Cessna. - Kirtland Flight Center

CESSNAMODEL R182vXSECTION 1GENERALBest Angle-of-Climb Speed is the speed which results inthe greatest gain of altitude in a given horizontal distance.Best Rate-of-Climb Speed is the speed which results in thegreatest gain in altitude in a given time.METEOROLOGICAL TERMINOLOGYOATOutside Air Temperature is the free air static temperature.It is expressed in either degrees Celsius (formerly Centigrade) or degrees Fahrenheit.StandardTempera·tureStandard Temperature is 15 C at sea level pressure altitude and decreases by 2 C for each 100(\ feet of altitude.PressureAltitudePressure Altitude is the altitude read irom an altimeterwhen the altimeter's barometric scale h,ts been set to 29.92inches of mercury (1013 mb).ENGINE POWER TERMINOLOGYBHPBrake Horsepower is the power de\-' oped by the engine.RPMRevolutions Per Minute is engineMPManifold Pressure is a pressure m .:::iUred in the engine'sinduction system and is expressec ill inches of mercury(Hg).S' ·c ed.AIRPLANE PERFORMANCE AND FLIGHT monstrated Crosswind Velocity is the velocity of thecrosswind component for which adequate control of theairplane during takeoff and landing was actually demonstrated during certification tests. The value shown is notconsidered to be limiting.Usable FuelUsable Fuel is the fuel available for flight planning.UnusableFuelUnusable Fuel is the quantity of fuel that can not be safelyused in flight.GPHGallons Per Hour is the amount of fuel (in gallons)consumed per hour.1-7

CESSNAMODEL R182SECTION 1GENERALNMPGNautical Miles Per Gallon is the distance (in nauticalmiles) which can be expected per gallon of fuel consumedat a specific engine power setting andl or flight configuration.gg is acceleration due to gravity.WEIGHT AND BALANCE TERMINOLOGYReferenceDatumReference Datum is an imaginary vertical plane fromwhich all horizontal distances are measured for balancepurposes.StationStation is a location along the airplane fuselage given interms of the distance from the reference datum.ArmArm is the horizontal distance from the reference datum tothe center of gravity (C.G.) of an item.MomentMoment is the product of the weight of an item multipliedby its arm. (Moment divided by the constant 1000 is used inthis handbook to simplify balance calculations by reducing the number of digits.)Center ofGravity(C.G.)Center of Gravity is the point at which an airplane, orequipment, would balance if suspended. Its distance fromthe reference datum is found by dividing the total momentby the total weight of the airplane.C.G.ArmCenter of Gravity Arm is the arm obtained by adding theairplane's individual moments and dividing the sum bythe total weight.C.G.LimitsCenter of Gravity Limits are the extreme center of gravitylocations within which the airplane must be operated at agiven weight.StandardEmptyWeightStandar1 Empty Weight is the weight of a standard airplane, including unusable fuel, full operating fluids andfull engine oil.Basic EmptyWeightBasic Empty Weight is the standard empty weight plus theweight of optional equipment.UsefulLoadUseful Load is the difference between ramp weight and thebasic empty weight.1-8

CESSNAMODEL R182SECTION 1GENERALMaximumRampWeightMaximum Ramp Weight is the maximum weight approvedfor ground maneuver. (It includes the weight of start, taxiand runup fuel.)Gross(Loaded)WeightGross (Loaded) Weight is the loaded weight of the airplane.MaximumTakeoffWeightMaximum Takeoff Weight is the maximum weightapproved for the start of the takeoff run.MaximumLandingWeightMaximum Landing Weight is the maximum weightapproved for the landing touchdown.TareTare is the weight of chocks, blocks, stands, etc. used whenweighing an airplane, and is included in the scale readings. Tare is deducted from the scale reading to obtain theactual (net) airplane weight.1-9/(1-10 blank)

CESSNAMODEL R182SECTION 2LIMITA TIONSSECTION 2LIMITATIONSTABLE OF CONTENTSPageIntroduction . . . . . . . .Airspeed LimitationsAirspeed Indicator MarkingsPower Plant LimitationsPower Plant Instrument MarkingsWeight Limits . . . . .Center Of Gravity Limits .Maneuver LimitsFlight Load Factor LimitsKinds Of Operation LimitsFuel 2-82-92-1/ (2-2 blank)

CESSNAMODEL R182SECTION 2LIMITATIONSINTRODUCTIONSection 2 includes operating limitations, instrument markings, andbasic placards necessary for the safe operation of the airplane, its engine,standard systems and standard equipment. The limitations included inthis section have been approved by the Federal Aviation Administration.When applicable, limitations associated with optional systems or equipment are included in Section 9.NOTEThe airspeeds listed in the Airspeed Limitations chart(figure 2-1) and the Airspeed Indicator Markings chart(figure 2-2) are based on Airspeed Calibration data shownin Section 5 with the normal static source. with theexception of the bottom of the green and white arcs on theairspeed indicator. These are based on a power-off airspeed calibration. If the alternate static source is beingused. ample margins should be observed to allow for theairspeed calibration variations between the normal andalternate static sources as shown in Section 5.Your Cessna is certificated under FAA Type Certificate No. 3A13 asCessna Model No. R182.2-3

CESSNAMODEL R182SECTION 2LIMITATIONSAIRSPEED LIMITATIONSAirspeed limitations and their operationalfigure 2-1.signifi( ance areshown inRI MAR KSKCASKIASSpef d175182Do not excetd this speed Inany operatlollMaximum Structural140143Do not excetd this speedexcept in smiJoth air, andthen only wih caution.1111008911210189Do not make full or abruptcontrol movements abovethis speed.1379414095Do not excetd these speedswith the give'l flap settings.Maximum L211ldlllg GearOperating Speed137140Do not extend or retract landirlljgear above this speed.MaximurT'. LdmJirlg GeCJr137140Do not exceed this speed withlanding gear extended175182Do 110t exceeJ this speed withwindows opell.SPEEDIV',\JEI[\Jevcr Exceed!IIV NOIIVAICru ISlrIlJ SpeedManeuveri ng Speed.3100 Pounds2550 Pounds2000 PoundsMaximum Flap ExtendedSpeedTo 10 0 FlapsV FE10 VLOV LEiI40 FlapsEx tended SpeedMaXimum Willdow OpellSpeedIIFigure 2-1. Airspeed LimitationsAIRSPEED INDICATOR MARKINGSAirspeed indicator markings and their color code significance areshown in figure 2-2.2-4

CESSNAMODEL R182SECTION 2LIMITATIONSrIKIA.S VALUE'v1ARt !r\Jl SIGNIFICANCEOR RANG[!IFUll Flap Operating ReJrlLJeLoweri37 - 95limit IS rT1CJXlmum weight VInii1.;:ldl::cJ lOl1 t iguratlorlIiISSoUpper 11I11,trndximurn speed perr 111ssible withflaps extcllded.Ir--------------- -------r-------------------I.]rcell Arr.42 - 143If\JorlT1dl OperatlricjRcll1CjlLuwer !ImitliS lrIiJXII11Urn weight V s cH most forW,Hdell With fidPS retracted. Upper IllTIltI'-----------I------------------- ) u(: dlT J l ,t J ris rrUX:fl UITI structural cru,s:rHj spel:dir------------- 1Iy,'I "mArli143- 182 ---------- :'::j"d LineI!WithI --------------------j182IIMcJxrlllurn speed for ail () H:rdtlonsFigure 2-2. Airspeed Indicator MarkingsPOWER PLANT LIMITATIONSEngine Manufacturer: A vco LycomingEngine Model Number: 0-540-J3C5D.Engine Operating Limits for Takeoff and Continuous Operations:Maximum Power: 235 BHP.Maximum Engine Speed: 2400 RPM.Maximum Cylinder Head Temperature: 260 C (500 C F).Maximum Oil Temperature: 118 C (245 coF).Oil Pressure. Minimum: 25 psi.Maximum: 100 psi.Fuel Pressure, Minimum: 0.5 psi.Maximum: 8.0 psi.Propeller Manufacturer: McCauley Accessory Division.Propeller Model Number: B2D34C214/90DHB-8Propeller Diameter. Maximum: 82 inches.Minimum: 80.5 inches.Propeller Blade Angle at 30 Inch Station, Low: 15.8 .High: 29.4 .2-5

SECTION 2LIMITATIONSCESSNAMODEL R182POWER PLANT INSTRUMENT MARKINGSPower plant instrument markings and their color code significanceare shown in figure 2-3.INSTRUMENTRED LINEGREEN ARCMINIMUMLIMITNORMALOPERATI NGTJchorneter--YELLOW ARCCAUTIONRANGE21002400 RPM- - -15-23in. Hg- - -Manifold Pressure---011 Temperature---100 - 245 F----200 - 500 F- -Cy II nder HeadTemperature-RED LINEMAXIMUMLIMIT2400 RPM----245 F-500 FFuel Pressure0.5 psi0.5 - 8.0 psi8.0 psi011 Pressure25 psi60 - 90 psi100 psiCar'buretor AirTemperature-- -- ---15 to SoC- --Figure 2-3. Power Plant Instrument MarkingsWEIGHT LIMITSMaximum Takeoff Weight: 3100 lbs.Maximum Landing Weight: 3100 lbs.Maximum Weight in Baggage Compartment:Baggage Area "A" (or passenger on child's seat) - Station 82 to 110: 120lbs. See note below.Baggage Area "B" - Station 110 to 134: 80 lbs. See note below.NOTEThe maximum combined weight capacity for baggageareas A and B is 200 lbs.2-6

CESSNAMODEL R182SECTION 2LIMITATIONSCENTER OF GRAVITY LIMITSCenter of Gravity Range:Forward: 33.0 inches aft of datum at 2250 lbs. or less, with straight linevariation to 35.5 inches aft of datum at 2700 lbs., with straight linevariation to 40.9 inches aft of datum at 3100 lbs.Aft: 47.0 inches aft of datum at all weights.Moment Change Due To Retracting Landing Gear: 3052 lb.-ins.Reference Datum: Front face of firewall.MANEUVER LIMITSThis airplane is certificated in the normal category. The normalcategory is applicable to aircraft intended for non-aerobatic operations.These include any maneuvers incidental to normal flying, stalls (exceptwhip stalls), lazy eights, chandelles, and steep turns in which the angle ofbank is not more than 60 0 Aerobatic maneuvers, including spins, are not approved.FLIGHT LOAD FACTOR LIMITSFlight Load Factors:*Flaps Up: 3.8g, -1.52g*Flaps Down: 2.0g*The design load factors are 150% of the above, and in all cases. thestructure meets or exceeds design loads.KINDS OF OPERATION LIMITSThe airplane is equipped for day VFR and may be equipped for nightVFR and! or IFR operations. FAR Part 91 establishes the minimumrequired instrumentation and equipment for these operations. The reference to types of flight operations on the operating limitations placardreflects equipment installed at the time of Airworthiness Certificateissuance.Flight into known icing conditions is prohibited.2-7

SECTION 2LIMITATIONSCESSNAMODEL R182FUEL LIMITATIONS2 Standard Tanks: 30.5 U. S. gallons each.Total Fuel: 61 U. S. gallons.Usable Fuel (all flight conditions): 56 U. S. gallons.Unusable Fuel: 5.0 U. S. gallons.2 Long Range Tanks: 40 U. S. gallons each.Total Fuel: 80 U .S. gallons.Usable Fuel (all flight conditions): 75 U.S. gallons.Unusable Fuel: 5.0 U. S. gallons.NOTETo ensure maximum fuel capacity when refueling, placethe fuel selector valve in either LEFT or RIGHT position toprevent cross-feeding.NOTETakeoff and land with the fuel selector valve handle in theBOTH position.Approved Fuel Grades (and Colors):100LL Grade Aviation Fuel (Blue).100 (Formerly 100/130) Grade Aviation Fuel (Green).2-8

CESSNAMODEL R182SECTION 2LIMITATIONSPLACARDSThe following information is displayed in the form of composite orindividual placards.1.In full view of the pilot: (The "DAY -NIGHT-VFR-IFR" entry,shown on the example below, will vary as the airplane isequipped.)This airplane must be operated as a normal category airplanein compliance with the operating limitations as stated in theform of placards, markings, and manuals.- - - - - - - - MAXIMUMS - - - - - - - GROSS WEIGHT . . . .FLIGHT LOAD FACTORFlaps Up . .Flaps Down. 3100 Ibs 3.8, -1.52. . . 2.0No acrobatic maneuvers, including spins, approved. Altitudeloss in a stall recovery - 240 ft. Flight into known icingconditions prohibited. This airplane is certified for the following flight operations as of date of original airworthinesscertificate:DAY-NIGHT- VFR-IFR2.Near airspeed indicator:MAX SPEED - KIASMANEUVER112GEAR OPER140GEAR DOWN1403.On control lock:CONTROL LOCK - REMOVE BEFORE STARTING ENGINE.2-9

SECTION 2LIMITATIONS4.CESSNAMODEL R182On the fuel selector valve (standard tanks):OFFLEFT - 29 GAL. LEVEL FLIGHT ONLYBOTH - 56 GAL. ALL FLIGHT ATTITUDESTAKEOFF AND LANDINGRIGHT - 29 GAL. LEVEL FLIGHT ONLYOn the fuel selector valve (long range tanks):OFFLEFT - 37 GAL. LEVEL FLIGHT ONLYBOTH - 75 GAL. ALL FLIGHT ATTITUDESTAKEOFF AND LANDINGRIGHT - 37 GAL. LEVEL FLIGHT ONLY5.On the baggage door:120 POUNDS MAXIMUMBAGGAGE AND/OR AUXILIARY PASSENGERFORWARD OF BAGGAGE DOOR LATCH AND80 POUNDS MAXIMUMBAGGAGE AFT OF BAGGAGE DOOR LATCHMAXIMUM 200 POUNDS COMBINEDFOR ADDITIONAL LOADING INSTRUCTIONSSEE WEIGHT AND BALANCE DATA6.On flap control indicator:0 to 10 10 to 20 to FULL2-10(Partial flap range with blue colorcode and 140 kt callout; also, mechanical detent at 10 .)(Indices at these positions with whitecolor code and 95 kt callout; also,mechanical detent at 10 and 20 .)

SECTION 2LIMITATIONSCESSNAMODEL R1827.Forward of fuel tank filler cap (standard tanks):SERVICE THIS AIRPLANE WITH 100LL/l00 MIN. A VIATION GRADE GASOLINE - CAPACITY 30.5 GAL.Forward of fuel tank filler cap (long range tanks):SERVICE THIS AIRPLANE WITH 100LL/l00 MIN. AVIATION GRADE GASOLINE - CAPACITY 40.0 GAL.8.Near gear hand pump:MANUALGEAR EXTENSION1. SELECT GEAR DOWN2. PULL HANDLE FWD3. PUMP VERTICALLYCAUTIONDO NOT PUMP WITHGEAR UP SELECTED2-11/ (2-12 blank)

SECTION 3EMERGENCY PROCEDURESCESSNAMODEL R182SECTION 3EMERGENCY PROCEDURESTABLE OF CONTENTSPageIntroduction . . . . . . . . . . . .Airspeeds For Emergency Operation3-33-3OPERATIONAL CHECKLISTSEngine FailuresEngine Failure During Takeoff RunEngine Failure Immediately After TakeoffEngine Failure During Flight . . . . . .Forced Landings . . . . . . . . . . . . . .Emergency Landing Without Engine PowerPrecautionary Landing With Engine f)uwerDitching . . . . . . . .Fires . . . . . . . . . . .During Start On GroundEngine Fire In Flight .Electrical Fire In FlightCabin FireWing Fire . . . . . .Icing. . . . . .Inadvertent Icing EncounterStatic Source Blockage (Erroneous Instrument ReadingSuspected) . . . . . . . . .Landing Gear Malfunction ProceduresLanding Gear Fails To RetractLanding Gear Fails To ExtendGear Up Landing . . . . . . .Landing Without Positive Indication Of Gear LockingLanding With A Defective Nose Gear (Or Flat 1'\ose Tire)Landing With A Flat Main Tire . . . . .Electrical Power Supply System MalfunctionsOver-Voltage Light IlluminatesAmmeter Shows 73-73-73-83-83-83-83-93-93-93-103-103-103- 103-1

SECTION 3EMERGENCY PROCEDURESCESSNAMODEL R182TABLE OF CONTENTS (Continued)PageAMPLIFIED PROCEDURESEngine Failure.Forced Landings.Landing Without Elevator ControlFires . . . . . . . . . . . . .Emergency Operation In Clouds (Vacuum System Failure)Executing A 180 0 Turn In CloudsEmergency Descent Through CloudsRecovery From A Spiral DiveFlight In Icing ConditionsStatic Source BlockedSpins.Rough Engine Operation Or Loss Of PowerCarburetor Icing . .Spark Plug Fouling.Magneto Malfunction . . . . . .Engine-Driven Fuel Pump FailureLow Oil Pressure . . . . . . . .Landing Gear Malfunction ProceduresRetraction MalfunctionsExtension MalfunctionsGear Up Landing . . . .Electrical Power Supply System MalfunctionsExcessive Rate Of ChargeInsufficient Rate Of Charge . . . . . . 163-163-163-163-163-163-173-173-173-183-183-183-19

CESSNAMODEL R182SECTION 3EMERGENCY PROCEDURESINTRODUCTIONSection 3 provides checklist and amplified procedures for coping withemergencies that may occur. Emergencies caused by airplane or enginemalfunctions are extremely rare if proper preflight inspections andmaintenance are practiced. Enroute weather emergencies can be minimized or eliminated by careful flight planning and good judgment whenunexpected weather is encountered. However, should an emergency arise,the basic guidelines described in this section should be considered andapplied as necessary to correct the problem. Emergency proceduresassociated with ELT and other optional systems can be found in Section 9.AIRSPEEDS FOR EMERGENCY OPERATIONEngine Failure After Takeoff:Wing Flaps Up .Wing Flaps DownManeuvering Speed:3100 Lbs2550 Lbs . .2000 Lbs . .Maximum Glide:3100 Lbs2550 Lbs . .2000 Lbs . .Precautionary Landing With Engine PowerLanding Without Engine Power:Wing Flaps Up .Wing Flaps Down70 KIAS65 KIAS112 KIAS101 KIAS89 KIAS80 KIAS72KIAS64 KIAS65 KIAS75 KIAS65 KIASOPERATIONAL CHECKLISTSENGINE FAILURESENGINE FAILURE DURING TAKEOFF RUN1.2.3.4.5.6.Throttle -- IDLE.Brakes -- APPLY.Wing Flaps -- RETRACT.Mixture -- IDLE CUT-OFF.Ignition Switch -- OFF.Master Switch -- OFF.3-3

SECTION 3EMERGENCY PROCEDURESCESSNAMODEL R182ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF1.2.3.4.5.6.Airspeed -- 70 KIAS (flaps UP).65 KIAS (flaps DOWN).Mixture -- IDLE CUT-OFF.Fuel Selector Valve -- OFF.Ignition Switch -- OFF.Wing Flaps -- AS REQUIRED (40 recommended).Master Switch -- OFF.ENGINE FAILURE DURING FLIGHT1.2.3.4.5.6.Airspeed -- 80 KIAS.Carburetor Heat -- ON.Fuel Selector Valve -- BOTHMixture -- RICH.Ignition Switch -- BOTH (or START if propeller is stopped).Primer -- IN and LOCKED.FORCED LANDINGSEMERGENCY LANDING WITHOUT ENGINE POWER1.2.3.4.5.6.7.8.9.10.Airspeed -- 70 KIAS (flaps UP).65 KIAS (flaps DOWN).Mixture -- IDLE CUT-OFF.Fuel Selector Valve -- OFF.Ignition Switch -- OFF.Landing Gear -- DOWN (UP if terrain is rough or soft).Wing Flaps -- AS REQUIRED (40 recommended).Doors -- UNLATCH PRIOR TO TOUCHDOWN.Master Switch -- OFF when landing is assured.Touchdown -- SLIGHTLY TAIL LOW.Brakes -- APPLY HEAVILY.PRECAUTIONARY LANDING WITH ENGINE POWER1.2.3.4.5.6.7.3-4Airspeed -- 65 KIAS.Wing Flaps -- 20 .Selected Field -- FLY OVER, noting terrain and obstructions, thenretract flaps upon reaching a safe altitude and airspeed.Electrical Switches -- OFF.Landing Gear -- DOWN (UP if terrain is rough or soft).Wing Flaps -- 40 (on final approach).Airspeed -- 65 KIAS.

SECTION 3EMERGENCY PROCEDURESCESSNAMODEL R1828.9.10.11.12.Doors -- UNLATCH PRIOR TO TOUCHDOWN.Avionics Power and Master Switches -- OFF.Touchdown -- SLIGHTLY TAIL LOW.Ignition Switch -- OFF.Brakes -- APPLY HEAVILY.DITCHING1.2.3.4.5.6.Radio -- TRANSMIT MAYDAY on 121.5 MHz, giving location andintentions.Heavy Objects (in baggage area) -- SECURE OR JETTISON.Landing Gear -- UP.Flaps -- 20 0 - 40 0 Power -- ESTABLISH 300 FT/MIN DESCENT at 60 KIAS.Approach -- High Winds, Heavy Seas -- INTO THE WIND.Light Winds, Heavy Swells -- PARALLEL TOSWELLS.NOTEIf no power is available, approach at 70 KIAS with flaps upor at 65 KIAS with 10 0 flaps.7.8.9.10.11.

We urge all Cessna owners to use the Cessna Dealer Organization to the fullest. A current Cessna Dealer Directory accompanies your new airplane. The Directory is revised frequently, and a currentcopy can be obtained from yourCessna Dealer. Makeyour . CESSNA s:' 182 C. CESSNA--- - ----- .