The Goodyear Tire & Rubber Co. 1144 East Market

Global Aviation TiresThe Goodyear Tire & Rubber Co.1144 East Market StreetAkron, Ohio 44316-0001, U.S.A.PH: 330/796-6306Fax: 2 2001, 2002. The Goodyear Tire & Rubber Company. All rights reserved.Effective Date 10/02Revised 10/02000000-10/02(005357)

contentsSection1INTRODUCTION. . . . . . . . . . . . . . . . . . . . . . . . . . . . 22DEFINITIONS AND ABBREVIATIONS . . . . . . . . . . 23QUALIFICATION SPECIFICATION . . . . . . . . . . . . . 44DATA SECTION – TIRESThree Part Name Sizes. . . . . . . . . . . . . . . . . . . . . . . 6Type I. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12Type III. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12Type VII . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18Metric And Radial . . . . . . . . . . . . . . . . . . . . . . . . . . 225DATA SECTION – TUBES AND VALVES5.1 Tube And Valve Technical Data. . . . . . . . . . . . . 245.2 Tube Valve Types And Technical Data . . . . . . . 266AIRCRAFT TIRES SERIAL NUMBER CODES6.1 All Commercial And Military . . . . . . . . . . . . . . . . 277APPLICATION CHARTS7.1 General Aviation/Business Aircraft. . . . . . . . . . . 287.2 Commercial Aircraft . . . . . . . . . . . . . . . . . . . . . . 327.3 Military Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . 357.4 International Military Aircraft. . . . . . . . . . . . . . . . 377.5 Commercial Rotary Wing Aircraft . . . . . . . . . . . 387.6 Military Rotary Wing Aircraft . . . . . . . . . . . . . . . 387.7 International Rotary Wing Aircraft . . . . . . . . . . . 388ENGINEERING AND TECHNICAL INFORMATION8.1 Tire Size Selection. . . . . . . . . . . . . . . . . . . . . . . 398.2 Inflation Under Load . . . . . . . . . . . . . . . . . . . . . 398.3 Tire Measurement Procedure . . . . . . . . . . . . . . 408.4 Operating Tire Temperatures. . . . . . . . . . . . . . . 408.5 Load Ratings Used For Helicopters. . . . . . . . . . 408.6 Radius Of Gyration . . . . . . . . . . . . . . . . . . . . . . 408.7 Aircraft Tire Dimensions And Deflection. . . . . . . 418.8 Growth And Minimum Clearance Allowance . . . 428.9 Aircraft Tire Operating Characteristics . . . . . . . . 448.10 Tubeless Tires In Place Of Tube Type Tires . . 44Notice: This Aircraft Tire Data Book effective 10/02 combines information from previousGoodyear Aircraft Tire Data Books and supercedes all previous manuals.1

section 1INTRODUCTIONGoodyear, founded in 1898, has been producing aircraft tires since 1909 and retreading aircraft tires since 1927.With more than 90 years in the aircraft tire business, Goodyear is the world’s largest supplier of aircraft tires.Goodyear aircraft tires have been selected as original equipment on virtually all current U.S. military aircraft.Type IIIType VIIGoodyear manufactures new tires in the United States, Brazil, and Thailand. Retreading facilities are located in theUnited States, Brazil, Thailand, the Netherlands and in Australia.Goodyear aircraft tires meet exacting specifications, are qualified to perform safely and economically, and hold upunder the stringent demands set forth by today’s high performance aircraft.Specific data on the proper tire sizes for different aircraft main and auxiliary/nose gear, speed ratings, nominalinflation pressures, dimensions, and other data needed by users to obtain the maximum service from their aircrafttires are presented in this booklet. Data are included for reference purposes for some tires that are not in theGoodyear authorized line. The data presented supersedes previously published Goodyear data.The data and general notes for civil aircraft tires are in accordance with The Tire & Rim Association Standards. Thecivil aircraft tire data also conform to Federal Aviation Agency Technical Standard Order C-62d, and other standardsas applicable.Ply RatingThe data for Military Aircraft are based on military specification MIL-PRF-5041J, unless otherwise indicated.The tire weights given in the Data Sheets are calculated weights on the basis of specifications in effect or contemplated at the time of publication. They are subject to change and are not to be construed as guaranteed weights.Loads shown are the recommended maximum for the indicated inflation. For loads less than maximum, the inflationpressure can be reduced proportionately.The physical tire data and applications herein are accurate to the best of our knowledge at the time of publication.For questions regarding specific applications, please contact your Goodyear aircraft tire distributor or the aircraftmanufacturer for current information.section 2TT or TLRated SpeedRated LoadRated InflationMaximumBraking LoadMaximumBottoming LoadPlantTread Design/TrademarkDEFINITIONS AND ABBREVIATIONSTIRE NAME SIZE CLASSIFICATIONThree Part TypeRadialMetric TypeType I2All new sizes being developed are in this classification. This group was developed tomeet the higher speeds and loads of today’s aircraft. NOTE: Some sizes have a lettersuch as “H” in front of the diameter. This is to identify a tire that is designed for a higherpercent deflection.Radial size nomenclature is the same as Three Part except an “R” replaces the “-”(dash) before the wheel/rim diameter.This size designation is the same as Three Part except the diameter and section widthdimensions are in millimeters, and the wheel/rim diameter is in inches.Oldest type/description giving outside diameter only.Part NumberWeightInflated DimensionsStatic Loaded RadiusFlat Tire RadiusAspect RatioWheelThis type was one of the earliest size designations used for early piston-prop typeaircraft. Its characteristic is low pressure for cushioning and flotation.This type covers most of the older sizes and was designed for today’s jet aircraft withits higher load capacity.TireNameTypeTire dth(Inches)NominalWheel/RimDiameter(Inches)Three PartMetricType IType IIIType )—10—16The term “Ply Rating” is used to identify a given tire with its maximum recommendedload when used in a specific type of service. It is an index of tire strength and does notnecessarily represent the number of carcass plies in the tire.Designates whether the tire is tube-type or tubeless construction.The maximum speed to which the tire is qualified.The maximum load rating in lbs.The rated inflation pressure required for the tire to support the rated load.The maximum steady braking load which may be applied to a tire.Approximate load required to bottom the tire on the rim at rated inflation pressure.The plant at which the tire was produced. *BRA – Brazil; DAN – Danville;*LUX – Luxembourg; THL – Thailand*Goodyear no longer manufactures aircraft tires in Luxembourg.RIB – RibFLC II – Flight Custom IISMO – SmoothFLC IIl – Flight Custom IIlAW – All WeatherFLS II – Flight Special IIG27 – Rib All WeatherFLDR – Flight LeaderDT – Deflector TypeFLRAD – Flight RadialDDT – Dual Deflector TypeRS700 – Red Streak 700FLE – Flight EagleTwin ContactThe part number assigned to the tire if applicable.Calculated weight of approved construction.The dimensions of a new tire inflated to rated inflation pressure.Loaded Radius is the distance from the center of the axle to the deflected treadsurface under normal load and inflation pressure.Flat Tire Radius is the distance from the center of the axle to the deflected tread surfacewhen subjected to bottoming load.Aspect Ratio is the ratio of tire section height to tire section width.The dimensions of the wheel on which the tire is to be used.3

section 3QUALIFICATION SPECIFICATIONBelow is a list of abbreviations used in following data ISWEVGTWESCommander Division Rockwell Intl.DassaultAerospatialeBritish Aircraft Corp.British AerospaceBeechBoeing Aircraft Corp.BombardierConstrucciones Aeronauticas SACessna Aircraft Co.General Dynamics – Convair Div.Douglas Aircraft Corp.DeHavilland Aircraft Co. Ltd.Dornier GmbHEmpresa Brasileria de Aeronautica SA (EMBRAER)FairchildFokkerGulfstreamGeneral Dynamics Corp.Grumman Corp.General Utility AircraftHandley PageHawker SiddeleyIsraeli Aircraft IndustriesAleniaKaman HelicoptersKawasaki Heavy Industries Ltd.Lockheed Aircraft Corp.Ling-Temco-Vought AeronauticalMartin s Corp.Mitsubishi Heavy Industries Ltd.North American RockwellNihonNorthrop Corp.PanaviaFairchildSikorsky AircraftSAAB Aircraft ABShortsSIA MarchettiSwearingenVoughtWestland FCFSAFC62bC62cC62dUSAFFrench Military of Armed Forces SpecMilitary Specification for Pneumatic TiresMilitary Specification for Navy Aircraft TiresRoyal Australian AirforceCanadian ForcesSwedish AirforceTechnical Standard Order – FAA (Rev-b)Technical Standard Order – FAA (Rev-c)Technical Standard Order – FAA (Rev-d)United States Air ForceLSTSCDT&RAULoad, Speed and Time CurveSpecification Control DocumentThe Tire and Rim AssociationUniversal LST Curve (TSO-C62d)5

section 4DATA SECTION – TIRESthree part name 75-106SERVICE RATINGINFLATED DIMENSIONS (IN)PLYRATINGTT OR MAXIMUMBRAKINGLOAD (LBS)MAXIMUMBOTTOMINGLOAD (LBS)TREADDESIGN/TRADEMARKPART 49002010020700Flight Eagle DTRib DTRibFlight Eagle DTRibRibFlight EagleFlight EagleFlight Eagle DDTFlight EagleFlight EagleRibFlight Custom IIFlight Special IIFlight Custom IIlFlight Custom IIRib DDTFlight Special IIFlight Special IISmoothRibRibRibRibRibRibRibFlight Leader DTRibRib DDTFlight EagleFlight LeaderFlight Custom IIlFlight Special IIRibRibRibFlight EagleRibFlight EagleFlight Eagle DTFlight Eagle DTFlight Eagle DTFlight LeaderRibRibRibFlight 0.925.425WHEEL (IN)STATIC FLATOUTSIDE DIA SECTION WIDTH SHOULDERLOADED TIREDIA WIDTH RADIUS RAD ASPECTMAX MIN MAX MINMAX MAX(IN)(IN) 1222x7.75-96.50-106.50-1025x7.75-10WIDTH SPECIFIEDMINBETWEENRIMFLANGE LEDGEFLANGES DIAMETER HEIGHT essna, DassaultRockwellHS, McDonnell-DouglasGUAGUAGUAEurocopterSniasPiper, chCanadairBeech, CessnaEmbraerC62cC62bC62cC62c16VL027-EGD 16VL036C62cC62cC62cC62cC62cUSN MILT MSC62cC62cC62cC62dC62cC62dC62cUSN KAMANUSAF 63J4242C62dC62dUSN MS14178USAF 84125685041GUSN MS14168C62dC62dC62dC62cEDD00046C62dC62dUSN 62dC62dC62c7

three part name sizesCONSTRUCTION8SERVICE RATINGINFLATED DIMENSIONS (IN)SIZEPLYRATINGTT OR MAXIMUMBRAKINGLOAD (LBS)MAXIMUMBOTTOMINGLOAD (LBS)TREADDESIGN/TRADEMARKPART 5150675006750067500675007180033600Rib DTFlight LeaderFlight Special IIFlight EagleFlight EagleRibRibRibRibFlight EagleFlight EagleRibFlight EagleRibRibRibFlight LeaderFlight LeaderRibFlight EagleFlight EagleRS-700Flight LeaderFlight LeaderFlight LeaderFlight LeaderRibRibRibRibSmoothFlight LeaderRibFlight LeaderFlight LeaderFlight LeaderFlight LeaderRibRibFlight EagleRibRibRibRibRibRibFlight Leader 6.566.474.272.461.1WHEEL (IN)STATIC FLATOUTSIDE DIA SECTION WIDTH SHOULDERLOADED TIREDIA WIDTH RADIUS RAD ASPECTMAX MIN MAX MINMAX MAX(IN)(IN) 0x11.5-14.530x11.5-14.530x11.5-14.532x11.5-15WIDTH SPECIFIEDMINBETWEENRIMFLANGE LEDGEFLANGES DIAMETER HEIGHT r, ShortsFokker, ShortsFokker, C62cC62cUSAF 73453CUSAF 16VL028USAF 61D3001EUSAFC62dC62dUSAF 63J4241FC62dC62cUSAF 16VL032USAF IAFUSAF 2dUSAFUSAFIAFCAFUSN MS14171USAF MS21781C62d9