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.
572:free air cylinders, with oil-cooled cylinder heads 114:company noted for its automotive racing engines. 211:The company's owner's manual disclaimer states: 213: 549:two intake and two exhaust valves per cylinder 8: 133:and electric start. The engine is mainly 739: 737: 735: 733: 731: 729: 727: 725: 497:Two cylinder, four-stroke aircraft engine 661: 659: 657: 655: 653: 651: 647: 208:light-sport aircraft (S-LSA or E-LSA). 707: 15: 94:aircraft engine, designed for use on 7: 667:Ultralight Aircraft Shopper's Guide 786:"HKS 700T four stroke turbo power" 14: 180: 171: 106:. The engine is manufactured by 24: 386:Green Sky Adventures Micro Mong 771:Compliance Statement July,2006 1: 859:2000s aircraft piston engines 351:Excalibur Aircraft Excalibur 286:Aviation Products Star Trike 127:capacitor discharge ignition 296:BB Microlight BB-two seater 261:Aéro Services Guépard Guépe 875: 466:TechProAviation Merlin 100 811:"HKS 700T Specifications" 749:"HKS 700E Specifications" 32: 23: 18: 515:60 mm (2.4 in) 506:85 mm (3.3 in) 331:Club ULM Rotor Ptenets-2 489:General characteristics 426:RagWing RW22 Tiger Moth 391:Hy-Tek Hurricane Hauler 436:SlipStream Ultra Sport 346:Earthstar Thunder Gull 218: 162:time between overhauls 33:HKS 700E mounted on a 844:Distributor's website 478:Specifications (700E) 371:Flying Machines FM301 714:: CS1 maint: year ( 524:680 cc (41.49 cu in) 416:Quad City Challenger 381:Garland Vampire GA-3 376:Harmening High Flyer 266:Air Creation Skypper 141:cylinder heads. The 84:horizontally opposed 82:is a twin-cylinder, 456:Summit Steel Breeze 411:Phoenix Air Phoenix 406:North Wing Sport X2 366:Flying K Sky Raider 311:ASAP Chinook Plus 2 256:Aeros del Sur Manta 96:ultralight aircraft 556:unleaded auto fuel 446:Sport Flight Talon 441:Solo Wings Aquilla 100:powered parachutes 599:Compression ratio 461:Sundog Two-Seater 431:Rainbow Aerotrike 421:Quicksilver GT400 356:Fletcher Hercules 306:Bede BD-17 Nugget 271:Air Creation Trek 251:Aeroalcool Quasar 192:Rans S-12 Airaile 122:The HKS 700E has 104:ultralight trikes 76: 75: 866: 840: 839: 837:Official website 822: 821: 819: 817: 807:HKS Aviation Co. 803: 797: 796: 794: 792: 782:HKS Aviation Co. 778: 772: 766: 760: 759: 757: 755: 741: 720: 719: 713: 705: 703: 702: 693:. Archived from 683: 677: 663: 563:dry sump with a 485:Cliche & HKS 316:Capella T-Raptor 184: 175: 57: 28: 16: 874: 873: 869: 868: 867: 865: 864: 863: 849: 848: 835: 834: 831: 826: 825: 815: 813: 805: 804: 800: 790: 788: 780: 779: 775: 767: 763: 753: 751: 743: 742: 723: 706: 700: 698: 685: 684: 680: 665:Cliche, Andre: 664: 649: 644: 610: 588: 570:Cooling system: 540: 491: 480: 475: 401:Murphy Maverick 246: 223: 197: 196: 195: 194: 187: 186: 185: 177: 176: 120: 56:National origin 55: 49:aircraft engine 12: 11: 5: 872: 870: 862: 861: 851: 850: 847: 846: 841: 830: 829:External links 827: 824: 823: 798: 773: 761: 721: 691:"HKS Aviation" 678: 646: 645: 643: 640: 637: 636: 634:ULPower UL260i 631: 626: 624:Pegasus PAL 95 621: 616: 609: 606: 605: 604: 595: 587: 584: 583: 582: 577:Reduction gear 573: 567: 558: 550: 539: 536: 535: 534: 525: 516: 507: 498: 490: 487: 479: 476: 474: 473: 468: 463: 458: 453: 448: 443: 438: 433: 428: 423: 418: 413: 408: 403: 398: 393: 388: 383: 378: 373: 368: 363: 358: 353: 348: 343: 338: 336:Cyclone AX2000 333: 328: 323: 318: 313: 308: 303: 298: 293: 288: 283: 278: 276:Airsport Sonet 273: 268: 263: 258: 253: 247: 245: 242: 241: 240: 233: 230: 227: 222: 219: 190:HKS 700E on a 189: 188: 179: 178: 170: 169: 168: 167: 166: 119: 116: 74: 73: 68: 64: 63: 58: 52: 51: 44:Twin cylinder 42: 38: 37: 30: 29: 21: 20: 13: 10: 9: 6: 4: 3: 2: 871: 860: 857: 856: 854: 845: 842: 838: 833: 832: 828: 812: 808: 802: 799: 787: 783: 777: 774: 770: 765: 762: 750: 746: 740: 738: 736: 734: 732: 730: 728: 726: 722: 717: 711: 697:on 1999-10-13 696: 692: 688: 682: 679: 676: 675:0-9680628-1-4 672: 668: 662: 660: 658: 656: 654: 652: 648: 641: 639: 635: 632: 630: 627: 625: 622: 620: 617: 615: 612: 611: 607: 602: 600: 596: 593: 592:Power output: 590: 589: 585: 580: 578: 574: 571: 568: 566: 565:trochoid pump 562: 559: 557: 554: 551: 548: 546: 542: 541: 537: 532: 530: 526: 523: 521: 517: 514: 512: 508: 505: 503: 499: 496: 493: 492: 488: 486: 484: 477: 472: 471:Titan Tornado 469: 467: 464: 462: 459: 457: 454: 452: 451:Stellar Astra 449: 447: 444: 442: 439: 437: 434: 432: 429: 427: 424: 422: 419: 417: 414: 412: 409: 407: 404: 402: 399: 397: 394: 392: 389: 387: 384: 382: 379: 377: 374: 372: 369: 367: 364: 362: 361:Flightstar II 359: 357: 354: 352: 349: 347: 344: 342: 339: 337: 334: 332: 329: 327: 324: 322: 319: 317: 314: 312: 309: 307: 304: 302: 299: 297: 294: 292: 289: 287: 284: 282: 281:Antares MA-33 279: 277: 274: 272: 269: 267: 264: 262: 259: 257: 254: 252: 249: 248: 243: 237: 234: 231: 228: 225: 224: 220: 217: 212: 209: 205: 203: 193: 183: 174: 165: 163: 158: 154: 152: 151:trochoid pump 148: 144: 140: 136: 132: 128: 125: 117: 115: 113: 109: 105: 101: 97: 93: 89: 85: 81: 72: 69: 67:Manufacturer 66: 65: 62: 59: 54: 53: 50: 47: 43: 40: 39: 36: 35:Flightstar II 31: 27: 22: 17: 814:. 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Retrieved 695:the original 681: 666: 638: 597: 591: 575: 569: 560: 552: 543: 527: 520:Displacement 518: 509: 500: 494: 482: 481: 396:Murphy JDM-8 244:Applications 236:Turbocharged 214: 210: 206: 198: 159: 155: 121: 79: 77: 769:HKS Engines 754:27 February 614:Jabiru 2200 586:Performance 561:Oil system: 143:OHV pushrod 137:, but with 131:carburetors 118:Development 92:carburetted 88:four stroke 46:four-stroke 701:2009-12-25 642:References 553:Fuel type: 545:Valvetrain 538:Components 529:Dry weight 291:BAaer Guri 139:oil-cooled 135:air-cooled 816:3 January 791:3 January 629:Rotax 912 483:Data from 341:DTA Combo 301:Bede BD-6 202:Rotax 582 149:, with a 19:HKS 700E 853:Category 809:(2011). 784:(2011). 747:(2011). 710:cite web 689:(n.d.). 619:KFM 112M 608:See also 326:CGS Hawk 221:Variants 147:dry sump 112:Japanese 80:HKS 700E 129:, dual 673:  603:11.3:1 511:Stroke 321:CBB O2 495:Type: 61:Japan 41:Type 818:2012 793:2012 756:2014 716:link 671:ISBN 502:Bore 232:700T 226:700E 124:dual 110:, a 102:and 78:The 745:HKS 687:HKS 108:HKS 71:HKS 855:: 724:^ 712:}} 708:{{ 650:^ 204:. 153:. 98:, 90:, 86:, 820:. 795:. 758:. 718:) 704:. 601:: 579:: 547:: 531:: 522:: 513:: 504::

Index


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
Aeros del Sur Manta

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