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P92 Eaglet G5 - LY - Tecnam.com

P92 Eaglet G5 - LY - Tecnam.com

P92 Eaglet G5 - LY - Tecnam.com

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<strong>P92</strong> <strong>Eaglet</strong> <strong>G5</strong> - <strong>LY</strong>light sport aircraft


CONSTRUCTION• This 5th generation <strong>P92</strong> <strong>Eaglet</strong> builds on our <strong>com</strong>mitment to continue to develop outstanding, stylish, innovative and affordableaeroplanes. For the <strong>Tecnam</strong> team, designing and building aeroplanes isn’t just a job, it’s an extension of our passion for flying.’’• The high efficiency wing is based on the well known NACA63A airfoil while the single-slot flaps, extending along much of the wingspan, allow low stall speeds with great take off and landing performance.• The all movable type (stabilator) horizontal tail,traditional on all <strong>Tecnam</strong> aeroplanes, allows excellent controllability and “hands off”longitudinal stability.• The instrument panel size is increased due to the wider cabin and its modular design can ac<strong>com</strong>modate the most <strong>com</strong>pleteinstrumentation, be it analogue or digital.• The <strong>P92</strong> <strong>Eaglet</strong> fuselage has modified in its forward section, thus allowing for an increase in the cabin width, larger doors for easieraccess and a wider baggage <strong>com</strong>partment, as well as the addition of a new vain provided with an external door which is usefulfor on-board equipment storage.LANDING GEAR• The main spring leaf landing gear, including wheels, tyres and fairings are the same as on all of the other non-retractable <strong>Tecnam</strong>aeroplane models.• The nose gear is free castering and consists of a tubular steel leg, connected to the lower engine mount attachments and isbraced by a oleo-pneumatic shock absorber which is dimensioned for unprepared surfaces and for nose landings, frequent inflight school activities.• All of the landing gear is faired to minimize drag. Ground steering is by differential braking.ENGINE• The Textron Ly<strong>com</strong>ing YO-233-B2A, with a 2400 hrs TBO, provides 115 hp @2800 rpm. Coupled to a fixed pitch propeller, whosegeometric and aerodynamic characteristics are carefully chosen, allowing it to reach top class performance.• The engine is well isolated from vibrations through dyna-focal attachments, its easy and <strong>com</strong>pact installation is readilyaccessible and fuel consumption at 5.3 gal/h in economy cruise, allows autonomies of automotive level. At the same time, thehigher power available magnifies climb and ceiling performance.• Traditional starter’s and alternator’s characteristic drives and the new Electronic Ignition <strong>com</strong>plete the efficiency and versatility ofthis new Textron Ly<strong>com</strong>ing YO-233-B2A engine.light sport aircraft


standard equipmentFlight Instruments And IndicatorsMagnetic CompassAirspeed Ind.,Altimeter Dual Mode (In/Mb)Vertical SpeedBank IndicatorFlap IndicatorPitot SystemStatic SystemStabilator Trim Position IndicatorEngine InstrumentsTachometerHour RecorderOil PressOil Temp.Head Temp.Fuel Press.VoltmeterLh + Rh Fuel QtyFlight ControlsHydraulic BrakesParking BrakeElectrical FlapsDual Flight ControlsSteerable Nose WheelStabilator Trim (Electric Actuated From Stick)Engine Controls:· Throttle, Two · ChokeFlight Trim Controls· Stabilator With IndicatorFuel Control Selector With On/OffPanel Switches:Avionic MasterElectrical System12 Volt 18a Amp. BatterySwitches·· Landing Light·· Strobe Light12 Volt SocketCircuit Breakers PanelFuel SystemTwo Integral Fuel Tanks with 92 Litres Total CapacityEngine Driven Fuel PumpFuel Quick DrainInteriorPilot And Copilot Seats·· Adjustable Fore And Aft·· Arm RestSeat Belts & Shoulder Harness, All SeatsWall To Wall CarpetingMap and Storage PocketsLuggage CompartmentsExteriorEpoxy Corrosion Proofing, All StructureLh/Rh Front Door Pilot/Copilot,Lock And KeyRear WindowAll Windows TintedMain Wheels, 5,00 X 5Nose Wheel, 4,00 X 6Exterior LightsVertical Tail StrobeTaxi LightCabin Confort SystemWindshield DefrosterVentilator Adjustable, 2 PlaceHeating System With DefrostPowerplant And Propeller·· Opion I ROTAXEngine 1 Rotax 912s2 100 Hp, 4 CylindersLiquid/Air Cooled, Integrated Reduction GearDual Ignition SystemThrottle Control Lh/RhTubular Steel Engine MountPropeller Gt 2 Blade FixPropeller SpinnerAir FilterOil Filter12 Volt Alternators 20 Amp.Opion Ii Ly<strong>com</strong>ingEngine 1 Ly<strong>com</strong>ing Yo-233-B2a 115 Hp,4 CylindersDirect DriveDual Ignition SystemThrottle ControlTubular Steel Engine MountPropeller Gt 2 Blade FixPropeller SpinnerAir FilterOil FilterOil Cooler12 Volt Alternators 60 AmpProduct Support/DocumentsManufacturers Full Two YearLimited WarrantyPilots Operation HandbookMaintenance ManualCOSTRUZIONI AERONAUTICHE TECNAM S.R.L.Costruzioni Aeronautiche <strong>Tecnam</strong> operates in two facilities. The Casoria facility is located adjacent to the Napoli Capodichino Airport and covers an area of about 12.000 sqm with about 4.000 sqm of enclosed facilities.The Capua facility is located adjacent to the “Oreste Salomone” Airport, covers an area of about 45.000 sqm with about 11.000 sqm of enclosed facilities.CAPUA plantCASORIA plantCapua Plant p2006t Line ProductionVIA MAIORISE081043 CAPUA (CE) ITA<strong>LY</strong>TEL.+39 0823 620134FAX +39 0823 622899WWW.TECNAM.COMINFO@TECNAM.COM

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