AIR-TEC’s TURBO PROP ENGINES

geh75

GE Aviation
Business & General Aviation


Overview

The GE H75 expands the GE Aviation turboprop lineup with power and performance tailored for business and general aviation aircraft. Featuring a maximum 750 SHP rating for both Takeoff and Maximum Continuous operation, the H75 is the ideal power solution to meet the requirements of many turboprop aircraft.

The GE H75 features sophisticated technologies to reach higher levels of performance than preceding engine models. These technologies deliver sustained shaft horsepower capability for hot-day takeoffs and high altitude performance combined with improved engine fuel efficiency and increased temperature margins.

In addition, the unique configuration of the engine simplifies maintenance by eliminating the need for recurrent fuel nozzle maintenance and periodic hot section inspections.

With the standard auto start and limiting unit for ground operations along with linear throttle response, the GE H75 eases pilot workload and enhances engine value and operability.

GE H75
Standard engine hardware


Overview

  • • Fuel control unit
  • • Fuel pump
  • • Ignition unit
  • • ITT transmitter
  • • Gas generator speed sensor
  • • Oil system sensors and transmitters
  • • Torquemeter transmitter
  • • Propeller speed governor with Beta switch
  • • Propeller speed sensor
  • • Propeller over speed limiter
  • • Engine mount isolators
  • • Engine auto start and limiter unit

    Optional accessories
  • • Engine fire bulkheads
  • • Starter/generator
  • • Exhaust stacks

GE Aviation
Business & General Aviation

Specifications

Sea level – standard day
Power Output shp 751 eshp 795
RPM gas gen (96.9%) – 35,524 shaft output – 2,080
Propeller Rotation cw from rear
Weight(basic dry mass) 390 lbs
Airflow 8.1 lb/s
Fuel Jet A, Jet A-1
Oil Mil-L 23699C
Electrical 28 VDC
Bleed Air 4% (max continuous)
TBO
Hours – 3,600
Cycles – 6,600
Basic Warranty
(whichever occurs first)
Hours – 1,000
Cycles – 1,100
Months – 24

Performance

Maximum takeoff power
(Preliminary Data)

h75-spec2

Dimensions


spec3
geh80

GE Aviation
Business & General Aviation


Overview

Certified and in production, the GE H80 turboprop engine combines advanced power and operability with maintenance simplicity. Featuring a maximum 800 SHP rating for both Takeoff and Maximum Continuous operation, this rugged powerplant provides enhanced value to operators worldwide.

The GE H80 features sophisticated technologies to reach higher levels of performance than preceding engine models. These technologies deliver more shaft horsepower, improve engine fuel efficiency and provide increased temperature margin, significantly enhancing hot-day takeoff capability and high-altitude performance.

In addition, the unique configuration of the engine simplifies maintenance by eliminating the need for recurrent fuel nozzle maintenance and periodic hot section inspections.

With the standard auto start and limiting unit for ground operations along with linear throttle response, the GE H80 eases pilot workload and enhances engine operability.

GE H80
Standard engine hardware


Overview

  • • Fuel control unit
  • • Fuel pump
  • • Ignition unit
  • • ITT transmitter
  • • Gas generator speed sensor
  • • Oil system sensors and transmitters
  • • Torquemeter transmitter
  • • Propeller speed governor with Beta switch
  • • Propeller speed sensor
  • • Propeller over speed limiter
  • • Engine mount isolators
  • • Engine auto start and limiter unit

    Optional accessories
  • • Engine fire bulkheads
  • • Starter/generator
  • • Exhaust stacks

GE Aviation
Business & General Aviation

Specifications

Sea level – standard day
Power Output shp 800 eshp 845
RPM gas gen (97.8%) – 35,854 shaft output – 2,080
Propeller Rotation cw from rear
Weight(basic dry mass) 390 lbs
Airflow 8.2 lb/s
Fuel Jet A, Jet A-1
Oil Mil-L 23699C
Electrical 28 VDC
Bleed Air 4% (max continuous)
TBO
Hours – 3,600
Cycles – 6,600
Basic Warranty
(whichever occurs first)
Hours – 1,000
Cycles – 1,100
Months – 24

Performance

Maximum takeoff power
(Preliminary Data)

spec22

Dimensions


engine-spec-2
h85-spec1

GE Aviation
Business & General Aviation


Overview

The GE H85 expands the GE Aviation turboprop lineup with higher levels of power and performance. Featuring a maximum 850 SHP rating for both Takeoff and Maximum Continuous operation, the H85 answers the need for increased power required by higher performance turboprop aircraft.

The GE H85 features sophisticated technologies to reach higher levels of performance than preceding engine models. These technologies deliver more shaft horsepower, improve engine fuel efficiency and provide increased temperature margin, significantly enhancing hot-day takeoff capability and high- altitude performance.

In addition, the unique configuration of the engine simplifies maintenance by eliminating the need for recurrent fuel nozzle maintenance and periodic hot section inspections.

With the standard auto start and limiting unit for ground operations along with linear throttle response, the GE H85 eases pilot workload and enhances engine value and operability.

GE H85
Standard engine hardware


Overview

  • • Fuel control unit
  • • Fuel pump
  • • Ignition unit
  • • ITT transmitter
  • • Gas generator speed sensor
  • • Oil system sensors and transmitters
  • • Torquemeter transmitter
  • • Propeller speed governor with Beta switch
  • • Propeller speed sensor
  • • Propeller over speed limiter
  • • Engine mount isolators
  • • Engine auto start and limiter unit

    Optional accessories
  • • Engine fire bulkheads
  • • Starter/generator
  • • Exhaust stacks

GE Aviation
Business & General Aviation

Specifications

Sea level – standard day
Power Output shp 850 eshp 898
RPM gas gen (98.7%) – 36,183 shaft output – 2,080
Propeller Rotation cw from rear
Weight(basic dry mass) 390 lbs
Airfl ow 8.4 lb/s
Fuel Jet A, Jet A-1
Oil Mil-L 23699C
Electrical 28 VDC
Bleed Air 4% (max continuous)
TBO
Hours – 3,600
Cycles – 6,600
Basic Warranty
(whichever occurs first)
Hours – 1,000
Cycles – 1,100
Months – 24

Performance

Maximum takeoff power
(Preliminary Data)

h85-spec2

Dimensions


spec3

Contact Us

  • Head Office:
    Office 111, Ebene Junction,
    Rue de la Démocratie, Ebene,
    Mauritius
  • May Zietsman
    +230 467 55 59
    sales@air-tecm.com
    www.air-tecm.com
  • © Air-Tec 2016