Technical data

• The AE2100 turboprop is a two-shaft design with a 14-stage compressor driven by a two-stage HP turbine
• The two-stage IP turbine drives the compound planetary reduction gearbox.
• The engine is the first to use dual FADECs (full authority digital engine control) to control both engine and propeller

Engine	EIS	Power	Applications	Seats	Range (nm)*
AE 2100A	1994	4,152shp 3,100kW	Saab 2000	50	1570
AE2100D3	1998	4,591shp 3,460kW	Lockheed C-130J Lockheed L-100F	-	-
AE2100D2	1999	4,591shp 3,460kW	LMATTS C-27J	-	-
AE2100J		4,591shp 3,460kW	ShinMaywa US-1A Kai	-	-
*Aircraft Manufacturer's Data