:Aeroalcool Quasar 203:Rans S-12 Airaile 133:The HKS 700E has 115:ultralight trikes 87: 86: 16:(Redirected from 877: 851: 850: 848:Official website 833: 832: 830: 828: 818:HKS Aviation Co. 814: 808: 807: 805: 803: 793:HKS Aviation Co. 789: 783: 777: 771: 770: 768: 766: 752: 731: 730: 724: 716: 714: 713: 704:. Archived from 694: 688: 674: 574:dry sump with a 496:Cliche & HKS 327:Capella T-Raptor 195: 186: 68: 39: 27: 21: 885: 884: 880: 879: 878: 876: 875: 874: 860: 859: 846: 845: 842: 837: 836: 826: 824: 816: 815: 811: 801: 799: 791: 790: 786: 778: 774: 764: 762: 754: 753: 734: 717: 711: 709: 696: 695: 691: 676:Cliche, Andre: 675: 660: 655: 621: 599: 581:Cooling system: 551: 502: 491: 486: 412:Murphy Maverick 257: 234: 208: 207: 206: 205: 198: 197: 196: 188: 187: 131: 67:National origin 66: 60:aircraft engine 23: 22: 15: 12: 11: 5: 883: 881: 873: 872: 862: 861: 858: 857: 852: 841: 840:External links 838: 835: 834: 809: 784: 772: 732: 702:"HKS Aviation" 689: 657: 656: 654: 651: 648: 647: 645:ULPower UL260i 642: 637: 635:Pegasus PAL 95 632: 627: 620: 617: 616: 615: 606: 598: 595: 594: 593: 588:Reduction gear 584: 578: 569: 561: 550: 547: 546: 545: 536: 527: 518: 509: 501: 498: 490: 487: 485: 484: 479: 474: 469: 464: 459: 454: 449: 444: 439: 434: 429: 424: 419: 414: 409: 404: 399: 394: 389: 384: 379: 374: 369: 364: 359: 354: 349: 347:Cyclone AX2000 344: 339: 334: 329: 324: 319: 314: 309: 304: 299: 294: 289: 287:Airsport Sonet 284: 279: 274: 269: 264: 258: 256: 253: 252: 251: 244: 241: 238: 233: 230: 201:HKS 700E on a 200: 199: 190: 189: 181: 180: 179: 178: 177: 130: 127: 85: 84: 79: 75: 74: 69: 63: 62: 55:Twin cylinder 53: 49: 48: 41: 40: 32: 31: 24: 14: 13: 10: 9: 6: 4: 3: 2: 882: 871: 868: 867: 865: 856: 853: 849: 844: 843: 839: 823: 819: 813: 810: 798: 794: 788: 785: 781: 776: 773: 761: 757: 751: 749: 747: 745: 743: 741: 739: 737: 733: 728: 722: 708:on 1999-10-13 707: 703: 699: 693: 690: 687: 686:0-9680628-1-4 683: 679: 673: 671: 669: 667: 665: 663: 659: 652: 650: 646: 643: 641: 638: 636: 633: 631: 628: 626: 623: 622: 618: 613: 611: 607: 604: 603:Power output: 601: 600: 596: 591: 589: 585: 582: 579: 577: 576:trochoid pump 573: 570: 568: 565: 562: 559: 557: 553: 552: 548: 543: 541: 537: 534: 532: 528: 525: 523: 519: 516: 514: 510: 507: 504: 503: 499: 497: 495: 488: 483: 482:Titan Tornado 480: 478: 475: 473: 470: 468: 465: 463: 462:Stellar Astra 460: 458: 455: 453: 450: 448: 445: 443: 440: 438: 435: 433: 430: 428: 425: 423: 420: 418: 415: 413: 410: 408: 405: 403: 400: 398: 395: 393: 390: 388: 385: 383: 380: 378: 375: 373: 372:Flightstar II 370: 368: 365: 363: 360: 358: 355: 353: 350: 348: 345: 343: 340: 338: 335: 333: 330: 328: 325: 323: 320: 318: 315: 313: 310: 308: 305: 303: 300: 298: 295: 293: 292:Antares MA-33 290: 288: 285: 283: 280: 278: 275: 273: 270: 268: 265: 263: 260: 259: 254: 248: 245: 242: 239: 236: 235: 231: 228: 223: 220: 216: 214: 204: 194: 185: 176: 174: 169: 165: 163: 162:trochoid pump 159: 155: 151: 147: 143: 139: 136: 128: 126: 124: 120: 116: 112: 108: 104: 100: 96: 92: 83: 80: 78:Manufacturer 77: 76: 73: 70: 65: 64: 61: 58: 54: 51: 50: 47: 46:Flightstar II 42: 38: 33: 28: 19: 825:. 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Retrieved 706:the original 692: 677: 649: 608: 602: 586: 580: 571: 563: 554: 538: 531:Displacement 529: 520: 511: 505: 493: 492: 407:Murphy JDM-8 255:Applications 247:Turbocharged 225: 221: 217: 209: 170: 166: 132: 90: 88: 780:HKS Engines 765:27 February 625:Jabiru 2200 597:Performance 572:Oil system: 154:OHV pushrod 148:, but with 142:carburetors 129:Development 103:carburetted 99:four stroke 57:four-stroke 712:2009-12-25 653:References 564:Fuel type: 556:Valvetrain 549:Components 540:Dry weight 302:BAaer Guri 150:oil-cooled 146:air-cooled 827:3 January 802:3 January 640:Rotax 912 494:Data from 352:DTA Combo 312:Bede BD-6 213:Rotax 582 160:, with a 30:HKS 700E 864:Category 820:(2011). 795:(2011). 758:(2011). 721:cite web 700:(n.d.). 630:KFM 112M 619:See also 337:CGS Hawk 232:Variants 158:dry sump 123:Japanese 91:HKS 700E 140:, dual 18:HKS 700 684:  614:11.3:1 522:Stroke 332:CBB O2 506:Type: 72:Japan 52:Type 829:2012 804:2012 767:2014 727:link 682:ISBN 513:Bore 243:700T 237:700E 135:dual 121:, a 113:and 89:The 756:HKS 698:HKS 119:HKS 82:HKS 866:: 735:^ 723:}} 719:{{ 661:^ 215:. 164:. 109:, 101:, 97:, 831:. 806:. 769:. 729:) 715:. 612:: 590:: 558:: 542:: 533:: 524:: 515:: 20:)

Index

HKS 700

Flightstar II
four-stroke
aircraft engine
Japan
HKS
horizontally opposed
four stroke
carburetted
ultralight aircraft
powered parachutes
ultralight trikes
HKS
Japanese
dual
capacitor discharge ignition
carburetors
air-cooled
oil-cooled
OHV pushrod
dry sump
trochoid pump
time between overhauls


Rans S-12 Airaile
Rotax 582
Turbocharged
Aeroalcool Quasar

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