Description
| Engine | Type | Power | Pressure Ratio | Length | Weight (dry) | Compressor/Turbine | Applications |
|---|---|---|---|---|---|---|---|
| AE 2100 | Turboprop | 4,152–4,637 shp (3,096–3,458 kW) | ~16.6 :1 | 114–124 in (2.9–3.15 m) | 1,610–1,925 lb (730–873 kg) | 14‑stage axial / 2‑stage HP + 2‑stage free turbine | AE 2100A: Saab 2000; D2/D3: C‑27J Spartan, C‑130J Super Hercules; J: US‑2 |
| Model 250‑C18 | Turboshaft | ~300 shp (RR300) | 6.2 :1 | 37.6 in (RR300) | 201 lb (RR300 dry) | 1‑stage centrifugal compressor, 2‑stage turbine | RR300: Robinson R66, Bell 47GT‑6; Model 250 series: utility helicopters |
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