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Turbine engine failure

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decided to return to the airport of departure, but during the landing approach a fire broke out, which destroyed the control systems and as a result, the plane crashed to the ground 3200 meters from the threshold of the runway of the Yemelyanovo airport and collapsed. Of the 111 people on board (104 passengers and 7 crew members), one survived. The cause of the catastrophe was the destruction of the disk of the first stage of the low pressure circuit of engine No. 3, which occurred due to the presence of fatigue cracks. The cracks were caused by a manufacturing defect – the inclusion of a titanium-nitrogen compound that has a higher microhardness than the original material. The methods used at that time for the manufacture and repair of disks, as well as the means of control, were found to be partially obsolete, which is why they did not ensure the effectiveness of control and detection of such a defect. The defect itself arose probably due to accidental ingestion of a titanium sponge or charge for smelting an ingot of a piece enriched with nitrogen.
264: 426:, Moscow in 1994, failed to stop after engine startup and continued to operate at over 40,000 rpm with open bleed valves from engines, which caused an uncontained failure of the starter. A detached turbine disk damaged fuel and oil supply lines (which caused fire) and hydraulic lines. The fire-extinguishing system failed to stop the fire, and the plane diverted back to Irkutsk. However, due to loss of hydraulic pressure the crew lost control of the plane, which subsequently crashed into a dairy farm killing all 124 on board and one on the ground. 72:. Engines operate efficiently with regularly scheduled inspections and maintenance. These units can have lives ranging in the tens of thousands of hours of operation. However, engine malfunctions or failures occasionally occur that require an engine to be shut down in flight. Since multi-engine airplanes are designed to fly with one engine inoperative and flight crews are trained to fly with one engine inoperative, the in-flight shutdown of an engine typically does not constitute a serious safety of flight issue. 22: 939: 171:— a malfunction that is typified by loud bangs and even flames from the engine's inlet and tailpipe. A compressor surge is a disruption of the airflow through a gas turbine jet engine that can be caused by engine deterioration, a crosswind over the engine's inlet, ice accumulation around the engine inlet, ingestion of foreign material, or an internal component failure such as a broken 306:
externally mounted components). Once the failure event starts, secondary events of a random nature may occur whose course and ultimate conclusion cannot be precisely predicted. Some of the structural interactions that have been observed to affect containment are the deformation and/or deflection of blades, cases, rotor, frame, inlet, casing rub strips, and the containment structure.
377:: a Boeing 737 flying from Manchester to Corfu in 1985 suffered an uncontained engine failure and fire on takeoff. The takeoff was aborted and the plane turned onto a taxiway and began evacuating. Fifty-five passengers and crew were unable to escape and died of smoke inhalation. The accident led to major changes to improve the survivability of aircraft evacuations. 521:, registration F-HPJE performing flight from Paris, France, to Los Angeles, United States, was en route about 200 nautical miles (230 mi; 370 km) southeast of Nuuk, Greenland, when it suffered a catastrophic engine failure in 2017 (General Electric / Pratt & Whitney Engine Alliance GP7000). The crew descended the aircraft and diverted to 349:, the failure of the aircraft's inner left (#2) engine damaged the outer left (#1) engine, setting both on fire and causing loss of flight controls, leading to a crash that killed all 183 people on board. In both cases, the turbine shaft in engine #2 disintegrated due to production defects in the engines' bearings, which were missing rollers. 238:. VR is the speed at which the nose is lifted off the runway, a process known as rotation. V2 is the single-engine safety speed, the single engine climb speed. The use of these speeds ensure that either sufficient thrust to continue the takeoff, or sufficient stopping distance to reject it will be available at all times. 356:
was a major aircraft crash that occurred on Sunday, December 23, 1984, in the vicinity of Krasnoyarsk. The Tu-154B-2 airliner of the 1st Krasnoyarsk united aviation unit (Aeroflot) performed passenger flight SU-3519 on the Krasnoyarsk-Irkutsk route, but during the climb, engine No. 3 failed. The crew
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Uncontained turbine engine disk failures within an aircraft engine present a direct hazard to an airplane and its crew and passengers because high-energy disk fragments can penetrate the cabin or fuel tanks, damage flight control surfaces, or sever flammable fluid or hydraulic lines. Engine cases are
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as long as the engine parts exit via the existing openings in the engine inlet or outlet, and do not create new openings in the engine case containment. Fan blade fragments departing via the inlet may also cause airframe parts such as the inlet duct and other parts of the engine nacelle to depart the
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Engine failures can be caused by mechanical problems in the engine itself, such as damage to portions of the turbine or oil leaks, as well as damage outside the engine such as fuel pump problems or fuel contamination. A turbine engine failure can also be caused by entirely external factors, such as
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engine. The failure was found to have been caused by a misaligned counter bore within a stub oil pipe leading to a fatigue fracture. This in turn led to an oil leakage followed by an oil fire in the engine. The fire led to the release of the Intermediate Pressure Turbine (IPT) disc. The airplane,
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positioned near the runway. The prompt landing is a precaution against the risk that another engine will fail later in the flight or that the engine failure that has already occurred may have caused or been caused by other as-yet unknown damage or malfunction of aircraft systems (such as fire or
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on 15 September 2001, suffered an uncontained engine failure (Rolls-Royce RB.183 Tay) in which fragments of the engine shattered three cabin windows, causing decompression and pulling a passenger partly out of the plane. Another passenger held the passenger in until the aircraft landed, but the
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of one per 375,000 flight hours, compared to of one every 3,200 flight hours for aircraft piston engines. Due to "gross under-reporting" of general aviation piston engines in-flight shutdowns (IFSD), the FAA has no reliable data and assessed the rate "between 1 per 1,000 and 1 per 10,000 flight
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The containment of failed rotating parts is a complex process which involves high energy, high speed interactions of numerous locally and remotely located engine components (e.g., failed blade, other blades, containment structure, adjacent cases, bearings, bearing supports, shafts, vanes, and
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In order to allow twin-engined aircraft to fly longer routes that are over an hour from a suitable diversion airport, a set of rules known as ETOPS (Extended Twin-engine Operational Performance Standards) is used to ensure a twin turbine engine powered aircraft is able to safely arrive at a
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diversionary airport after an engine failure or shutdown, as well as to minimize the risk of a failure. ETOPS includes maintenance requirements, such as frequent and meticulously logged inspections and operation requirements such as flight crew training and ETOPS-specific procedures.
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flying from Chicago to Miami in 2016 suffered an uncontained engine failure on its #2 engine (General Electric CF6) during takeoff resulting in a large fire which destroyed the outer right wing. The aircraft aborted takeoff and was evacuated with 21 minor injuries, but no
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to ensure containment of shrapnel if blade separation occurs. Blade fragments exiting the inlet or exhaust can still pose a hazard to the aircraft, and this should be considered by the aircraft designers. A nominally contained engine failure can still result in engine
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on June 8, 1995, suffered an uncontained engine failure of the 7th stage high pressure compressor disk due to inadequate inspection of the corroded disk. The resulting rupture caused jet fuel to flow into the cabin and ignite, and the fire caused the jet to be a
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not designed to contain failed turbine disks. Instead, the risk of uncontained disk failure is mitigated by designating disks as safety-critical parts, defined as the parts of an engine whose failure is likely to present a direct hazard to the aircraft.
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did not account for the position of the number-two engine, mounted at the tail close to hydraulic lines, nor the results of fragments released in many directions. Since then, aircraft engine designs have focused on keeping shrapnel from puncturing the
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A contained engine failure is one in which all internal rotating components remain within or embedded in the engine's case (including any containment wrapping that is part of the engine), or exit the engine through the tail pipe or air
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The very specific technical distinction between a contained and uncontained engine failure derives from regulatory requirements for design, testing, and certification of aircraft engines under Part 33 of the U.S.
1075:"Катастрофа Ту-154М а/к 'Байкал' в районе Иркутска (борт RA-85656), 03 января 1994 года. // AirDisaster.ru - авиационные происшествия, инциденты и авиакатастрофы в СССР и России - факты, история, статистика" 116:
damage to aircraft flight controls) that may pose a continuing risk to the flight. Once the aircraft lands, fire department personnel assist with inspecting the aircraft to ensure it is safe before it
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A turbine-powered aircraft's takeoff procedure is designed around ensuring that an engine failure will not endanger the flight. This is done by planning the takeoff around three critical
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and are subject to engine failures for many similar reasons as jet-powered aircraft. In the case of an engine failure in a helicopter, it is often possible for the pilot to enter
1204: 395:. There were 111 fatalities. Prior to this crash, the probability of a simultaneous failure of all three hydraulic systems was considered as low as one in a billion. However, 704: 182:. This additional fuel can result in flames extending from the engine's exhaust pipe. As alarming as this would appear, at no time is the engine itself actually on fire. 463: 147:, using the unpowered rotor to slow the aircraft's descent and provide a measure of control, usually allowing for a safe emergency landing even without engine power. 625: 103:
is known for its reliability with an in-flight shutdown rate of one per 333,333 hours from 1963 to 2016, lowering to one per 651,126 hours over 12 months in 2016.
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engine during takeoff, resulting in a large fire on its port side. The aircraft successfully aborted takeoff and the plane was evacuated with no fatalities.
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An uncontained engine event occurs when an engine failure results in fragments of rotating engine parts penetrating and escaping through the engine case.
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As a work of the United States Federal Government, the source is in the public domain and may be adapted freely per USC Title 17; Chapter 1; §105 (see
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reports the FAA states general aviation engines experience one failures or IFSD every 10,000 flight hours, and states its
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Other events that can happen with jet engines, such as a fuel control fault, can result in excess fuel in the engine's
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Most in-flight shutdowns are harmless and likely to go unnoticed by passengers. For example, it may be prudent for the
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flying from Pensacola, Florida to Atlanta in 1996 had a cracked compressor rotor hub failure on one of its
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Antoni Milkiewicz (October 1991). "Jeszcze o Lesie Kabackim" [More on the Kabacky Forest].
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Turbine engine unexpectedly stops producing power due to a malfunction other than fuel exhaustion
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flying from London Heathrow to Sydney (via Singapore) in 2010 had an uncontained failure in a
581:"Aircraft ReciprocatingEngine Failure: An Analysis of Failure in a Complex Engineered System" 558: 482: 96: 53: 740: 705:"Airplane Turbofan Engine Operation and Malfunctions Basic Familiarization for Flight Crews" 341:, suffered catastrophic uncontained engine failures in the 1980s. The first was in 1980 on 263: 1260: 514: 391:-6 engine caused the loss of all hydraulics, forcing the pilots to attempt a landing using 388: 353: 327: 185:
Also, the failure of certain components in the engine may result in a release of oil into
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flying from Las Vegas to London in 2015 suffered an uncontained engine failure on its #1
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Following an engine shutdown, a precautionary landing is usually performed with airport
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is one per 20,704 flight hours, lowering to one per 163,934 flight hours in 2013–2014.
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aircraft due to deformation from the fan blade fragment's residual kinetic energy.
235: 168: 872:"FAA Advisory Circular AC 33-5: Turbine Engine Rotor Blade Containment/Durability" 486:
however, landed safely. This led to the grounding of the entire Qantas A380 fleet.
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has an in-flight shutdown rate (IFSD) of one per million engine flight-hours. The
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to shut down an engine and perform a precautionary landing in the event of a low
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after it experienced catastrophic uncontained compressor rotor failure in 1996.
175:. While this situation can be alarming, the engine may recover with no damage. 1249: 990: 943: 522: 275:
Engine failures may be classified as either as "contained" or "uncontained".
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where flight controls were destroyed, killing all 87 on board. In 1987, on
193:. The dangers of fume events are the subject of debate in both aviation and 207: 160: 144: 80: 518: 478: 326:
flying from Miami to San Francisco in 1973 had an overspeed failure of a
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or high oil temperature warning in the cockpit. However, passengers in a
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flying between Douala and Garoua, Cameroon in 1984 had a failure of a
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that can cause an odor or oily mist in the cabin. This is known as a
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Turbine engines in use on today's turbine-powered aircraft are very
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This article contains text from a publication of the United States
1006:"ASN Aircraft accident Boeing 737-2H7C TJ-CBD Douala Airport (DLA)" 691:
a helicopter can be landed safely in the event of an engine failure
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The damaged fan disk of the engine that catastrophically failed on
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This article incorporates text from this source, which is in the
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to achieve penetration resistance while keeping the weight low.
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flying from Denver to Chicago in 1989. The failure of the rear
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may become quite alarmed by other engine events such as a
674:. U.S. Government Printing Office, Washington D.C.: U.S. 150: 1203:
Bryan, Victoria; Dobuzinskis, Alex (30 September 2017).
962:. National Transportation Safety Board. 15 January 1975 840:"Uncontained Engine Failure - SKYbrary Aviation Safety" 464:
Recife/Guararapes–Gilberto Freyre International Airport
256: 241: 1053:"ASN Aircraft accident Tupolev 154M RA-85656 Mamony" 600:(Press release). Continental Motors. 10 April 2014. 525:, Canada, for a safe landing about two hours later. 79:(FAA) was quoted as stating turbine engines have a 52:, but other turbine engines can also fail, such as 653:"Flight test: Upgraded Pilatus PC-12 powers ahead" 404:or ductwork, increasingly utilizing high-strength 980: 618: 1247: 1202: 556: 435:Hartsfield Jackson Atlanta International Airport 544:"What is the Lifespan of an Airplane's Engine?" 650: 614:(Press release). GE Aviation. 19 January 2012. 559:"Aerial Perspective: Flying Dollars and Sense" 899:Blade containment and rotor unbalance tests. 598:"Continental: 4 Million Diesel Flight Hours" 314:Notable uncontained engine failure accidents 586:. Australian Transport Safety Bureau. 2007. 866: 864: 862: 860: 225: 628:. AirInsight. 9 June 2016. Archived from 468:São Paulo/Guarulhos International Airport 738: 262: 20: 1176: 857: 604: 471:passenger blown out of the window died. 1248: 1150: 151:Shutdowns that are not engine failures 1055:. Aviation-safety.net. 3 January 1994 892: 815:"ETOPS, EROPS and Enroute Alternates" 1231:National Transportation Safety Board 106: 1151:Phipps, Claire (9 September 2015). 1031:"Lessons of Manchester runway fire" 732: 557:Steven E. Scates (September 2007). 13: 1177:Shapiro, Emily (28 October 2016). 1126:"Qantas grounds A380s after scare" 1003: 793:"Aeronatutical Information Manual" 659: 257:Contained and uncontained failures 242:Failure during extended operations 200: 14: 1292: 773:. Federal Aviation Administration 414:: a starter of engine No. 2 on a 937: 739:Nassauer, Sarah (30 July 2009). 44:due to a malfunction other than 1196: 1170: 1144: 1118: 1092: 1067: 1045: 1023: 997: 974: 949: 832: 807: 785: 760: 710:Federal Aviation Administration 676:Federal Aviation Administration 347:LOT Polish Airlines Flight 5055 77:Federal Aviation Administration 697: 651:Mike Gerzanics (6 June 2016). 644: 590: 573: 550: 536: 330:-6, resulting in one fatality. 101:Pratt & Whitney Canada PT6 63: 1: 1276:Emergency aircraft operations 1102:. 11 May 2009. Archived from 529: 354:Tu-154 crash near Krasnoyarsk 123: 40:unexpectedly stops producing 504:American Airlines Flight 383 371:-15 engine. Two people died. 361:Cameroon Airlines Flight 786 343:LOT Polish Airlines Flight 7 299:parts departing the aircraft 290:Federal Aviation Regulations 7: 490:British Airways Flight 2276 442:Delta Air Lines Flight 1288 375:British Airtours Flight 28M 320:National Airlines Flight 27 269:Delta Air Lines Flight 1288 214:or weather conditions like 10: 1297: 1233:. which can be found here 668:Rotorcraft Flying Handbook 412:Baikal Airlines Flight 130 381:United Airlines Flight 232 245: 27:United Airlines Flight 232 120:to its parking position. 113:fire and rescue equipment 450:Pratt & Whitney JT8D 369:Pratt & Whitney JT8D 56:used in power plants or 1238:Knowledge:Public Domain 983:Aero: Technika Lotnicza 747:The Wall Street Journal 452:-219 engines. Two died. 446:McDonnell Douglas MD-88 385:McDonnell Douglas DC-10 324:McDonnell Douglas DC-10 226:Failures during takeoff 58:combined diesel and gas 48:. It often applies for 272: 131:-powered aircraft and 60:vessels and vehicles. 34:turbine engine failure 29: 483:Rolls-Royce Trent 900 266: 97:General Electric GE90 54:ground-based turbines 24: 908:, 14 CFR 33.94, 1984 904:12 June 2011 at the 820:. The Boeing Company 678:. 2000. p. 30. 515:Air France Flight 66 389:General Electric CF6 328:General Electric CF6 165:jet powered aircraft 139:are also powered by 1010:aviation-safety.net 406:composite materials 393:differential thrust 335:LOT Polish Airlines 1079:www.airdisaster.ru 795:. Transport Canada 546:. 13 January 2023. 397:statistical models 273: 86:Continental Motors 38:gas turbine engine 30: 1242: 1132:. 4 November 2010 844:www.skybrary.aero 632:on 17 August 2016 107:Emergency landing 90:Centurion engines 1288: 1281:Aircraft engines 1227: 1220: 1219: 1217: 1215: 1200: 1194: 1193: 1191: 1189: 1174: 1168: 1167: 1165: 1163: 1148: 1142: 1141: 1139: 1137: 1122: 1116: 1115: 1113: 1111: 1096: 1090: 1089: 1087: 1085: 1071: 1065: 1064: 1062: 1060: 1049: 1043: 1042: 1040: 1038: 1033:. 23 August 2010 1027: 1021: 1020: 1018: 1016: 1001: 995: 994: 978: 972: 971: 969: 967: 961: 953: 947: 941: 940: 936: 934: 932: 918: 909: 896: 890: 889: 887: 885: 876: 868: 855: 854: 852: 850: 836: 830: 829: 827: 825: 819: 811: 805: 804: 802: 800: 789: 783: 782: 780: 778: 772: 764: 758: 757: 755: 753: 744: 736: 730: 729: 727: 725: 720:on 22 April 2023 719: 713:. 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FAA-8083-21. 686: 671: 665: 664: 660: 655:. flightglobal. 649: 645: 635: 633: 624: 623: 619: 610: 609: 605: 596: 595: 591: 583: 579: 578: 574: 555: 551: 542: 541: 537: 532: 456:TAM Flight 9755 429:ValuJet 597: A 339:Ilyushin Il-62s 316: 294:blade off tests 259: 250: 244: 228: 203: 201:Possible causes 153: 141:turbine engines 126: 109: 66: 46:fuel exhaustion 17: 12: 11: 5: 1294: 1284: 1283: 1278: 1273: 1271:Aviation risks 1268: 1263: 1258: 1244: 1243: 1222: 1221: 1195: 1169: 1143: 1117: 1106:on 11 May 2009 1091: 1066: 1044: 1022: 996: 973: 948: 910: 891: 856: 831: 806: 784: 759: 731: 696: 684: 658: 643: 617: 603: 589: 572: 549: 534: 533: 531: 528: 527: 526: 512: 501: 487: 472: 453: 439: 427: 409: 378: 372: 358: 350: 337:flights, both 331: 315: 312: 285: 284: 281: 267:The engine of 258: 255: 246:Main article: 243: 240: 227: 224: 202: 199: 152: 149: 125: 122: 108: 105: 65: 62: 36:occurs when a 15: 9: 6: 4: 3: 2: 1293: 1282: 1279: 1277: 1274: 1272: 1269: 1267: 1264: 1262: 1259: 1257: 1254: 1253: 1251: 1241: 1239: 1235: 1232: 1226: 1225: 1210: 1206: 1199: 1184: 1180: 1173: 1158: 1154: 1147: 1131: 1127: 1121: 1105: 1101: 1095: 1080: 1076: 1070: 1054: 1048: 1032: 1026: 1011: 1007: 1000: 992: 988: 984: 977: 958: 952: 945: 944:public domain 927: 923: 917: 915: 907: 903: 900: 895: 880: 873: 867: 865: 863: 861: 845: 841: 835: 816: 810: 794: 788: 769: 763: 748: 743: 735: 716: 712: 711: 706: 700: 693: 692: 687: 685:1-56027-404-2 681: 677: 670: 669: 662: 654: 647: 631: 627: 621: 613: 607: 599: 593: 582: 576: 568: 566: 563:Professional 560: 553: 545: 539: 535: 524: 520: 516: 513: 509: 505: 502: 499: 495: 491: 488: 484: 480: 476: 473: 469: 465: 461: 457: 454: 451: 447: 443: 440: 436: 432: 428: 425: 421: 418:heading from 417: 413: 410: 407: 403: 398: 394: 390: 386: 382: 379: 376: 373: 370: 366: 362: 359: 355: 351: 348: 344: 340: 336: 332: 329: 325: 321: 318: 317: 311: 307: 303: 300: 295: 291: 282: 278: 277: 276: 270: 265: 261: 254: 249: 239: 237: 233: 223: 221: 217: 216:precipitation 213: 209: 198: 196: 192: 188: 183: 181: 176: 174: 170: 166: 162: 158: 148: 146: 142: 138: 134: 130: 121: 119: 114: 104: 102: 98: 93: 91: 87: 82: 78: 73: 71: 61: 59: 55: 51: 47: 43: 39: 35: 28: 23: 19: 1228: 1212:. 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Index


United Airlines Flight 232
gas turbine engine
power
fuel exhaustion
aircraft
ground-based turbines
combined diesel and gas
reliable
Federal Aviation Administration
failure rate
Continental Motors
Centurion engines
General Electric GE90
Pratt & Whitney Canada PT6
fire and rescue equipment
taxis
Turboprop
turboshaft
helicopters
turbine engines
autorotation
flight crew
oil pressure
jet powered aircraft
compressor surge
blade
combustor
bleed air
fume event

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