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TPE331
Also Known As:
TPE331-1, TPE331-10, TPE331-10GD, TPE331-11, TPE331-12, TPE331-14, TPE331-14GR-801E (engine powering An-38), TPE331-15, TPE331-2, TPE331-3, TPE331-5, TPE331-6, TPE331-8
Origin:United States of America
Contractor/s:
Honeywell
Description:
The Honeywell TPE331 is a family of turboprop engines developing between 715 and 1,645 shaft-horse-power (shp). The TPE331 engine has been selected to power the Antonov An-38 turboprop aircraft.
Specifications
Weights: Dry Weight 629 lb (285 kg)
Power: Emergency Power 1,712 shp, Max Power at TakeOff 1,645 shp
Other: Fan Pressure Ratio 11
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Applications
An-38-120, Jetstream 32, Jetstream 41, MQ-9A Reaper, Pilatus PC-6 Porter
Operators
see operators map
 Russia
 United Kingdom
 United States of America
Internet Resources
e-engines.honeywell.com
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)
Last Updated: Sunday, September 28, 2008
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