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Fuji FA-200 Aero Subaru

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1,343 km (834 mi, 725 nmi) ; 55% power at 2,300 m (7,500 ft) with no reserve (max fuel)
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four cylinder air-cooled horizontally-opposed piston engine, 130 kW (180 hp)
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On May 13, 2017, a Fuji FM 200-160 with tail number E7-AAS, crashed in Jasenica, near
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Powered by 130 kW Lycoming IO-320 engine and fitted with fixed-pitch propeller.
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Production started in March 1968, continuing until 1986, with a total of 275 built.
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167 km/h (104 mph, 90 kn) 55% power at 1,525 m (5,000 ft)
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in 1964, the first prototype flying on 12 August 1965. It is a low-wing
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aircraft, fitted with a fixed nosewheel undercarriage and a sliding
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204.5 L (54.0 US gal; 45.0 imp gal)
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More powerful development - 130 kW (180 hp)
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began development of a four-seat light aeroplane, the
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is a single-engine piston-powered monoplane built by
651: 593: 160:in Japan on 6 July 1966, with certification in the 103: 95: 87: 82: 74: 62: 54: 49: 32: 411:97 km/h (60 mph, 52 kn) flaps down 243:Proposed two-seat aerobatic variant, not built. 510:"Light plane crash in Bosnia leaves five dead" 463:. London: Jane's Yearbooks. pp. 120–121. 570: 454: 452: 450: 8: 384:, 1.88 m (6 ft 2 in) diameter 429:3.9 m/s (760 ft/min) at sea level 293:Jane's All the World's Aircraft, 1976-1977 179:Prototype with a 120 kW (160 hp) 577: 563: 555: 255:Proposed crop spraying variant, not built. 29: 399:233 km/h (145 mph, 126 kn) 219:Experimental short takeoff and landing ( 189:Initial version, powered by 120 kW 461:Jane's all the World's Aircraft 1976-77 446: 380:2-bladed McCauley B2D34C53/74E-0 metal 237:Proposed three-seat variant, not built. 690:1960s Japanese civil utility aircraft 27:Single-engine piston-powered airplane 7: 325:9.42 m (30 ft 11 in) 319:8.17 m (26 ft 10 in) 486:The Encyclopedia of World Aircraft 25: 337:14.0 m (151 sq ft) 331:2.59 m (8 ft 6 in) 193:engine and fixed-pitch propeller. 459:Taylor, John W. R., ed. (1976). 223:) version, developed by Japan's 164:occurring on 26 September 1967. 38: 695:Single-engined tractor aircraft 1: 516:. 13 May 2017. Archived from 423:4,200 m (13,700 ft) 358:1,150 kg (2,535 lb) 225:National Aerospace Laboratory 705:Aircraft first flown in 1965 484:Donald, David, ed. (1997). 352:650 kg (1,433 lb) 278:Specifications (FA-200-180) 721: 37: 488:. Aerospace Publishing. 382:constant-speed propeller 205:constant speed propeller 543:FUJI/FA-200 AERO SUBARU 298:General characteristics 260:Accidents and incidents 146:Fuji FA-200 Aero Subaru 123:Fuji FA-200 Aero Subaru 287: 271:Bosnia and Herzegovina 249:Proposed STOL variant. 229:boundary layer control 137:Design and development 118: 18:Fuji FA200 Aero Subaru 285: 142:Fuji Heavy Industries 127:Fuji Heavy Industries 116: 58:Civil light aircraft 356:Max takeoff weight: 50:General information 548:2014-07-17 at the 372:Lycoming IO-360B1B 288: 119: 33:FA-200 Aero Subaru 700:Low-wing aircraft 667: 666: 111: 110: 96:Introduction date 16:(Redirected from 712: 579: 572: 565: 556: 530: 529: 527: 525: 520:on 12 April 2019 514:Business Insider 506: 500: 499: 481: 475: 474: 456: 421:Service ceiling: 392: 300: 156:. It was first 42: 30: 21: 720: 719: 715: 714: 713: 711: 710: 709: 670: 669: 668: 663: 647: 595: 589: 586:Fuji and Subaru 583: 550:Wayback Machine 539: 534: 533: 523: 521: 508: 507: 503: 496: 483: 482: 478: 471: 458: 457: 448: 443: 436: 388: 296: 280: 262: 201:Lycoming IO-360 173: 139: 117:Fuji FA-200-180 45: 44:Fuji FA-200-160 28: 23: 22: 15: 12: 11: 5: 718: 716: 708: 707: 702: 697: 692: 687: 682: 672: 671: 665: 664: 662: 661: 655: 653: 649: 648: 646: 645: 640: 635: 630: 625: 620: 615: 610: 605: 599: 597: 591: 590: 584: 582: 581: 574: 567: 559: 553: 552: 538: 537:External links 535: 532: 531: 501: 494: 476: 469: 445: 444: 442: 439: 435: 432: 431: 430: 427:Rate of climb: 424: 418: 412: 406: 400: 397:Maximum speed: 386: 385: 375: 365: 362:Fuel capacity: 359: 353: 347: 338: 332: 326: 320: 314: 313:2/3 passengers 308: 279: 276: 275: 274: 261: 258: 257: 256: 253: 250: 247: 244: 241: 238: 235: 232: 217: 214: 211: 208: 197: 194: 191:Lycoming O-320 187: 184: 181:Lycoming O-320 177: 172: 169: 138: 135: 109: 108: 107:12 August 1965 105: 101: 100: 97: 93: 92: 89: 85: 84: 80: 79: 76: 72: 71: 66: 60: 59: 56: 52: 51: 47: 46: 43: 35: 34: 26: 24: 14: 13: 10: 9: 6: 4: 3: 2: 717: 706: 703: 701: 698: 696: 693: 691: 688: 686: 685:Fuji aircraft 683: 681: 678: 677: 675: 660: 657: 656: 654: 650: 644: 641: 639: 636: 634: 631: 629: 626: 624: 621: 619: 616: 614: 611: 609: 606: 604: 601: 600: 598: 592: 587: 580: 575: 573: 568: 566: 561: 560: 557: 551: 547: 544: 541: 540: 536: 519: 515: 511: 505: 502: 497: 495:1-85605-375-X 491: 487: 480: 477: 472: 470:0-354-00538-3 466: 462: 455: 453: 451: 447: 440: 438: 433: 428: 425: 422: 419: 416: 413: 410: 407: 404: 403:Cruise speed: 401: 398: 395: 394: 393: 391: 383: 379: 376: 373: 369: 366: 363: 360: 357: 354: 351: 350:Empty weight: 348: 345: 343: 339: 336: 333: 330: 327: 324: 321: 318: 315: 312: 309: 306: 303: 302: 301: 299: 294: 292: 284: 277: 272: 268: 264: 263: 259: 254: 251: 248: 245: 242: 239: 236: 233: 230: 226: 222: 218: 215: 212: 209: 206: 202: 198: 195: 192: 188: 185: 182: 178: 175: 174: 170: 168: 165: 163: 162:United States 159: 155: 151: 147: 143: 136: 134: 132: 128: 124: 115: 106: 102: 98: 94: 90: 86: 81: 77: 73: 70: 67: 65: 61: 57: 53: 48: 41: 36: 31: 19: 602: 522:. Retrieved 518:the original 513: 504: 485: 479: 460: 437: 426: 420: 414: 409:Stall speed: 408: 402: 396: 389: 387: 377: 367: 361: 355: 349: 342:Aspect ratio 340: 334: 328: 322: 316: 310: 304: 297: 295: 290: 289: 227:fitted with 210:FA-200-180AO 166: 145: 140: 122: 120: 104:First flight 88:Manufactured 75:Number built 64:Manufacturer 652:Helicopters 594:Fixed-wing 390:Performance 378:Propellers: 368:Powerplant: 286:Fuji FA-200 203:engine and 674:Categories 441:References 335:Wing area: 196:FA-200-180 186:FA-200-160 524:3 January 323:Wingspan: 311:Capacity: 291:Data from 158:certified 150:all-metal 91:1968–1986 596:aircraft 588:aircraft 546:Archived 434:See also 216:FA-203-S 176:F-200-II 171:Variants 329:Height: 317:Length: 231:system. 83:History 680:Subaru 608:FA-300 603:FA-200 492:  467:  415:Range: 346:6.34:1 267:Mostar 183:engine 154:canopy 305:Crew: 252:F-204 246:F-203 240:F-202 234:F-201 131:Japan 659:UH-2 623:LM-1 618:KM-2 613:KM-1 526:2019 490:ISBN 465:ISBN 370:1 × 221:STOL 121:The 99:1968 69:Fuji 55:Type 643:T-7 638:T-5 633:T-3 628:T-1 307:1/2 269:in 129:of 78:275 676:: 512:. 449:^ 133:. 578:e 571:t 564:v 528:. 498:. 473:. 344:: 207:. 20:)

Index

Fuji FA200 Aero Subaru

Manufacturer
Fuji

Fuji Heavy Industries
Japan
Fuji Heavy Industries
all-metal
canopy
certified
United States
Lycoming O-320
Lycoming O-320
Lycoming IO-360
constant speed propeller
STOL
National Aerospace Laboratory
boundary layer control
Mostar
Bosnia and Herzegovina

Aspect ratio
Lycoming IO-360B1B
constant-speed propeller



ISBN
0-354-00538-3

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