| LTC4B-8 ✕ | |
|---|---|
| Family | T55 |
| Aircraft Engine Manufacturer | Honeywell |
| Aircraft Engine Type | Turboshaft |
| Comment | company designation for L-7 |
| Dry Weight (kg) | 377 |
| Length (mm) | 1196.3 |
| Height (mm) | 615.9 |
| Width (mm) | 615.9 |
| Time Between Overhaul (h) | 3000 |
| Fuel | Jet-A1 |
| LP Compressor Stages | 0 |
| IP Compressor Stages | 0 |
| HP Compressor Stages | 8 |
| HP Compressor Technology | 6 axial, 1 centrifugal |
| Combustion Chamber | Annular reverse flow |
| HP Turbine Stages | 2 |
| HP Turbine Technology | axial |
| IP Turbine Stages | 0 |
| LP Turbine Stages | 2 |
| LP Turbine Technology | axial |
| Overall Pressure Ratio | 9.32 |
| T4 Take Off (°C) | 815 |
| Output Take Off Speed (rpm) | 14750 |
| Output Clockwise Rotation | Yes |