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    Maintenancecosts

    comparable to todays industry-leadingCFM56 engines

    Aircraft compliance with future Chapter 14

    noise regulation

    Dispatch reliability99.98%Margin in NOx emissions versus CAEP/6 standards50%

    2 emissionsReduction in fuel consumption and COversus todays engines15%

    CUTTING-EDGE

    PERFORMANCE

    Wihlowerelcosmpio,simplifemaieace a more, he ew LEAPegiewill eliverrivale reliabili, cos-eecive

    perormace,a a improve eviromealoopri.

    CFM commimes: Proven performance Low Risk Execution LeadingTechnology

    CFM Internationals new LEAPengine is pavingtheway for tomorrows aircraft by incorporatingtheindustrys most advancedtechnologiesdevelopedby Snecma (Safran) andGE:morefuel efcient 15%lowerfuelconsumption andCO2emissions comparedtothe current generation quieter,andwithmaintenancecostscomparabletotodaysengines.

    As a worthy successor totheCFM56 famtheworlds best-sellingaircraft enginestheLEAP enginecombines theexpertiseits parent companies tomeet customersincreasingly demandingeconomic and

    environmental requirements.TheLEAPlineincorporates a number of innovativetechnologies developedover nearly 40yresearch anddevelopment,includingoptthermodynamic design,higher bypass ancompression ratios,advanced3-D aeroddesign andgreater useof advanced mat

    TheLEAP enginerepresents theoptimucombination of CFMs unrivaledexperienas thepreferredengine supplier for singaisleaircraft andGEs andSnecmas provexpertiseandconstant investment in res&technology development.All todeliverclass performance,reliability,and cost oownerships toairlines aroundthe globe.

    LEAP OVERVIEW

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    99.98%

    Morethan

    millifligh

    dr

    63025,000

    More

    than

    years of reve(first CFM5-2service in 19

    applications40

    30Prove perormaceCFM has always met its commitments bydelivering reliability for all customers.

    To date, the company has developed21 different engine models, all deliveredon time and on spec as well as 8 enginesupgrades, certied on time and on spec.

    Today, this textbook case of French-American industrial partnershipcan be summarized in three gures:25,000 engines delivered on time, more than630 million ight-hours, and a eet-wide99.98% dispatch reliability rate.

    CFM has leveraged all of this unrivaledexperience for the LEAP engine program,and the basic principle hasnt changed: givecustomers the best possible engine,today and for years to come.

    CFM has a long history of constantlyinvesting in its product lines to delivergreater value.

    This is the approach the company is usingto develop the LEAP engine and will continueto develop new technologies that will beincorporated into the engine throughoutits service life, as well as in a new generationof engines.

    GuARAntEEd On-tIME dELIVERyGaraee o-ime eliver

    PROVEnEXECutIOn

    techolog rives perormaceThe overall performance of an aircraft

    engine is the sum of an optimizedarchitecture and the technologies usedin all major components: the low- andhigh-pressure compressor and turbine,combustor, accessory equipment, digitalengine control unit, and even the nacelle.

    Successfully integrating all of these factorsdemands extensive experience and aportfolio of world-class technologies.

    Thenew LEAPengineembodies theexpertiseand technologies developed over the lastfour decades by GE and Snecma.

    The LEAP engine combines breakthroughtechnologies with proven performance,drawing on CFMs experience as a worldleader in the narrow-body market.

    For the new family of advanced LEAP

    turbofans, CFM chose technologies thatbring high propulsive efciency, low fuelconsumption, and low maintenance costs,including a larger diameter, low-speed fanfor a higher bypass ratio and an advancedhigh-efciency core.

    Advanced LEAP technologies include carbonbercomposites, ceramicmatrix composites,and other leading-edge materials, as well asfourth-generation 3-D aerodynamic designfeatures developed by world-class R&Dteams and proven through extensivetesting and hundreds of millions of hoursof operational experience.

    The result is an outstanding powerplantready to deliver a host of benets to CFMcustomers.

    StAtE-OF-tHE ARttECHnOLOGy

    GE And SntOGEtHER SIn

    PARtnERS tHRO

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    CFMsocs o coiosimprovemeisreflece i he iovaive echologiesiroce i he LEAPegie, rawigoecaeso R&da operaigeebackrom he CFM56amil.Allohese

    echologieshave bee mare avaliae i exesive esig.

    3-Dwoven RTM fan bladesand fan case:intensivetests of a full-scalefan/caseassembly,includinga highly successful5,000cycleendurancetest andblade-outtests.Thesetests haveproven the effectiveness oftheLEAP fan,combining high performance,light weight andstrength.

    Core: the eCore 1, eCore 2, and eCore 3demonstrators have logged more than 400hours of comprehensive testing to validateaerodynamics, performance, aeromechanicalresponse and operability. In addition, tests onthe TAPS II (Twin-Annular, Pre-Swirl) combustor,system dynamics, airfoil aeromechanicalproperties, and operability have validatedtargeted fuel efciency and operationalperformance.

    the low-pressre rbiehas shownoutstandingefciency duringextensive tests.

    Theenginewill beginighttests in2014,leadingtoengine certicationin 2015andentryinto commercialservicein 2016.

    COntInuOuS tEStInG FOR PROVEn

    MAtuRItyCFM has always invested in technologiesthat enhance its products to make sure that

    customers continue to improve their ownperformance. The best-selling CFM56 familysuccessively introduced full authority digitalengine control (FADEC), several generationsof 3-D aero design and, most recently, the suiteof improvements dubbed Tech Insertion in2007 and the CFM56-7BE and CFM56-5P PIP(Performance Improvement Package) in 2011.

    All of these enhancements were not onlyincorporated in new engines, but also availableon engines already in service. Over the years,CFM has decreased specic fuel consumptionby more than 5% and increased thrust by 16%,while reducing emissions and signicantlydecreasing maintenance costs.

    This long-standing philosophy of continuousimprovement, part of CFMs DNA, is already

    an integral part of the LEAP family, and willbe pursued throughout its service life.

    CFM has also introduced lighter and strongermaterials. The companys experience withcomposites reaches back some 30 years,unrivaled among aero-engine manufacturers.

    Research is ongoing and the product linewill eventually add an increasing number ofthermo-structural composite parts to reap thebenets of both the lighter weight and highertemperature capabilities these materialsprovide.

    tECHnOLOGICALMAtuRAtIOn And

    COntInuOuS IMPROVEMEnt

    Mascot test

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    CFM PROduCtIOnAt GE AndSAFRAnFACILItIES

    JV50/50

    CFMS EXPERIEnCEASSuRES SuCCESSFuL

    EXECutIOnIsrial aciliiessmooh rig,cosal improvig

    CFMhas designed,tested,certied,producedandsupported thelargestnumber ofcommercial

    jetenginesin thesingle-aislemarketoverthelast30 years.Thisachievementisanchoredin thedevelopmentandcontinuousimprovementofworld-classfacilitieson bothsides ofthe Atlantic,witheachpartnerresponsibleforhalf theworkload.

    GEisinchargeofthecore,comprisingthehigh-pressurecompressorand turbineandthecombustor.Snecmadesignsand buildsthelow-pressuresection,includingthe fan,thelow-pressurecompressorandturbine,andthe accessorygearbox.FinalassemblyofCFM56enginesis performedbyGE inEvendale,Ohio,nearCincinnatiand bySnecmaat itsfacilitiesin Villaroche,FrancenearParis.

    Procio

    CFM maintains tin theindustry aandexpandingitsin production foBoth GEandSnemanufacturingctheU.S.and Frainvestment of ne

    Thecompany wiproduction betwmorethan 1,550totransition toLThefull transitio2020with an antof 1,700enginesbuildCFM56spa

    Peebles, OH: testing capability

    dao, OH: ducts and tubes

    Eveale, OH: HQ, design,assembly & engine testing

    Rla, Vt: airoils

    Hookse, nH:stator vanes & tubes

    L, MA: combustorliners

    Fama, Sai-nazaire (Frace):rames

    techspace Aero, Liers (Belgim):low-pressure compressor production

    Hispao-Siza (Polska):dressing and equipment

    CFM Ieraioal, CIn

    Secma HAL (Iia): controland accessory production

    Secma Szho (Chia):engine module manuacturingand assembly

    Vicorville, CAfight testing

    Secma, Qeraro (Mexico):engine modules manuacturing

    and assembly

    drham, nC:assembly and engine testing

    Wilmigo, nC:shats & disks

    Greeville, SC:turbine blades

    Abr, AL:engine components

    Ellisville, MS: compositeengine parts, thrust reversers

    Rocheser, ny:3-D Woven RTM an bladeand case

    Secma, Commerc (Frace):3-D Woven RTM an blade and case

    Secma, Geevilliers (Frace): orging, castingand machining o mechanical parts

    Secma, Evr-Corbeil: machining andassembly o engine parts

    Secma, Villaroche: design, assemblyand testing o engines

    Secma, Le Creso: machiningo low-pressure turbine disks

    Hispao-Siza, Colombes: accessory gearbox

    Sagem, Mass: FADEC

    Aircelle, Le Havre: nacelles

    Regesbrg (Germa):TiAl material

    CFM Ieraioal (Frace)

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    LEAP-1AAirbus A320neo Takeoff thrust upto32,900 lbs Enginecert ication:2015 Entry intoservice: 2016

    LEAP-1CCOMAC919

    Takeoff thrust upto30,000 lbs Enginecert ication:2015 Entry intoservice: 2016 SoleWestern powerplant/IPS

    LEAP-1BBoeing 737 MAX

    Takeoff thrust upto28,000 lbs Enginecert ication:2016 Entry intoservice: 2017 Exclusivepowerplant

    Since its formal launch in 2008, the LEAPengine has been setting a new standardfor the single-aisle commercial jet market.Its leadership is anchored in innovative,

    even revolutionary technologies, includingthe wide use of composite materials anda proven architecture that provides industryleading propulsive efciency.

    In 2009, Chinese aircraft manufacturerCOMAC chose the LEAP-1C as the soleWestern powerplant for its new C919,opting for an integrated propulsionsystem (IPS) that includes the engine,nacelle and thrust reverser. At the endof 2010, Airbus chose the LEAP-1A to powerits new A320neo, followed in August 2011by Boeing, which selected the LEAP-1Bas the exclusive engine on its new 737 MAX.

    Each version of this engine is being optimizedto meet the aircraft manufacturers specicrequirements, delivering maximum performancein terms of reliability, fuel consumption and

    maintenance costs. CFM already has a veryhealthy backlog of orders for all threeLEAP-powered airplane applications.

    The LEAP engine family will maintain CFMslong-standing leadership position in thesingle-aisle segment, for which there isa projected demand for more than40,000 engines over the next 20 years.

    LEAP,tHE nEW BEnCHMARK

    In SInGLE-AISLE POWERPLAntS

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    LEAP...A PROVEn BREAKtHROuGH

    FROM CFM

    PROVEn Mature technologies, proven through extensive testing & eld experience.

    Engines delivered on time and on spec.

    CFM and its parent companies have introduced more new engines

    with more operating experience than any other manufacturer.

    BREAKtHROuGH New technologies have always driven progress.

    CFM continually introduces new technologies to improve performance,

    durability, and cost of ownership

    The LEAP technology incorporates 1,003 innovations.

    the LEAP egie coies CFMsraiio o isr-leaigperormace.

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    LEAP-1A AIRBUS A320neo

    LEAP-1A engine

    LEAP 1A AIRBUS A320

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    LEAP-1A AIRBUS A320neo

    The LEAP amily o engines is designed to power commercial aircrat requiring 20,000 to 33,000 pounds o thrust.

    These new-generation engines will set the standard in terms o uel efciency and total cost o ownership.

    LEAP incorporates improvements developed through advanced research & technology, to oer:

    > 15% decrease in uel consumption and CO2 emissions versus todays engines> 50% margin in NOx emissions versus CAEP/6 standards

    > 99.98% dispatch reliability

    > Maintenance costs comparable to todays industry-leading CFM56 engines

    > Aircrat compliance with uture Chapter 14 noise regulation

    Airbus A320neo / LEAP-1A timetable 2011

    A320neolaunch

    2012

    Design reeze

    2013

    First EngineTo Test

    2014

    Flight Tests

    2015

    LEAP-1Acertifcation

    2016

    A320neo /LEAP-1AEIS

    Characteristics

    A/C application A320neo amily

    Takeo thrust Up to 32.9 K

    Bypass ratio (CR) 11:1 class

    Overall pressure ratio (T/O) 40:1 classFan diameter 78

    Compressor Stages

    (an / booster / HPC) 1/3/10

    Turbine Stages (HP / LP) 2/7

    Combustor TAPS IIControl FADEC III

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    LEAP-1B BOEING 737 MAX

    LEAP-1B engine

    LEAP 1B BOEING 737 MAX

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    LEAP-1B BOEING 737 MAX

    The LEAP amily o engines is designed to power commercial aircrat requiring 20,000 to 33,000 pounds o thrust.

    These new-generation engines will set the standard in terms o uel efciency and total cost o ownership.

    LEAP incorporates improvements developed through advanced research & technology, to oer:

    > 15% decrease in uel consumption and CO2

    emissions versus todays engines

    > 50% margin in NOx emissions versus CAEP/6 standards

    > 99.98% dispatch reliability

    > Maintenance costs comparable to todays industry-leading CFM56 engines

    > Aircrat compliance with uture Chapter 14 noise regulation

    Boeing 737 MAX / LEAP-1B timetable 2011

    737 MAXlaunch

    2012 2013

    Design reeze

    2014

    First EngineTo Test

    2015

    Flight tests

    2016

    LEAP-1Bcertifcation

    Characteristics

    A/C application 737 MAX amily

    Takeo thrust Up to 28 K

    Bypass ratio (CR) 9 class

    Overall pressure ratio (T/O) 40:1 classFan diameter 69

    Compressor Stages

    (an / booster / HPC) 1/3/10

    Turbine Stages (HP / LP) 2/5

    Combustor TAPS IIControl FADEC III

    LEAP 1C COMAC919

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    LEAP-1C COMAC919

    LEAP-1C engine

    LEAP 1C COMAC919

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    LEAP-1C COMAC919

    The LEAP amily o engines is designed to power commercial aircrat requiring 20,000 to 33,000 pounds o thrust.

    These new-generation engines will set the standard in terms o uel efciency and total cost o ownership.

    LEAP incorporates improvements developed through advanced research & technology, to oer:

    > 15% decrease in uel consumption and CO2

    emissions versus todays engines

    > 50% margin in NOx emissions versus CAEP/6 standards

    > 99.98% dispatch reliability

    > Maintenance costs comparable to todays industry-leading CFM56 engines

    > Aircrat compliance with uture Chapter 14 noise regulation

    C919 / LEAP-1C timetable 2011

    C919launch

    2012

    Design reeze

    2013

    First EngineTo Test

    2014

    Flight tests

    2015

    LEAP-1Ccertifcation

    2016

    C919 /LEAP-1CEIS

    Characteristics

    A/C application C919 amily

    Takeo thrust Up to 30 K

    Bypass ratio (CR) 11:1 class

    Overall pressure ratio (T/O) 40:1 classFan diameter 78

    Compressor Stages

    (an / booster / HPC) 1/3/10

    Turbine Stages (HP / LP) 2/7

    Combustor TAPS IIControl FADEC III