Turboprop Engines
TPE331 Turboprop Engine
TPE331 Turboprop Engine
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Overview
Originally designed in 1959 and certified in 1965, the TPE331 was our first turboprop engine. Developed for multiple applications within military, regional airline, agricultural and general aviation aircraft, the series now includes 18 engine models and 106 configurations.
Today, with more than 13,000 engines delivered and more than 122 million hours of flight time, the TPE331 is one of the most reliable and proven turboprop engines in the world.
Pilots flying TPE331-powered aircraft enjoy exceptional horsepower response and best-in-class fuel economy. Additional TPE331 benefits include quick throttle response for shorter take-offs, good power-to-weight ratio and long maintenance intervals.
Today, with more than 13,000 engines delivered and more than 122 million hours of flight time, the TPE331 is one of the most reliable and proven turboprop engines in the world.
Pilots flying TPE331-powered aircraft enjoy exceptional horsepower response and best-in-class fuel economy. Additional TPE331 benefits include quick throttle response for shorter take-offs, good power-to-weight ratio and long maintenance intervals.
Specifications
Performance
- Oil
- Mil-L-23699B, Mil-L-7808, Type I/ Type II
- (Demonstrated) Operational Limits
- SL–45,000 ft. No minimum O.A.T to + 55ºC
- (Demonstrated) Start Capability
- SL–30,000 ft. No minimum O.A.T. to + 55ºC
- Pressure Ratio
- 10.55
- Key Benefits
- Excellent power-to-weight ratio
- Exceptional horsepower response
- Faster climb and cruising speed
- Improved fuel efficiency
- Larger operating range
- Longer maintenance intervals
- Lower overall operating costs
- Quicker throttle response for shorter takeoffs
- Reduced fuel burn
Power and Electrical
- Electrical Configuration
- 24 vdc,16.2 amp (max)
Maintenance
- Usually Bought With
- Aluminum Gearbox
- Water Methanol Augmentation Manifold
Connectivity and Systems
- Compressor Bleed
- high pressure 10% (max)
- Components
- Air Speed and Ambient Pressure Ratio Transducer
- Beta-Pressure Sensing Switch
- Control System
- Dual Continuous Ignition System
- Fire-Shield Adapter
- Fuel Anti-ice Heating System
- Fuel Pump
- Fuel Purge System
- Fuel Shutoff Valve
- Lubrication System
- Negative-Torque-Sensing (NTS) System
- Oil Temperature-Sensing Bulb
- Propeller Flange
- Propeller Governor
- Propeller-Pitch Control
- Torque and Temperature Limiting
Physical
- Airflow
- 7.7lb/sec
- Weight
- 385 lb
Environmental
- Fuel
- Jet A, Jet B, Jet A-1, JP-8, JP-1, JP-4, JP-5, JP8+100
Performance
- Oil
- Mil-L-23699B, Mil-L-7808, Type I/ Type II
- (Demonstrated) Operational Limits
- SL–45,000 ft. No minimum O.A.T to + 55ºC
- (Demonstrated) Start Capability
- SL–30,000 ft. No minimum O.A.T. to + 55ºC
- Pressure Ratio
- 10.55
- Key Benefits
- Excellent power-to-weight ratio
- Exceptional horsepower response
- Faster climb and cruising speed
- Improved fuel efficiency
- Larger operating range
- Longer maintenance intervals
- Lower overall operating costs
- Quicker throttle response for shorter takeoffs
- Reduced fuel burn
Power and Electrical
- Electrical Configuration
- 24 vdc,16.2 amp (max)
Maintenance
- Usually Bought With
- Aluminum Gearbox
- Water Methanol Augmentation Manifold
Connectivity and Systems
- Compressor Bleed
- high pressure 10% (max)
- Components
- Air Speed and Ambient Pressure Ratio Transducer
- Beta-Pressure Sensing Switch
- Control System
- Dual Continuous Ignition System
- Fire-Shield Adapter
- Fuel Anti-ice Heating System
- Fuel Pump
- Fuel Purge System
- Fuel Shutoff Valve
- Lubrication System
- Negative-Torque-Sensing (NTS) System
- Oil Temperature-Sensing Bulb
- Propeller Flange
- Propeller Governor
- Propeller-Pitch Control
- Torque and Temperature Limiting
Physical
- Airflow
- 7.7lb/sec
- Weight
- 385 lb
Environmental
- Fuel
- Jet A, Jet B, Jet A-1, JP-8, JP-1, JP-4, JP-5, JP8+100
- Oil : Mil-L-23699B, Mil-L-7808, Type I/ Type II
- (Demonstrated) Operational Limits : SL–45,000 ft. No minimum O.A.T to + 55ºC
- (Demonstrated) Start Capability : SL–30,000 ft. No minimum O.A.T. to + 55ºC
- Electrical Configuration : 24 vdc,16.2 amp (max)
- Usually Bought With : Aluminum Gearbox|Water Methanol Augmentation Manifold
- Compressor Bleed : high pressure 10% (max)
- Pressure Ratio : 10.55
- Key Benefits : Excellent power-to-weight ratio|Exceptional horsepower response|Faster climb and cruising speed|Improved fuel efficiency|Larger operating range|Longer maintenance intervals|Lower overall operating costs|Quicker throttle response for shorter takeoffs|Reduced fuel burn
- Components : Air Speed and Ambient Pressure Ratio Transducer|Beta-Pressure Sensing Switch|Control System|Dual Continuous Ignition System|Fire-Shield Adapter|Fuel Anti-ice Heating System|Fuel Pump|Fuel Purge System|Fuel Shutoff Valve|Lubrication System|Negative-Torque-Sensing (NTS) System|Oil Temperature-Sensing Bulb|Propeller Flange|Propeller Governor|Propeller-Pitch Control|Torque and Temperature Limiting
- Airflow : 7.7lb/sec
- Weight : 385 lb
- Fuel : Jet A, Jet B, Jet A-1, JP-8, JP-1, JP-4, JP-5, JP8+100
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