Originally developed as the T63 to meet a US Army requirement for a 250 shp turboshaft, the Series I M250 has spawned an entire family of small turbine engines. A program of continuous development has resulted in today's range of Series II and Series IV engines, which power many of the world's most popular helicopters. The recently introduced Value Improvement Package (VIP) kit gives Series IV operators a post-production option to improve performance by five percent. A FADEC upgrade program will also deliver improved capability and reliability.
Specifications
General Characteristics
- Created On Windows
- Wingspan 7.5ft (2.3m)
- Length 13.4ft (4.1m)
- Height 5.1ft (1.6m)
- Empty Weight 551lbs (250kg)
- Loaded Weight 551lbs (250kg)
Performance
- Wing Loading N/A
- Wing Area 0.0ft2 (0.0m2)
- Drag Points 127
Parts
- Number of Parts 1
- Control Surfaces 0
- Performance Cost 150
