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SPECIFICATION AND DESCRIPTIONTTxDecember 2015Revision DUnits T240-2096 to TBD

CESSNA TTxSPECIFICATIONAND DESCRIPTIONUNITS 2096 TO TBDDECEMBER 2015REVISION DC e ssna A irc raft C ompanyP.O. B ox 7 7 06W ic hita, Kansas 6 7 27 7 -7 7 0 6

CESSNA TTxINTRODUCTIONThis document is published for the purpose of providinggeneral information for the evaluation of design, performance and equipment of the TTx Model T240. Should moreinformation be required, please contact:Cessna Aircraft CompanySingle Engine Piston AircraftP.O. Box 7706Wichita, Kansas 67277-7706This document supersedes all previous Specification andDescription documents and describes only the TTx ModelT240, its powerplant and equipment. Also included are thewarranties applicable to the TTx Model T240 aircraft, theContinental Motors TSIO-550-C engine and the installedGarmin avionics. In the event of any conflict or discrepancybetween this document and the basic purchase agreement,the basic purchase agreement language shall govern. Dueto the time span between the date of this Specification andDescription and the scheduled delivery date of the aircraft,Cessna reserves the right to revise the “Specification”whenever occasioned by product improvements, government regulations or other good cause.1-800-4-CESSNAwww.se.cessna.comDecember 2015, Revision D1

CESSNA TTxTABLE OF CONTENTSCESSNA TTx SPECIFICATION AND DESCRIPTIONSECTION PAGE1.General Description .1.1Certification .1.2Approximate Dimensions .1.3Design Weights and Capacities .2.Performance .3.Powerplant & Accessories .4.TTx Equipment List .5.Instrument Panel .6.Electrical Power .7.Engine Indicating System .8.Environmental .9.Exterior .10.Exterior Lights .11.Flight Controls .12.Fuel System .13.Interior .14.Interior Lighting .15.Exterior Striping Options .16.Limited Warranties .16.1Cessna’s Limited Warranty - Single Engine Piston Aircraft .16.2Aircraft Paint and Graphics - Single Engine Piston Aircraft .16.3McCauley Propeller Systems Standard Limited Warranty .16.4OEM Aircraft Engine Warranty .16.5Garmin Avionics - Limited Warranty .FIGURE I — CESSNA TTx EXTERIOR DIMENSIONS .FIGURE II — CESSNA TTx INTERIOR DIMENSIONS .FIGURE III — CESSNA TTx INSTRUMENT PANEL ber 2015, Revision D

CESSNA TTx1. GENERAL DESCRIPTION1. GENERAL DESCRIPTIONAll information herein applies to the TTx Model T240.The TTx Model T240 is a pre-molded, composite built,semi-monocoque, four seat, single engine, low wing, tricycle design airplane. Suitable allowance for luggage isprovided.1.1 CERTIFICATIONThe TTx Model T240 is certified to the requirements ofU.S. Federal Aviation Regulation Part 23 through amendment 23-46, including day, night, VFR and IFR. The aircraftis approved for flight-into-known-icing when equippedwith the appropriate options.December 2015, Revision D3

CESSNA TTx1. GENERAL DESCRIPTION(CONTINUED)14 ft 3 in35 ft 10 in25 ft 4 in9 ft 0 inFIGURE I — CESSNA TTx EX TERIOR DIMENSIONS4December 2015, Revision D

CESSNA TTx1. GENERAL DESCRIPTIONFirewall49 in(124.5 cm)(CONTINUED)35 in(87.65 cm)Baggage Shelf140 in(354.6 cm)Firewall49 in(124.5 cm)39 in(97.8 cm)BaggageShelf28 in(71.1 cm)FIGURE II — CESSNA TTx INTERIOR DIMENSIONSDecember 2015, Revision D5

CESSNA TTx1. GENERAL DESCRIPTION(CONTINUED)1.2 APPROXIMATE DIMENSIONSOverall Height . 9 ft 0 in (2.74 m)Overall Length . 25 ft 4 in (7.74 m)WINGSpan (overall) . 35 ft 10in (10.92 m)Area . 141.2 ft2 (13.1 m2)CABIN INTERIORHeight (maximum) . 49 in (124.5 cm)Width (maximum) . 49 in (124.5 cm)Length (firewall to aft limit of baggage compartment) . 140 in (354.6 cm)CABIN DOORMinimum Entry Width . 33 in (83.8 cm)Minimum Entry Height . 33 in (83.8 cm)Minimum Entry Clearance . 46 in (116.8 cm)BAGGAGE COMPARTMENTMaximum Baggage Compartment Width .39 in (97.8 cm)Maximum Baggage Compartment Length . 52 in (132 cm) (Including shelf)Maximum Baggage Compartment Height . 35 in (87.6 cm)Maximum Baggage Entry Width . 28 in (71.1 cm) (Diagonal Measurement)1.3 DESIGN WEIGHTS AND CAPACITIESMaximum Ramp Weight . 3,600 lb (1,633 kg)Maximum Takeoff Weight . 3,600 lb (1,633 kg)Maximum Landing Weight . 3,420 lb (1,551 kg)Standard Empty Weight . 2,534 lb (1,149 kg)Maximum Useful Load . 1,066 lb (484 kg)Baggage Allowance . 120 lb (54.4 kg)FUEL CAPACITYTotal Capacity . 106 gal (401 L)Total Useable . 102 gal (386 L)Total Capacity (each tank) . 53 gal (201 L)OIL CAPACITYSump . 8 qts (7.6 L)Total Capacity . 10 qts (9.5 L)6December 2015, Revision D

CESSNA TTx2. PERFORMANCEAll estimated performance data are based on airplane weights at 3,600 pounds; standard atmospheric conditions; level, hardsurface, dry runways; and no wind. They are calculated values derived from flight tests under carefully documented conditions and will vary with individual airplanes, pilots, and numerous other factors affecting flight performance.Service Ceiling . 25,000 ftTakeoff Distance Ground Roll (S.L.) . . . . 1,300 ftTakeoff Distance To Clear 50 ft. Obstacle (S.L.) . 1,900 ftMaximum Climb Rate (S.L., ISA, MTOW) . 1,400 fpmMaximum Cruise Speed (85% at 25,000 ft) . 235 kts / 270 mphEconomy Cruise Speed (55% at 25,000 ft) . 208 kts / 239 mphRange at Max Cruise Speed (85% at 25,000 ft) . 825 nmRange at Economy Cruise Speed (55% at 25,000 ft) . 1,250 nmLanding Distance Ground Roll (S.L., at Max Landing Weight 3,420 lb) . 1,250 ftLanding Distance To Clear 50 ft. Obstacle (S.L., at Max Landing Weight 3,420 lb) . 2,600 ft3. POWERPLANT & ACCESSORIES Continental Motors TSIO-550-C Engine310 HP @ 2600 RPMTwin Turbo-Charged / Twin IntercoolersCertified for 100LL & 100 FuelFuel Injection SystemHigh-Pressure Wet-Sump Oil SystemOil CoolerDual IntercoolersBleed Air HeatInduction Air FilterFull Flow Oil FilterThrottle Control - VernierMixture Control - VernierPropeller Control - VernierDual Ignition SystemConstant Speed, 3 Blade Metal Propeller with BladeHeatersDecember 2015, Revision D Propeller GovernorPropeller Spinner, PolishedElectric Starter7

CESSNA TTx4. TTx EQUIPMENT LISTThe following list of equipment is included on the standard aircraft and does not reflect optional equipment.Intrinzic Cockpit powered by Garmin 8GMA-36 Remote Digital Audio Panel w/MarkerBeacon/IntercomGTC-570 Touch Screen ControllerGTX-33ES Transponder-Mode S, w-Traffic InformationSystem capabilityGIA-63W NAV/COM/GPS/WAAS w/GS #1GIA-63W NAV/COM/GPS/WAAS w/GS #2GDU-1400 Primary Flight Display (PFD)GDU-1400 Multi-Function Display (MFD)GEA-71 Engine/Airframe ComputerGRS-77 AHRS (dual)GDC-74A Air Data Computer w/OAT ProbeGMU-44 Magnetometer (dual)GCU-275 Primary Flight Display (PFD) ControllerElectronic ChecklistGFC-700 Autopilot Go-Around Switch Electric Trim A/P Disconnect Control Stick Steering ButtonGMC-720 Auto Flight Controller System (AFCS)Garmin SafeTaxi & FliteCharts (FliteCharts do not provide Geosynchronous Positioning)ESI-1000 L-3 Trilogy (Backup Airspeed, Altimeter andAttitude (Electric) Indicator)Control Stick Push-To-Talk Switch-Pilot/CopilotMic & Phone Jacks-Pilot/Copilot/Passengers (Boseand Standard)Antennas: Marker Beacon Antenna Transponder Antenna WAAS/COMM Antenna (1) GPS (1) COMM Antenna (1) NAV Antenna TAS Omni (1) TAS Directional (1)Artex ELT-ME406 Emergency Locator TransmitterPitot System - HeatedStatic SystemAlternate Static SourceCO Detector/Pulse Oximeter Synthetic Vision Technologies (SVT) - Garmin Synthetic Vision utilizes GPS-based graphic technologyproviding virtual depiction of terrain and water features, complete with obstacles and airborne traffic,in 3-D perspective that allows pilots enhanced visualcues and improved situational awareness regardlessof meteorological or lighting conditions.Electronic Stability Protection (ESP) Garmin - Electronic monitoring and exceedance-correcting systemthat operates in the background, in concert with theautopilot. Assists the pilot in maintaining the aircraft ina safe, flight-stable condition, helping to prevent theonset of stalls/spins, overspeeds, steep spirals or other loss of control conditions should the pilot becomedistracted, disorientated or incapacitated during flight.December 2015, Revision D

CESSNA TTx5. INSTRUMENTATIONFIGURE III — CESSNA TTx INSTRUMENT PANELDecember 2015, Revision D9

CESSNA TTx6. ELECTRICAL POWER Belt Driven Alternator, 28 Volts, 70 amps max designratingGear Driven Alternator, 28 Volts, 60 amps max designratingDual 28 Volt, 8.5 AH BatteriesDual Voltage Regulators, 28 VoltCross-Tie ability during alternator failureCold Weather starting ability with either Battery orboth BatteriesBattery Charging Circuit Digital Display of the Battery amps, Alternator amps,and BUS voltages on MFDOverhead Master Switch PanelDual 12 Volt, 2 amp Auxiliary Power OutletsExternal Ground Power Plug7. ENGINE INDICATING SYSTEM AmmeterVoltmeterManifold PressureOil Pressure and TemperatureTachometer - Hour RecorderFuel Flow (GPH)Cruise % Power LH/RH Fuel QuantityCHT - Cylinder Head Temperature (6)EGT - Exhaust Gas Temperature (6)TIT - Turbo Inlet Temperature (2)Annunciation – Caution and Warning Alerts (PFD) Defrosting SystemInsulation / SoundproofingCO Detector/Pulse Oximeter8. ENVIRONMENTAL 10Integrated Environmental Control System (ECS)Built in Oxygen (4 Places)Individual Eyeball VentsFloor Vent SystemDecember 2015, Revision D

CESSNA TTx9. EXTERIOR Composite StructureLH and RH Gull Wing Style Doors w/Lock and KeyRemote Keyless Entry with Automatic Light SystemPneumatic Door Seal SystemLH Cargo Door, w/Lock and KeyFixed Landing Gear w/castering Nose WheelLighted Entrance StepEntry Assist and Exit HandlesMain Gear FairingsNose Gear and Strut FairingsTie Down Rings, LH/RH Wing & Tail Jack Adapters (2)Tube Type Tires Nose – 5.00 X 5 Mains - 15x6.00 X 6Static Wicks (9)Emergency Exterior Door ReleaseRear Tinted Passenger WindowsTitanium Leading Edges10. EXTERIOR LIGHTS Position, LH/RH Wing TipWing Tip Strobe, LH/RHTaxi Lights, LH Wing - HIDLanding Light - HID11. FLIGHT CONTROLS Dual Hydraulic Brakes, Toe-OperatedParking BrakeDual Flight Controls - Aileron/Elevator/RudderLH/RH Control Sticks, All Purpose Pilot/CopilotSpeedbrake Go-Around SwitchElectric Elevator/Aileron TrimRudder Hold SystemCarbon Fiber Control Surfaces Fuel Strainer, Incorporated with Fuselage Quick DrainFuel Sampler CupFuel Vapor Suppression System12. FUEL SYSTEM Electric Auxiliary Fuel PumpEngine Driven Fuel PumpIntegral Wet Wing Fuel Tanks, 102 Gal. UsableFuel Selector Valve, Left//Right/OffDecember 2015, Revision D11

CESSNA TTx13. INTERIOR Intuitive design, comfortable seating and qualityleathers. Four distinct, attractive interior selectionsavailable.Controllable Air Vents (6)Reclining Front Sport SeatsRear Seat and Seatback CushionPilot’s and Copilot’s Three Point Restraint SystemRear Seat Passengers Three Point Restraint SystemBaggage Tie Downs and Restraining NetFire Extinguisher and Mounting BracketPilot’s Check ListPilot’s Operating Handbook Instrument Panel GlareshieldRosen Sun VisorsCenter Console Storage AreaRadio Call PlateConsole Headset HangerRear Passenger Entry/Exit Assist StrapPilot

C ESSNA TTx SPECIFICATION AND DESCRIPTION UNITS 2096 TO TBD DECEMBER 2015 REVISION D Cessna