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The H80 was certificated by EASA at 13 December 2011, followed by the FAA at 13 March 2012. Its
Russian type certificate was received in October 2012, and the engine also approved by Brazilian Civil Aviation agency (ANAC) and the Argentine Administración Nacional de Aviación Civil.
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of 4,000 hr which could be increased with experience. It promises 10% better fuel burn, 10% longer overhaul and lower maintenance costs than the PT6A-135 for the
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and upgraded the hot section and turbine stages with modern metal alloys for higher temperatures with the same durability.
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stage, and its propulsion section is powered by a single-stage turbine driving a two-stage
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744:"GE's H-Series aerobatic engine powers its first flight on the Diamond DART-550"
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military trainer is due to fly it in early 2018 and it will be certified on the
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The H80 was launched in 2009 based on the M601. GE added a new compressor,
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655:"GE Aviation's H80 Turboprop Engine Gains Its Russian Type Certification"
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The H75-100 weighs 94 lb (43 kg) more than the equivalent
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694:"Nextant G90XT Pilot Report: GE Czech, Nextant Transform King Air"
1341:
812:"Technoavia Purchases GE's H80 Engines for New Rysachok Aircraft"
673:"H75-100 Turboprop Resembles The Walter/Motorlet M601 Powerplant"
212:
179:(EEPC) system received EASA type certification in late 2016. The
890:
GE Aviation Set to Begin
Testing of its New H80 Turboprop Engine
714:"GE Aviation Launches Two New H80 Turboprop Engine Derivatives"
157:
164:) from the M601-F's 580 kW (780 hp), and improves
602:"GE Sees Catalyst As Engine For Change In Turboprop Push"
231:
641:"U.S. FAA Certified GE Aviation's H80 Turboprop Engine"
195:
The two-shaft, reverse flow design is derived from the
234:but pioneers single lever electronic propeller and
133:. The initial H80 is an updated derivative of the
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1378:
814:(Press release). GE Aviation. February 28, 2011.
282:550 shp derivative with aerobatic modifications
137:, while the H75 and H85 are later derivatives.
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657:(Press release). GE Aviation. October 8, 2012.
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643:(Press release). GE Aviation. March 14, 2012.
419:1-stage axial gas.gen + 1-stage axial power
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380:1,670×560×580 mm (66×22×23 in)
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177:Electronic Engine and Propeller Control
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606:Aviation Week & Space Technology
238:in general aviation, for an initial
219:. GE redesigned the compressor with
885:EASA type certification data sheet
330:UVP-E20 (H80-200) and L-410NG (H85)
13:
772:. Gomolzig Aircraft Services GmbH.
699:Business & Commercial Aviation
678:Business & Commercial Aviation
14:
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931:GE Aircraft Engines/GE Aviation/
199:: its core features a two-stage
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620:"Type Certification Data Sheet"
292:
826:"GE H Series Turboprop Engine"
762:
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561:Pratt & Whitney Canada PT6
276:750 shp or 550 shp derivatives
140:
1:
1368:Joint development aeroengines
863:Jane's Aero-Engines 2016-2017
627:Type Certification Data Sheet
583:
358:GE H Series Turboprop Engine
720:. 2012-07-23. Archived from
692:Fred George (Jan 26, 2018).
671:Fred George (Dec 21, 2017).
7:
600:Guy Norris (Mar 19, 2018).
537:
503:8.1 lb (3.7 kg)/s
249:
10:
1403:
629:. EASA. 12 September 2017.
509:8.4 lb (3.8 kg)
457:898 hp (670 kW)
443:850 hp (634 kW)
411:Annular with fuel slinger
388:390 lb (180 kg)
187:crop duster in this year.
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1200:
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566:General Electric Catalyst
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506:8.2 lb (3.7 kg)
494:
454:845 hp (630 kW)
451:795 hp (593 kW)
440:800 hp (597 kW)
437:751 hp (560 kW)
426:
418:
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120:General Electric H-Series
32:
23:
18:
831:. GE Aviation. Nov 2017.
770:"Do28 engine conversion"
578:List of aircraft engines
149:The H80 is based on the
1387:2000s turboprop engines
895:H80 on LeteckeMotory.cz
880:H-Series | GE Aviation
848:"GE's H-Series Engine"
523:Overall pressure ratio
305:
263:
258:H80 installation in a
205:centrifugal compressor
153:
865:. London: Ihs Jane's.
463:Power-to-weight ratio
300:
270:formerly the M601H-80
257:
148:
861:Daly, Mark (2015).
543:Related development
359:
353:Specification (H80)
340:Technoavia Rysachok
99:Technoavia Rysachok
1292:Aeroderivative gas
791:nextantpacific.com
724:on 22 October 2012
555:Comparable engines
377:Dimensions (L×W×H)
357:
328:Let L-410 Turbolet
306:
288:850 shp derivative
264:
154:
86:Major applications
1374:
1373:
535:
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217:planetary gearbox
209:annular combustor
203:and single-stage
131:GE BGA Turboprops
116:
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71:GE BGA Turboprops
36:H85 installation
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346:Thrush Model 510
316:Diamond Dart 550
310:CAIGA Primus 150
304:H85 installation
302:CAIGA Primus 150
181:Diamond Dart 550
162:shaft horsepower
127:aircraft engines
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91:Thrush Model 510
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122:is a family of
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52:National origin
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874:External links
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236:engine control
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106:Developed from
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572:Related lists
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334:Nextant G90XT
332:
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324:G92 (H75-200)
323:
322:Dornier Do-28
320:
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244:Nextant G90XT
241:
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222:
218:
214:
211:and a single
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67:Manufacturer
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61:United States
58:
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933:GE Aerospace
862:
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794:. Retrieved
790:
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764:
752:. Retrieved
750:. 2020-12-10
747:
738:
726:. Retrieved
722:the original
717:
708:
697:
687:
676:
649:
635:
626:
614:
605:
571:
570:
554:
553:
542:
541:
478:gas gen. RPM
293:Applications
229:
194:
174:
170:
166:hot and high
155:
129:produced by
119:
117:
1207:turboshafts
796:4 September
754:10 December
748:GE Aviation
718:GE Aviation
549:Walter M601
434:Shaft power
402:centrifugal
393:Compressor
197:Walter M601
185:Thrush 510G
151:Walter M601
141:Development
135:Walter M601
111:Walter M601
95:Let L-410NG
34:Let L-410NG
1202:Turboprops
728:12 October
584:References
400:+ 1-stage
77:First run
1156:F404/F412
1039:Turbofans
944:Turbojets
492:Shaft RPM
424:fuel type
408:Combustor
385:basic dry
336:(H75-100)
318:(H75-100)
124:turboprop
45:Turboprop
19:H-Series
1381:Category
1342:Propfans
1245:H-Series
1215:Catalyst
1117:Passport
1079:CJ805-23
1047:Affinity
538:See also
517:4,000 h
428:Jet-A/A1
396:2-stage
250:Variants
784:"G90XT"
500:airflow
487:36,183
416:turbine
363:Variant
221:3D aero
213:turbine
1332:LMS100
1327:LM9000
1322:LM6000
1317:LM2500
1312:LM1600
1307:LM1500
1099:GP7000
1067:CFE738
967:GE4/J5
495:2,080
484:35,854
481:35,524
260:Thrush
191:Design
158:blisks
1302:LM500
1192:XA102
1187:XA100
1145:YF120
1105:HF120
1073:CFM56
1062:CF700
1029:YJ101
957:CJ805
952:CJ610
829:(PDF)
787:(PDF)
623:(PDF)
529:6.7:1
473:2.18
398:axial
348:(H80)
342:(H80)
312:(H85)
279:H75-A
207:, an
201:axial
80:2009
41:Type
1355:RISE
1350:GE36
1282:T901
1277:T700
1272:T408
1267:T407
1240:GE38
1235:GE27
1230:CT64
1225:CT58
1205:and
1182:TF39
1177:TF34
1172:RM16
1166:RM12
1161:F414
1150:F136
1140:F118
1135:F110
1129:F108
1124:F101
1111:LEAP
1094:GEnx
1089:GE9X
1084:GE90
1057:CF34
1019:YJ93
897:(cs)
798:2015
756:2020
730:2012
470:2.05
467:1.93
372:H85
262:510G
175:Its
118:The
1262:T64
1257:T58
1252:T31
1220:CT7
1052:CF6
1024:J97
1014:J87
1009:J85
1004:J79
999:J73
994:J47
989:J35
984:J33
979:J31
972:I-A
962:GE1
514:TBO
369:H80
366:H75
285:H85
273:H75
267:H80
240:TBO
232:PT6
1383::
1366:†
837:^
789:.
746:.
716:.
696:.
675:.
663:^
625:.
604:.
592:^
246:.
1357:†
1168:†
1152:†
1131:†
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1101:†
1075:†
1069:†
924:e
917:t
910:v
800:.
758:.
732:.
702:.
681:.
608:.
59:/
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
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