Transcription
'Deechcraft Bonanza C35Pilot's Operating HandbookandFAA Approved Airplane Flight ManualFAA Approved in Utility Category based on CAR 3. This documentmust be carried in the airplane at all times and be kept within reachof the pilot during all flight operations.This handbook includes the material required to be furnished to thepilot by CAR 3.Airplane Serial Number:This handbook supersedes all BEECH published owner's manuals,flight manuals, and check lists issued for this airplane with theexception of FAA Approved Airplane Flight Manual Supplements.COPYRIGHT BEECH 1994P/N 35-590057-97Issued: January, 1977P/N 35-590057-97 A4Revised: July, 1994
Published ByRAYTHEON AIRCRAFT COMPANYP.O. Box85Wichita, Kansas 67201U.S.ANOTEWhere Beech Aircraft Corporationor Beechcraftis referredto in thispublication, it will be taken to read RaytheonAircraftCompany. ------EXPORTSTATEMENTExportedunder the authorityof license exception:TSU."Thesecommodities,technologyor softwarewere exportedfrom theUnited States in accordancewith o U.S. law prohibited."RaylheanRaytheonAirc:raftCompany8M mbw·ulCAMI.( n11"'HI "-V1NlmnGAMA Mr,,uloclu10r As.ocl.llcn
ay111ean AircraftBonanza C35Log of TemporaryChangesto thePIiot"sOperating HandbookandFAA Approved Alrplane Flight ManualP/N 35-590057-97Changes to this Pilot's Operating Handbook and FAA ApprovedAirplane Fl/ght Manus/ must be In the airplane for ail flightoperations.Part onDatePlacard 8/26/97Note: This page should be filed In the front of the Pilot's OperatingHandbook and FAA Approved Airplane Flight Manus/ Immediately following the Title page. This page replaces any Log of TemporaryChanges page dated prior to the date In the lower right corner of thispage.1 of 1August 28, 1997
BONANZAC35PILOT'S OPERATINGHANDBOOKANDFAA APPROVEDAIRPLANEFLIGHT MANUALA4 Revision.July, 1994LOG OF REVISIONSPageDescription·:·-Title PageUpdatedPage A (A4)New10-1 thru10-48Revised Section X, Safetylnfonnation (May, 1994) PAGEA
BONANZA C35PILOT'S OPERATING HANDBOOKANDFAA APPROVED AIRPLANE FLIGHT MANUALA3 Revision.October, 1990LOG OF REVISIONSPageDescriptionTitle PageUpdatedPage A (A3)New10-1 thru10-48Revised Section X,Safety Information (October, 1990) PAGE A
Bonanza C35Pilot's Operating HandbookandFAA Approved Airplane Flight ManualA2 .MARCH 1987LOG OF REVISIONSPageDescriptionTitle PagePage A (A2)2-7UpdateNewRevise "WEIGHT AND CENTER OFGRAVITY" and "CG LIMITS"Add "WARNING" PlacardUpdate Table of ContentsAdd "WARNING"Shift Material2-226-16-4 & 6-56-66-8A, 6-8B,6-BC & 6-BDAdd "SAMPLE LOADINGS" Page A
Bonanza C35Pilot's Operating HandbookandFAA Approved Airplane Flight ManualAl .March 1983LOG OF REVISIONSPAGESTitle PageLogo PagePage A (A1)Page A (Orig)a&b1-11-3 & 1-41-4A & 1-4B1-51-6 & 1-6B2-82-16A, 2-17,2-20 & 2-213-13-73-83-9 & 3-104-14-6A, 4-7 &4-87-17-6 & 7-6A8-22, 8-22A& 8-2288-37, 8-38, 8-38A& 8-38BDESCRIPTIONUpdateAddNewUpdateRevise "Introduction"and Add "Warning"Update Table of ContentsRevise "ImportantNotice" and "Use ofthe Handbook"Revise "NOTE"Revise "Revising the Handbook"Add "Airplane Flight Manual SupplementsRevision Record", "Vendor-Issued STCSupplements", Shift Material and Add"Wing Area"Revise "Approved Maneuvers"Revise "Placards" and Shift MaterialUpdate Table of ContentsRevise "Landing Gear Manual Extension"Revise "Emergency Landing"Revise "Emergency Exits", "EmergencySpeed Reduction" and Shift MaterialUpdate Table of ContentsRevise "Starting" and "Before Takeoff"and Shift MaterialUpdate Table of ContentsRevise "Openable Cabin Windows", Add"Emergency Exits" and Shift MaterialRevise "Cleaning - Exterior PaintedSurfaces"Revise "Consumable Materials"IA1Page A
BONANZA C35PILOT'S OPERATING HANDBOOKandFAA APPROVED AIRPLANE FLIGHT MANUALLOG OF REVISIONS EFFECTIVE PAGEORIGINAL .ISSUEOR nalTitle Page"A" Pagea and b1-1 thru 1-162-1 thru 2-223-1 thru 3-104-1 thru 4-125-1 th ru 5-306-1 thru 6-207-1 thru 7-368-1 thru 8-46Section IXRevision10-1 thru 10-67JANUARY 1977DESCRIPTIONOF REVISIONSee Log ofSupplementsMarch 1981IAPage A
C35 BonanzaINTRODUCTIONThis Pilot's Operating Handbook and FAA Approved Airplane Flight Manual is in the format and contains datarecommendedin the GAMA (General Aviation Manufacturers Association) Handbook Specification Number 1Use of this specification by all manufacturerswill providethe pilot the same type data in the same place in all of thehandbooks.In recent years, BEECHCRAFT handbooks contained mostof the data now provided, however, the new handbookscontain more detailed data and some entirely new data.For example, attention is called to Section X SAFETY INFORMATION. BEECHCRAFT feels it is highly important to haveSAFETY INFORMATION in a condensed form in the handsof the pilots The SAFETY INFORMATION should be readand studied. Periodic review will serve as a reminder ofgood piloting techniques.WARNINGUse only genuine BEECH CRAFT or BEECH CRAFT approvedparts obtained from BEECHCRAFT approved sources, inconnection with the maintenanceand repair of Beechairplanes.Genuine BEECHCRAFT parts are produced and inspectedunder rigorous procedures to ensure airworthinessandsuitability for use in Beech airplane applications.Partspurchased from sources other than BEECHCRAFT, eventhough outwardly identical in appearance, may not havehad the required tests and inspections performed, may bedifferent in fabrication techniques and materials, and maybe dangerous when installed in an airplane.Revised: March 1983a
C35 BonanzaSalvaged airplane parts, reworked parts obtained from nonBEECHCRAFT approved sources, or parts, components, orstructuralassemblies,the service history of which isunknown or cannot be authenticated,may have beensubjected to unacceptable stresses or temperatures or haveother hidden damage, not discerniblethrough routinevisual or usual nondestructive testing techniques This mayrender the part, component or structural assembly, eventhough originally manufacturedby BEECHCRAFT, unsuitable and unsafe for airplane use.BEECHCRAFT expressly disclaims any responsibilityformalfunctions,failures, damage or injury caused by use ofnon-BEECHCRAFT approved parts.TABLE OF CONTENTSSECTION I .SECTION II, .General.SECTION IllLimitationsEmergencySECTION IVSECTION VSECTION VINormal Procedures., .PerformanceWeight and Balance/EquipmentSECTION VII .SECTION VIIIProceduresHandling,SECTION IX .ListSystems DescriptionServicingand MaintenanceSupplementsSECTION X ., . Safety InformationbRevised: March 1983
BEECHCRAFTBonanza C35SECTIONIGENERALTABLE OF CONTENTSSUBJECTImportant Notice .Use of the Handbook .Revising the Handbook .Airplane Flight ManualSupplements Revision Record .Vendor-Issued STC Supplements.Airplane Three View . . . . . . . . . . . . . . . . . . . . . . . . . . . .Descriptive Data .Engine .Propeller .Fuel .Oil Capacity .Weights.Cabin Dimensions.Baggage .Specific Loadings .General Airspeed Terminology and Symbols .Meteorological Terminology .Power Terminology .Engine Controls and Instruments.Airplane Performance and FlightPlanning Terminology.Weight and Balance Terminology .Revised: March 1983PAGE1-31-41-51 -61-61-6B1 -71-71 -71 -81 -81-81 -81 -81-91-91-111-121-121-131-141-1
BEECHCRAFTBonanzaC35Section IGeneralINTENTIONALLY1-2LEFT BLANKJanuary 1977
BEECHCRAFTBonanza C35Section IGeneralTHANK YOU .for displaying confidencein us byselecting a BEECHCRAFT airplane. Our design engineers,assemblers and inspectors have utilized their skills andyears of experienceto ensure that the BEECHCRAFTBonanza meets the high standards of quality and performance for which BEECHCRAFT airplanes have becomefamous throughout the worldIMPORTANTNOTICEThis handbook must be read carefully by the owner andoperator in order to become familiar with the operation ofthe BEECH CRAFT Bonanza The handbook presents suggestions and recommendationsto help obtain safe andmaximum performance without sacrificing economy. TheBEECHCRAFT Bonanza must be operated according to thePilot's Operating Handbook and FAA Approved AirplaneFlight Manual, and/or placards located in the airplane.As a further reminder, the owner and operator of thisairplane should also be familiar with the Federal AviationRegulations applicable to the operation and maintenance ofthe airplane and FAR Part 91 General Operating and FlightRules. Further, the airplane must be operated and maintained in accordance with FAA AirworthinessDirectiveswhich may be issued against it.The Federal Aviation Regulations place the responsibilityfor the maintenance of this airplane on the owner and theoperator who must ensure that all maintenance is done byqualified mechanics in conformity with all airworthinessrequirements established for this airplane.All limits, procedures, safety practices, time limits, servicing,and maintenance requirements contained in this handbookare considered mandatory for the continued airworthinessRevised: March 1983.1-3
Section IGeneralBEECHCRAFTBonanza C35of this airplane,manufacture.in a conditionequal to that of its originalIAuthorized BEECHCRAFT Aero or Aviation Centers or International Distributors or Dealers can provide recommendedmodification, service, and operating procedures issued byboth FAA and Beech Aircraft Corporation,which aredesigned to get maximum utility and safety from thisairplane.USE OF THE HANDBOOKIThe Pilot's Operating Handbook is designed so that necessary documents may be maintained for the safe andefficient operation of the BEECHCRAFT Bonanza Thehandbook has been prepared in loose leaf form for ease inmaintenance and in a convenient size for storage. Thehandbook has been arranged with quick reference tabsimprinted with the title of each section and contains tenbasic IIXXGeneralLimitationsEmergency ProceduresNormal ProceduresPerformanceWeight and Balance/EquipmentListSystems DescriptionHandling, Servicing and MaintenanceSupplementsSafety InformationRevised: March 1983
BEECHCRAFTBonanza C35Section IGeneralNOTEExcept as noted, all airspeeds quoted in thishandbook are Indicated Airspeeds (IAS) and assume zero instrument error.In an effort to provide as complete coverage aspossible, applicable to any configuration of theairplane, some optional equipment has beenincluded in the scope of the handbook. However, due to the variety of airplane appointments and arrangementsavailable, optionalequipment described and depicted herein maynot be designated as such in every case.The following information may be provided tothe holder of this manual automatically:1. Original issues and revisions of Class I andClass II Service Instructions2. Original issues and revisions of FAA Approved Airplane Flight Manual Supplements3. Reissues and revisions of FAA ApprovedAirplane Flight Manuals, Flight Handbooks,Owner's Manuals, Pilot's Operating Manuals, and Pilot's Operating HandbooksThis service is free and will be provided only toholders of this handbook who are listed on theFAA Aircraft Registration Branch List or theBEECHCRAFT InternationalOwners Notification Service List, and then only if listed by airplane serial number for the model for whichthis handbook is applicable. For detailed information on how to obtain "Revision Service"Revised: March 19831-4A
Section IGeneralBEECHCRAFTBonanza C35applicable to this handbook or other BEECHCRAFT Service Publications, consult a BEECHCRAFT Aero or Aviation Center, InternationalDistributor or Dealer, or refer to the latestrevision of BEECHCRAFT Service InstructionsNo. 0250-010.BEECH AIRCRAFTCORPORATIONEXPRESSLY RESERVES THE RIGHT TO SUPERSEDE, CANCEL, AND/ORDECLARE OBSOLETE, WITHOUT PRIOR NOTICE, ANY PART,PART NUMBER, KIT OR PUBLICATION REFERENCED IN THIS HANDBOOK.The owner/operatorshould always refer to allsupplements, whether STC Supplements orBeech Supplements, for possible placards, limitations, normal, emergency and other operational procedures for proper operation of theairplane with optional equipment installed.1-4BRevised: March 1983
Section IGeneralBEECHCRAFTBonanza C35REVISING THE HANDBOOKImmediatelyfollowingthe title page is the "Log ofRevisions" page(s). The log of Revisions pages are used formaintaining a listing of all effective pages in the handbook(except the SUPPLEMENTS section), and as a record ofrevisions to these pages. In the lower right corner of theoutlined portion of the Log of Revisions is a box containing acapital letter which denotes the issue or reissue of thehandbook. This letter may be suffixed by a number whichindicates the numerical revision. When a revision to anyinformationin the handbook is made, a new Log of Revisions will be issued. All Logs of Revisions must be retained in the handbook to provide a current record of material status until a reissue is made.WARNINGWhen this handbook is used for airplane operational purposes, it is the pilot's responsibility tomaintain it in current status.Revised: March 19831-5
BEECHCRAFTBonanza C35Section IGeneralAIRPLANE FLIGHT MANUALSUPPLEMENTS REVISION RECORDSection IX contains the FAA Approved Airplane FlightManual Supplements headed by a Log of Supplementspage. On the "Log" page is a listing of the FAA ApprovedSupplemental Equipment available for installation on theairplane. When new supplements are received or existingsupplements are revised, a new "Log" page will replace theprevious one, since it contains a listing of all previousapprovals, plus the new approval. The supplemental material will be added to the grouping in accordance with thedescriptive listing.NOTEUpon receipt of a new or revised supplement,compare the "Log" page just received with theexisting "Log" page in the manual. Retain the"Log" page with the latest date on the bottom ofthe page and discard the other log.VENDOR-ISSUEDSTC SUPPLEMENTSWhen a new airplane is delivered from the factory, thehandbook delivered with it contains either an STC (Supplemental Type Certificate) Supplement or a Beech FlightManual Supplement for every installed item requiring asupplement. If a new handbook for operation of the airplaneis obtained at a later date, it is the responsibilityof theowner/operatorto ensure that all required STC Supplements (as well as weight and balance and other pertinentdata) are transferred into the new handbook.1-6Revised: March 1983
BEECHCRAFTBonanzaC35INTENTIONALLYRevised: March 1983Section IGeneralLEFT BLANK1-6A
Section IGeneralBEECHCRAFTBonanza C35t c --- '--10'1-5;8"II\WING AREA177.6 sq. ft.\I\ J !· ---32'9-7;8"----------- t9-1/2"f.- 9' 7-1;8"1-6B---1Revised: March 1983
BEECHCRAFTBonanza C35Section IGeneralDESCRIPTIVE DATAENGINEThe BEECHCRAFT Bonanza C35 is powered by aContinental E-185-11 (serial 5122D and above) sixcylinder, horizontallyopposed engine rated at 205horsepower at 2600 rpm for take-off (max. 1 min) and 185hp at 2300 rpm maximum continuous operation.NOTEOther engines are approved for this modelBonanza but not installed as original equipment. These are listed in the FAA AircraftSpecificationA- 777 or approved by Supplemental Type Certificate.PROPELLERBeech electrically controlled variable pitch, two blade, 88inch diameter propeller with Beech pitch control motor andspinner. The propeller uses a Beech 215-109 hub with215-207-88 blades.ORBeech electric constant speed two blade, 88 inch diameterpropeller using Beech 215-107 hub and 215-207-88blades.NOTEOther propellers are approved for this modelBonanzabut not installedas originalequipment. These are listed in the FAA AircraftSpecification A- 777 or approved by Supplemental Type Certificate.January 19771-7
Section IGeneralBEECHCRAFTBonanza C35FUELAviation Gasoline 80/87 (red) minimum grade or alternategrades 100LL (blue) or 100/130 (green). See EngineManufacturer'sBulletin.Standard fuel system: Two 20-gallon tanks in wings. Total34 gallons usable.Optional fuel system: Two 20 gallon main tanks in wingsand either one 10 gallon or one 20 gallon auxiliary tank installed in the baggage compartment. All of the capacity ofthe 10 gallon tank is usable. The 20 gallon tank adds 19gallons usable fuel to the system.OIL CAPACITYThe oil capacity is 10 quarts.WEIGHTSMaximumMaximumMaximumRamp Weight.2710 lbsTake-Off Weight . . . . . . . . . . . . . . 2700 lbsLanding Weight . . . . . . . . . . . . . . 2700 lbsCABIN DIMENSIONSLength .6 ft 11Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 ft 2Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 ft 6Entrance Door .36 in. x 37in.in.in.in.BAGGAGEVolume . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 6.5 cu ftCapacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 270 lbsBaggage Door . . . . . . . . . . . . . . . . . 22.5 in. x 18.5 in.1-8January 1977
BEECHCRAFTBonanzaC35Section IGeneralSPECIFIC LOADINGSWing Loading . . . . . . . . . . . . . . . . . . . . . . 15.2 lbs/sq ftPower Loading . . . . . . . . . . . . . . . . . . . . . . . 13.2 lbs/hpGENERAL AIRSPEED TERMINOLOGYAND SYMBOLSCASCalibrated Airspeed is the indicated speedof an airplane, corrected for position andinstrument error. Calibrated airspeed is equalto true airspeed in standard atmosphere atsea level.GSGround Speed is the speed of an airplanerelative to the ground.IASIndicated Airspeed is the speed of an airplaneas shown on the airspeed indicator whencorrected for instrument error. IAS valuespublished in this handbook assume zeroinstrument error.KCAS Calibrated Airspeed expressed in "knots".KIASIndicated Airspeed expressed in "knots".TASTrue Airspeed is the airspeed of an airplanerelative to undisturbed air which is the CAScorrected for altitude, temperature, andcompressibility.VAManeuvering Speed is the maximum speedat which application of full available aerodynamic control will not overstress theairplane.January 19771-9
Section IGeneralBEECH CRAFTBonanzaC35VFEMaximum Flap Extended Speed is the highestspeed permissible with wing flaps in a prescribed extended position.VLEMaximum Landing Gear Extended Speed isthe maximum speed at which an airplanecan be safely flown with the landing gearextended.VLOMaximum Landing Gear Operating Speed isthe maximum speed at which the landinggear can be safely extended or retracted.VNENever Exceed Speed is the speed limit thatmay not be exceeded at any time.VNoor VeMaximum Structural Cruising Speed is thespeed that should not be exceeded exceptin smooth air and then only with caution.VsStalling Speed or the minimum steady flightspeed at which the airplane is controllable.VsoStalling Speed or the minimum steady flightspeed at which the airplane is controllablein the landing configuration.VxBest Angle-of-Climb Speed is the airspeedwhich delivers the greatest gain of altitudein the shortest possible horizontal distance.VyBest Rate-of-Climb Speed is the airspeedwhich delivers the greatest gain in altitudein the shortest possible time.1-1 0January 1977
BEECHCRAFTBonanzaC35Section IGeneralMETEOROLOGICAL TERMINOLOGYISAInternational Standard Atmosphere in which(1) The air is a dry perfect gas;(2) The temperature at sea level is 15 Celsius (59 Fahrenheit);(3) The pressure at sea level is 29.92inches Hg. (1013.2 millibars);(4) The temperature gradient from sealevel to the altitude at which thetemperature is -56.5 C (-69.7 F)is -0.00198 C (-0.003566 F)per foot and zero above that altitude.OATOutside Air Temperature is the free airstatic temperature, obtained either frominflight temperature indications adjustedfor instrument error and compressibilityeffects, or ground meteorological sources.IndicatedPressureAltitudeThe number actually read from analtimeter when the barometric subscale has been set to 29.92 inches ofmercury (1013.2 millibars).PressureAltitudeAltitude measured from standardsea-level pressure (29.92 in. Hg) bya pressure or barometric altimeter.It is the indicated pressure altitudecorrected for position and instrumenterror. In this Handbook, altimeterinstrument errors are assumed to bezero. Position errors may beobtained from the AltimeterCorrection Chart.StationPressureActual atmospheric pressure at fieldelevation.January 19771-11
BEECHCRAFTBonanza C35Section IGeneralWindThe wind velocities recorded asvariables on the charts of this handbook are to be understood as the headwind or tailwind components of thereported winds.POWER TERMINOLOGYTake offMaximum power rating,limited by time.MaximumContinuousHighest power ratingnot limited by time.CruiseClimbPower recommendedcruise climb.forENGINE CONTROLS AND INSTRUMENTSThrottleControlUsed to control power by introducing fuel-air mixture into theintake passages of the engine.Settings are reflected by readingson the manifold pressure gage.MixtureControlThis control is used to set fuel to airratio in all modes of operationand cuts off fuel completely forengine shut down.EGT(Exhaust GasTemperatureIndicator)This indicator is used to identifythe lean and best power fuel/air mixtures for various powersettings.TachometerIndicates the rpm of the engine/propeller.1-12January 1977
Section IGeneralBEECHCRAFTBonanza C35PropellerControlSwitchThis control is used to change thepropeller blade angle.AutomaticPropellerControl(APC)Regulates the rpm of the engine/propeller electrically by increasingor decreasing the propeller pitchthrough a pitch change mechanismin the propeller hub.AIRPLANE PERFORMANCE ANDFLIGHT PLANNING TERMINOLOGYClimbGradientThe ratio of the changein height during a portion of a climb,to the horizontal distance traversedin the same time interval.DemonstratedCrosswindVelocityThe demonstrated crosswind velocityis the velocity of the crosswind component for which adequate control ofthe airplane during take-off and landing was actually demonstrated duringcertification tests. The value shownis considered to be limiting.MEAMinimumRouteSegmentA part of a route. Each end of thatpart is identified by: (1) a geographical location; or (2) a point at whicha definite radio fix can be established.GPHU.S. Gallons per hour.PPHPounds per hour.January 1977enroute IFR altitude.1-13
Section IGeneralBEECHCRAFTBonanza C35WEIGHT AND BALANCE TERMINOLOGYReferenceDatumAn imaginary vertical plane fromwhich all horizontal distances aremeasured for balance purposes.StationA location along the airplane fuselageusually given in terms of distancefrom the reference datum.ArmThe horizontal distance from the reference datum to the center of gravity(C.G.) of an item.MomentThe product of the weight of an itemmultiplied by its arm. (Moment dividedby a constant is used to simplify balance calculations by reducing thenumber of digits.)AirplaneCenter ofGravity(C.G.)The point at which an airplane wouldbalance if suspended. Its distancefrom the reference datum is foundby dividing the total moment by thetotal weight of the airplane.C.G. ArmThe arm obtained by adding the airplane's individual moments anddividing the sum by the total weight.C.G. LimitsThe extreme center of gravity locations within which the airplane mustbe operated at a given weight.Usable FuelFuel available for flight planning.1-14January 1977
Section IGeneralBEECHCRAFTBonanzaC35UnusableFuelFuel remaining after a runout testhas been completed in accordancewith governmental regulations.StandardEmptyWeightWeight of a standard airplaneincluding unusable fuel, fulloperating fluids and full oil.BasicEmptyWeightStandard empty weight plusoptional equipment.PayloadWeight of occupants, cargo andbaggage.UsefulLoadDifference between take off weight,or ramp weight if applicable, andbasic empty weight.MaximumRampWeightMaximum weight approved for groundmaneuvering. (It includes weight ofstart, taxi, and run up fuel).MaximumTake-offWeightMaximum weight approved for thestart of the take off run.MaximumLandingWeightMaximum weight approved for thelanding touchdown.Zero FuelWeightWeight exclusive of usable fuel.January 19771-15
BEECHCRAFTBonanza C35Section IGeneralINTENTIONALLY1-16LEFT BLANKJanuary1977
BEECHCRAFTBonanza C35SECTION IILIMITATIONSTABLE OF CONTENTSSUBJECTPAGEAirspeed Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-3Airspeed Indicator Markings. . . . . . . . . . . . . . . . . . . . . 2-4Power Plant Limitations. . . . . . . . . . . . . . . . . . . . . . . . . 2-5Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5Oil .2-5Propeller .: . . . . . . . . . . . . . . . . . . . . . . . . . 2-5Power Plant Instrument Markings . . . . . . . . . . . . . . . . 2-6Oil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6Tachometer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6Cylinder Head Temperature. . . . . . . . . . . . . . . . . . 2-6Manifold Pressure .2-7Instrument Vacuum .2-7Fuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2- 7Weight and Center of Gravity . . . . . . . . . . . . . . . . . . . . 2- 7CG Limits (Gear Down) .2-7Approved Maneuvers (2700 Pounds) . . . . . . . . . . . . . 2-8Flight Load Factors (2700 Pounds) . . . . . . . . . . . . . . . 2-8Required Equipment for VariousConditions of Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-8Fuel .2-16Placards . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-16January 19772-1
Section EFT BLANKJanuary 1977
BEECHCRAFTSection IILimitationsBonanzaC35The limitationsincludedin this sectionhaveapproved by the Federal Aviation Administration.The followinglimitationsoperation of this airplane.mustbeobservedbeenintheAIRSPEED LIMITATIONSSPEEDCASIASKNOTS MPH KNOTS MPHNever ExceedVNE176MaximumStructuralCruisingVNO or VFEMaximumLanding GearOperating/ExtendedVLO and VLEJanuary 1977203177REMARKS204 Do not exceedthis speed inany operation160140161 Do not exceedthis speedexcept in smoothair and then onlywith caution130114131 Do not make fullor abrupt controlmovements abovethis speed9110592109125110106Do not extendflaps or operatewith flaps extended abovethis speed127 Do not extend,retract or operatewith landing gearextended abovethis speed exceptin emergency2-3
r-N'-·3en(I)-·.-·!:t. ::s II)000*AIRSPEED SMPHWhite Arc48-9155-10549-9256-106Full Flap Operating RangeGreen Arc57-13966-16057-14066-161Normal Operating RangeYellow Arc139-176160-203140-177161-204176203177204Red LineII) II) .(0.,.,SIGNIFICANCE*The Airspeed Indicator is marked in CAS valuesOperate with caution only insmooth airMaximumspeed for ALL operationsCDCD mo m::s (')::c: (')II)II)JJ(') l w "Tl0, -t
BEECHCRAFTBonanza C35Section IILimitationsPOWER PLANT LIMITATIONSENGINEContinentalE185-11 engineTake-off (one minute)Maximum continuous operation(S;N 5122D and above)Full Throttle, 2600 rpmFull Throttle, 2300 rpmNOTEOther engines are approved for this modelBonanza but not installed as original equipment. These are listed in the FAA AircraftSpecificationA- 777 or approved by Supplemental Type Certificate.FUELAviation Gasoline 80/87 (red) minimum grade or alternategrades 100LL (blue) or 100/130 (green). See EngineManufacturer's Bulletin.OILAshless dispersant oils must meet Continental MotorsCorporation Specification MHS-24A. Refer to APPROVEDENGINE OILS, Section 8, Servicing.PROPELLERBeech electrically controlled variable pitch, two blade propeller with Beech pitch control motor and spinner. The propeller uses a Beech 215-109 hub with 215-207-88 blades.Diameter: maximum 88 in., minimum 86 in.(prior to Engine Serials 22183)minimum 84 in.(Engine Serials 22183 and after)Pitch settings at 33 in. sta.: high not under 30 low 13 (Engine Serials prior to 22183)low 13-3/4 (Engine Serials 22183 and after)January 19772-5
Section IILimitationsBEECHCRAFTBonanzaC35ORBeech electric constant speed two blade propeller usingBeech 215-107 hub and 215-207-88 blades.Diameter is maximum 88 in . minimum 86 in. Pitchsettings at 33 in. sta.: low 12 , high not under 30 NOTEOther propellers are approved for this modelBonanza but not installedas originalequipment. These are listed in the FAA AircraftSpecification A- 777 or approved by Supplemental Type Certificate.POWER PLANT INSTRUMENTMARKINGSOIL TEMPERATURECaution (Yellow Radial) . . . . . . . . . . . . . . 100 F;38 COperating Range(Green Arc) . . . . . . . . 100 to 225 F;38 to 107 CMaximum (Red Radial) . . . . . . . . . . . . . . 225 F/107 COIL PRESSUREMinimum Pressure (Red Radial) .30 psiOperating Range (Green Arc) . . . . . . . . . 30 to 60 psiMaxi
visual or usual nondestructive testing techniques This may render the part, component or structural assembly, even though originally manufactured by BEECHCRAFT, unsuit . handbook has been prepared in loose leaf form for ease in maintenance and in a convenient size for storage. The handbook has been arranged with quick reference tabs .
