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- Rolls-Royce_AE_2100 abstract "The Rolls-Royce AE 2100 is a turboprop developed by Allison Engine Company, now part of Rolls-Royce North America. A derivative of the Allison AE 1107C-Liberty (Rolls-Royce T406) turboshaft engine, the AE 2100 shares the same high-pressure core as that engine, as does the Rolls-Royce AE 3007. The engine is a two-shaft design, and was the first to use dual FADECs (full authority digital engine control) to control both engine and propeller. There are two versions of the engine: the civil AE2100A, and the AE2100D3 military variant. The engine uses new six-bladed Dowty propellers for use on the 50-seat Saab 2000 and the Lockheed C-130J Hercules military transport. Each engine develops 4,591 shaft horsepower.".
- Rolls-Royce_AE_2100 thumbnail C-130_Hercules_over_Santa_Cruz_Island.jpg?width=300.
- Rolls-Royce_AE_2100 wikiPageExternalLink Spec_Book.pdf.
- Rolls-Royce_AE_2100 wikiPageExternalLink index.php?page=capabilities&lang_id=1&page_id=33.
- Rolls-Royce_AE_2100 wikiPageExternalLink ae_2100.jsp.
- Rolls-Royce_AE_2100 wikiPageExternalLink ae2100.pdf.
- Rolls-Royce_AE_2100 wikiPageID "582907".
- Rolls-Royce_AE_2100 wikiPageRevisionID "587978779".
- Rolls-Royce_AE_2100 compression "16.6".
- Rolls-Royce_AE_2100 compressor "14".
- Rolls-Royce_AE_2100 diameter "28.7".
- Rolls-Royce_AE_2100 hasPhotoCollection Rolls-Royce_AE_2100.
- Rolls-Royce_AE_2100 length "118.0".
- Rolls-Royce_AE_2100 lists "* List of aircraft engines".
- Rolls-Royce_AE_2100 majorApplications Lockheed_Martin_C-130J_Super_Hercules.
- Rolls-Royce_AE_2100 majorApplications "Alenia C-27J Spartan".
- Rolls-Royce_AE_2100 majorApplications "ShinMaywa US-2".
- Rolls-Royce_AE_2100 manufacturer Allison_Engine_Company.
- Rolls-Royce_AE_2100 manufacturer "Rolls-Royce plc".
- Rolls-Royce_AE_2100 nationalOrigin United_States.
- Rolls-Royce_AE_2100 power "4637".
- Rolls-Royce_AE_2100 weight "2.7".
- Rolls-Royce_AE_2100 ref "Rolls-Royce product data sheet.".
- Rolls-Royce_AE_2100 related "* Allison T56 * Rolls-Royce AE 3007 * Rolls-Royce T406".
- Rolls-Royce_AE_2100 turbine "2".
- Rolls-Royce_AE_2100 type Turboprop.
- Rolls-Royce_AE_2100 weight "1727.0".
- Rolls-Royce_AE_2100 subject Category:Rolls-Royce_aircraft_gas_turbine_engines.
- Rolls-Royce_AE_2100 subject Category:Turboprop_engines_1990–1999.
- Rolls-Royce_AE_2100 comment "The Rolls-Royce AE 2100 is a turboprop developed by Allison Engine Company, now part of Rolls-Royce North America. A derivative of the Allison AE 1107C-Liberty (Rolls-Royce T406) turboshaft engine, the AE 2100 shares the same high-pressure core as that engine, as does the Rolls-Royce AE 3007. The engine is a two-shaft design, and was the first to use dual FADECs (full authority digital engine control) to control both engine and propeller.".
- Rolls-Royce_AE_2100 label "Rolls-Royce AE 2100".
- Rolls-Royce_AE_2100 label "Rolls-Royce AE 2100".
- Rolls-Royce_AE_2100 label "Rolls-Royce AE 2100".
- Rolls-Royce_AE_2100 label "Rolls-Royce AE 2100".
- Rolls-Royce_AE_2100 label "ロールス・ロイス AE 2100".
- Rolls-Royce_AE_2100 sameAs Rolls-Royce_AE_2100.
- Rolls-Royce_AE_2100 sameAs Rolls-Royce_AE_2100.
- Rolls-Royce_AE_2100 sameAs Rolls-Royce_AE_2100.
- Rolls-Royce_AE_2100 sameAs Rolls-Royce_AE_2100.
- Rolls-Royce_AE_2100 sameAs ロールス・ロイス_AE_2100.
- Rolls-Royce_AE_2100 sameAs m.02sb_p.
- Rolls-Royce_AE_2100 sameAs Q826898.
- Rolls-Royce_AE_2100 sameAs Q826898.
- Rolls-Royce_AE_2100 wasDerivedFrom Rolls-Royce_AE_2100?oldid=587978779.
- Rolls-Royce_AE_2100 depiction C-130_Hercules_over_Santa_Cruz_Island.jpg.
- Rolls-Royce_AE_2100 isPrimaryTopicOf Rolls-Royce_AE_2100.