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GE Aviation Overview Featuring 17 million hours on more than 30 applications since its introduction in 1975, the M601 series turboprop engine has a proven record of durability, reliability and ease of maintenance. Derived from this dependable platform, the H80 is bringing advanced power to the turboprop landscape. GE is incorporating sophisticated technologies into the H80 to elevate it to even higher levels of performance. Modern 3D aero design and advanced materials have been integrated into the compressor stages and turbine of the engine's gas generator. A blisk design, replacing individually bladed compressor disks, has also been incorporated in the axial compressor stages. Materials with higher temperature capabilities have been introduced into the turbine nozzle guide vanes of both the gas generator and power turbine. These technologies deliver more shaft horsepower, improve engine fuel efficiency and provide increased temperature margin, significantly enhancing hot-day takeoff performance and high-altitude cruise speeds. H80 Turboprop Engine Standard Engine Hardware Fuel control unit Fuel pump ignition unit Oil filter impeding by-pass signaller Gas generator speed transmitter Prop speed transmitter iTTtransmitter Torquemeter Oil temperature transmitter Engine mount body Accessories Starter/generator Propeller speed governor Propeller speed limiter Engine limiting unit Beta signaller switch Fuel filter with by-pass signaller H8G Turboprop Engine Advancing a legacy of reliable power for turboprop aircraft

Turboprop Engine - Cascade Aircraft Conversionscascadeaircraftconversions.com/images/H80.pdfH80 Turboprop Engine Standard Engine Hardware • Fuelcontrol unit • Fuelpump • ignition

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GE Aviation

OverviewFeaturing 17 million hours on more than 30 applicationssince its introduction in 1975, the M601 series turbopropengine has a proven record of durability, reliability andease of maintenance. Derived from this dependableplatform, the H80 is bringing advanced power to theturboprop landscape.

GEis incorporating sophisticated technologies into theH80 to elevate it to even higher levels of performance.Modern 3D aero design and advanced materials have beenintegrated into the compressor stages and turbine of theengine's gas generator. A blisk design, replacing individuallybladed compressor disks, has also been incorporated in theaxial compressor stages. Materials with higher temperaturecapabilities have been introduced into the turbine nozzleguide vanes of both the gas generator and power turbine.These technologies deliver more shaft horsepower, improveengine fuel efficiency and provide increased temperaturemargin, significantly enhancing hot-day takeoff performanceand high-altitude cruise speeds.

H80Turboprop Engine

Standard Engine Hardware• Fuel control unit

• Fuel pump• ignition unit• Oil filter impeding by-pass signaller

• Gas generator speed transmitter• Prop speed transmitter

• iTTtransmitter

• Torquemeter• Oil temperature transmitter

• Engine mount body

Accessories• Starter/generator• Propeller speed governor• Propeller speed limiter

• Engine limiting unit• Beta signaller switch• Fuel filter with by-pass signaller

H8G Turboprop EngineAdvancing a legacy of reliablepower for turboprop aircraft

GE Aviation

SpecificationsNorth AmericaMatt GerusT 513.552.2985C 513.658.5096rnotthew.qerusssoe.com

EuropeMichal PtacnikT +420222 538 111C +420 602 643 [email protected]

Czech RepublicBercnoych 6519902 Praha 9

Power Output

Sea level - standard dayshp 800

846

ESFC 0.585

gas gen (98.4%) - 36,059shaft - 2,080RPM

ccw from rearPropeller Rotation

390lbsWeight(Basic Dry Mass)

geaviation.com Pressure Ratio

8.2 Ibis

6.7

AirflowSpecifications subject to change without notice.

© 2009 General Electric CompanyAll Rights Reserved.

Fuel Jet A, Jet A-1

27 VDC, 200

Oil Mil-L 23699C

Electrical

Hours - 3,600

Bleed Air 2.4% (maxi

TBOCycles - 6,600

Dimensions

560mm/22"

Prop governor Prop speed

Starter generator

PerformanceMaximum take-off power

(Preliminary Datal850

800

750 a::I!!l

•....(lJ

700 ~o,.:t:!c.s:

650 U1

600

550

500-40 0 40 80 120

OAT (F)

Aircraft accessory

Fuelcontrolunit

1,670mm/66"

Generator speed

580mm/23" Aircraftaccessoriesor alternator

• imagination at work

Ignition

AE-57856 2009/06 (583911