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- ITEC_F124 abstract "The Honeywell/ITEC F124 is a low-bypass turbofan engine derived from the civilian Honeywell TFE731. The F125 is an afterburning version of the engine. The engine began development in the late 1970s for the Republic of China (Taiwan) Air Force AIDC F-CK Indigenous Defence Fighter (IDF), and it first ran in 1979. The F124/F125 engine has since been proposed for use on other aircraft, such as the T-45 Goshawk and the SEPECAT Jaguar, and currently powers the Aero L-159 Alca and the Alenia Aermacchi M-346.The F124 has a rather unusual design for a two spool gas turbine engine, using both axial and centrifugal compressors in its high pressure compressor. There are currently only three production variants of the engine, although several more have been proposed throughout its lifespan.".
- ITEC_F124 thumbnail IAF_Jaguar_and_Honeywell's_F125.JPG?width=300.
- ITEC_F124 wikiPageExternalLink ching.
- ITEC_F124 wikiPageExternalLink announcement_details.jsp?rowID=62&docID=4243&catID=2.
- ITEC_F124 wikiPageExternalLink portal?smap=aerospace&page=Propulsion_Engines3&theme=T5&catID=CDAB5CA0F-004C-6DBB-B50C-20859E156C16&id=HC4776FB6-2D69-1471-51F3-739EC7B713CE&sel=3.
- ITEC_F124 wikiPageExternalLink portal?smap=aerospace&page=Propulsion_Engines3&theme=T5&catID=CDAB5CA0F-004C-6DBB-B50C-20859E156C16&id=HC51EF4A4-AE60-532D-0C77-AC88C834A6B0&sel=4.
- ITEC_F124 wikiPageID "15484915".
- ITEC_F124 wikiPageRevisionID "603507751".
- ITEC_F124 bypass "0.472".
- ITEC_F124 compression "19.4".
- ITEC_F124 compressor "3".
- ITEC_F124 developedFrom Garrett_TFE731.
- ITEC_F124 diameter "36.0".
- ITEC_F124 firstRun "1979".
- ITEC_F124 hasPhotoCollection ITEC_F124.
- ITEC_F124 length "67.0".
- ITEC_F124 lists "*List of aircraft engines".
- ITEC_F124 majorApplications Alenia_Aermacchi_M-346_Master.
- ITEC_F124 majorApplications "AIDC F-CK-1 Ching-kuo".
- ITEC_F124 majorApplications "Aero L-159 Alca".
- ITEC_F124 manufacturer International_Turbine_Engine_Corporation.
- ITEC_F124 manufacturer "Honeywell".
- ITEC_F124 nationalOrigin United_States.
- ITEC_F124 nationalOrigin "Republic of China (Taiwan)".
- ITEC_F124 numberBuilt "460".
- ITEC_F124 related "*Honeywell TFE731".
- ITEC_F124 similarEngines "*Ivchenko-Progress_AI-222 *Rolls-Royce Turbomeca Adour *Lotarev DV-2".
- ITEC_F124 specfuelcon "0.81".
- ITEC_F124 thrust "6300".
- ITEC_F124 weight "5.3".
- ITEC_F124 turbine "1".
- ITEC_F124 type Turbofan.
- ITEC_F124 unitCost "Est. $2.5 million USD .".
- ITEC_F124 weight "1178.0".
- ITEC_F124 subject Category:Honeywell.
- ITEC_F124 subject Category:Low-bypass_turbofan_engines.
- ITEC_F124 subject Category:Turbofan_engines_1970–1979.
- ITEC_F124 comment "The Honeywell/ITEC F124 is a low-bypass turbofan engine derived from the civilian Honeywell TFE731. The F125 is an afterburning version of the engine. The engine began development in the late 1970s for the Republic of China (Taiwan) Air Force AIDC F-CK Indigenous Defence Fighter (IDF), and it first ran in 1979.".
- ITEC_F124 label "Honeywell/ITEC F124".
- ITEC_F124 sameAs m.03mbwhv.
- ITEC_F124 sameAs Q16995809.
- ITEC_F124 sameAs Q16995809.
- ITEC_F124 wasDerivedFrom ITEC_F124?oldid=603507751.
- ITEC_F124 depiction IAF_Jaguar_and_Honeywell's_F125.JPG.
- ITEC_F124 isPrimaryTopicOf ITEC_F124.