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Cessna 162 SKYLANE Owner's Manual
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Cessna 162 SKYLANE Owner's Manual

Cessna 162 SKYLANE Owner's Manual

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Qssna.
M ORE PEOPL E BUY AND
flY CES SNA AIRPLANES
THAN ANY OTHER MAKE
1974
WORL D'S LARGEST PRO.
DUCER
OF G EN ERA L
AVIA TI O N A IRCRAFT
S I NCE
1956
MODEL
162
OWNERS
MANUAL
SKYLANE

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Summary of Contents for Cessna 162 SKYLANE

  • Page 1 Qssna. MODEL 162 M ORE PEOPL E BUY AND flY CES SNA AIRPLANES THAN ANY OTHER MAKE SKYLANE 1974 OWNERS WORL D'S LARGEST PRO. DUCER OF G EN ERA L MANUAL AVIA TI O N A IRCRAFT S I NCE 1956...
  • Page 2 182 shown for the Skylane . *This manual covers operation of the Model 182/Skylane which is certificated as Model 182P under Type Certificate No. 3A13. COPYRIGHT C 1989 DI021-13 Cessna Aircraft Company Wichita, Kansas USA...
  • Page 3 We urge you to read it from cover to cover, and to refer to it frequentiy. and care. Our interest in your flying pleasure has not ceased with your purchase of a Cessna. World-wide, the Cessna Dealer Organization backed by the Cessna Service Depart­...
  • Page 4 Maximum height of airplane nose gear depressed, al1 witb res and nose 8trut properly In!laled, and optional flashing beacon installed. Wing span airplane with opUona! strobe lights installed. PRINCIPAL DIMENSIONS ** 36'. 0"...
  • Page 5 ALPHABETICAL INDEX Index- 1 __________ _ ________________ This manual describes the operation and performance of both the Cessna Model 182 and the Cessna Skylane. Equipment described as "Optional" denotes that the subject equipment is o ptional on the Model 182.
  • Page 7 Section I OPERA TING CH ECK LIST One of the first steps in obtaining the utmost performance. service, and flying enjoyment from your Cessna is to familiarize yourself with your airplane's equipment, systems, and controls. This can best be done by reviewing this equipment while sitting in the airplane.
  • Page 8 Refer to inside back cover of this manual for quantities, materials, and specifications used of frequanlly service items. Note walk­ Visually check aircraft for general condition during around inspection. In cold weather, remove even small accumulations of frost, ice or snow from wing, tail and control surfaces.
  • Page 9 ® Remove rudder gust lock, if installed. Disconnect tail tie-down. Check control surfaces for freedom movement and security. ® Check aileron for freedom of movement and security. Disconnect wing tie-down. b. Check main wheel tire for proper inflation. Visually check fuel quantity; then check fuel filler cap secure and vent unobstructed.
  • Page 10 BEFORE STARTING THE ENGINE. Seats, Seat Belts and Shoulder Harnesses -- Adjust and lock. Brakes -- Test and set. Cowl Flaps -- "OPEN". (Move lever out of locking hole to reposition. Fuel Selector Valve Handle -- "BOTH". Radios and Electrical Equipment -- "OFF". STARTING ENGINE.
  • Page 11 Magnetos -- Check ( RPM drop should not exceed RPM on either magneto or RPM differential between magnetos). (10) Carburetor Heat -- Check operation. Propeller -- Cycle from high to low RPM; return to high RPM (11) (full in). (12) Flight Instruments and Radios -- Set.
  • Page 12 MAXIMUM PERFORMANCE CLIMB. (1) Airspeed -- 89 MPH (sea level) to 85 MPH (10,000 feet). (2 ) Power -- Full throttle and 2600 RPM. (3) Fuel Selector Valve Handle -- "BOTH." (4) Mixture -- rich (unless engine is rough). Full ( 5 ) Cowl Flaps -- Full "OPEN ...
  • Page 13 Carburetor Heat -- Cold. Flaps -- Retract to (3) Wing 20°. Cowl Flaps -- "OPEN." Upon reaching an airspeed of approximately MPH, retract flaps slowly. NORMAL LANDING. Touchdown -- Main wheels first. Landing Roll -- Lower nose wheel gently. Braking -- Minimum required. AFTER LANDING.
  • Page 14 INSTRUMENT PANEL l. Marker Beaton Indicator 27. Cowl Flap Control Lever Light. and Switch.s (Opt. ) 2B. Microphone (Opt. ) 2. Fllght In strument Group 29. Fuel Selector Light Aircrart Registration Number 30. Fuel Selector Valve fiandle 15. Economy Mixture Indicator (Opt.) 4.
  • Page 15 Section II DESCRIPTION AND OPERATING DETAILS The following paragraphs describe the systems and equipm ent whose This function and o peration is not obvious when sitting in the airplane. section also covers in somewhat greater detail some of the items listed in Check List form in Section that require further explanation.

  • Page 16: Fuel System

    To ensure maximum fuel capacity during refueling, place the fUel selector valve "LEFT" handle in either "RIGHT" position to prevent cross-feeding. FUEL SYSTEM SCHEMATIC TO ENGINE " FUEL ENGINE PRIMER STRAINER CODE THROTTLE ,:l@:i@M FUEL SUPPLY c::J CARBURETOR VENT __ -- - MECHANICAL LINKAGE...
  • Page 17 the opposite tank, expect an equal duration from the remaining fuel. The airspace in both fuel tanks is inter­ connected by a vent line (see figure 2-2) and, therefore, some sloshing of fuel between tanks can be expected when the tanks are nearly full and the wings are not level. For fuel system servicing information, refer to Servicing Require­...

  • Page 18: Electrical System

    ELECTRICAL SYSTEM LANDING .. fAl'l LIGHTS IGNtTlON/STARTER SWITCH INSTRUMENT LIGHTING. PIEDUTAl UGHTING. GLARE SHlElD MOUNTED MAP LIGHT. COMPASS UGHT .& OpnONAl OXYClM LIGHTING & OPTIONAl CQURTESY flASHING BEACON (OPT) TO RADIO (OPTI RADIO (OPTI RADIO (OPTI AurOMAlIC Pllor (OPTI AUDIO AMPLIfiER !OPTI UNSOI WAINING...
  • Page 19 electrical load is placed on the battery. Continued operation with the alternator switch off will reduce battery power low enough to open the battery contactor, remove power from the alternator field, and prevent alternator restart. AMMETER. The ammeter indicates the flow of current, in amperes, from the al­ ternator to the battery or from the battery to the aircraft electrical sys­...
  • Page 20 reset type circuit breaker mounted directly on the back of the lighter be­ hind the instrument panel. When more than one radio is installed, the radio transmitter relay (which is a part of the radio installation) is protected by the navigation lights circuit breaker labeled "NAV LIGHTS."...
  • Page 21 concentric rheostat control knobs labeled "LWR PANEL, ENG-RADIO, " a rheostat control knob labeled "INSTRUMENTS" control the intensity of instrument and control panel lighting. A rocker-type selector switch labeled "POST-FLOOD" is used to lect either standard flood lighting or optional post lighting. These controls are located on the left switch and control panel.
  • Page 22 A map light, mounted in the lower surface of the glare shield, is used for illuminating approach plates or other charts when using a control wheel mounted approach plate clip. The map light switch, labeled "MAP LIGHT," is located adjacent to the light. To use the light, turn on the "MAP LIGHT"...
  • Page 23 from the cabin manifold. Separate adjustable ventilators supply additional air; one near each upper corner of the windshield supplies air for the pilot and copilot, and two optional ventilators in the rear cabin ceiling supply air to the rear seat passengers. SHOULDER HARNESSES.
  • Page 24 primer in warm temperatures to six strokes in cold weather with the throttle open approximately inch. In extremely cold temperatures it may be necessary to continue priming while cranking. Weak inter­ mittent firing followed by puffs of black smoke from the exhaust stack Excess fuel can be cleared from the indicate overpriming or flooding.
  • Page 25 TAXIING DIAGRAM NOTE CODE Strong quartering tail winds require caution. DmECTION WIND Avoid s udden bursts of the throttle and sharp braking when the airplane is in this attitude. Use the steerable nose wbeel and rudder to maintain direction. Figure 2-4. 2-11...
  • Page 26 back to "BOTH" to clear the other set plugs. Then move switch to "L" position, note RPM and return the switch to the "BOTH" position. RPM drop should not exceed 150 RPM on either magneto or show greater than 50 RPM differential between magnetos. there is a doubt concerning operation of the ignition system, RPM checks at higher engine speeds will u sually confirm whether a deficiency exists.
  • Page 27 the obstacle by approximately 20 per cent. Soft field take-offs are per­ formed with 20° flaps by lifting the airplane off the ground as soon as practical in a slightly tail-low attitude. However, the airplane should be leveled off immediately to accelerate to a safe climb speed. 20°...
  • Page 28 2-5. settings required to obtain these powers can be determined by using your Cessna Power Computer or the OPERATIONAL DATA, Section VI. The Maximum Cruise Speed Performance table (figure 2-5) shows that cruising can be done most efficiently at higher altitudes because very nearly the same cruising speed can be maintained at much less power.
  • Page 29 The mixture setting should be readjusted for smoothest operatio n. LEANING WITH A CESSN A ECONOMY MIXTURE INDICATOR (EGT). Exhaust gas temperature (EGT) as shown on the optional Cessna Economy Mixture Indicator may be used as an aid for mixture leaning in cruising flight at power or less.
  • Page 30 lean to peak EGT and then enrichen the mixture until the EGT is on the 125°F. rich side of peak by an increment of An extended range mixture is obtained by leaning to peak EGT and then enrichening to an increment 75"F.
  • Page 31 LANDING. NORMAL LANDING. Landings should be made on the main wheels first to re duce the land­ ing speed and the subsequent need for braking in the landing roll. nose wheel is lowered gently to the runway after the speed has diminished to avoid unnecessary nose gear load.
  • Page 32 NOTE When pulling the propeller through by hand, treat it as if the ignition switch is turned on. A loose or broken ground wire on either magneto could cause the engine to fire. In extremely cold (O°F and lower) weather, the use of an external preheater (for both the engine and battery) and external power source is recommended whenever possible to obtain positive starting and to re­...
  • Page 33 Turn master switch "ON". Turn ignition switch to "START". Pump throttle rapidly to full open t wice. Return to 1/2" open position. Release ignition switch to "BOTH" when engine starts. Continue to prime the engine until it is running smoothly, or alternately, pump the throttle rapidly over the first total travel.
  • Page 34 one magneto in ground checks wllere only one spark plug fires in eacll cylinder. For optimum operation of the engine in cold weather, the appropriate use of carburetor heat is recommended. The following procedures are Indicated as a guideline: Use carburetor heat duTing engine warm-up and ground check. Full carburetor heat may UC! required for temperatures below 10°F, whereas partial heat could be used in temperatures between 10°F and 40°F.
  • Page 35 NOISE ABATEMENT. Increased emphasis on improving the quality of our environment re­ quires renewed effort on the part of all pilots to minimize the effect of aircraft noise on the public. We, as pilots, can demonstrate our concern for environmental im­ provement, by application of the following suggested procedures, and thereby tend to build public support for aviation: Pilots operating aircraft under VFR over outdoor assemblies...
  • Page 37 Section III EM ERG ENCY PROCEDURES Emergencies caused by aircraft or engine malfunctions are extreme­ ly rare proper pre-flight inspections and maintenance are practiced. Enroute weather emergencies can be minimized or eliminated by careful flight planning and good judgement when unexpected weather is encounter­ However should an emergency arIse, the basic guidelines described this section should...
  • Page 38 light will illuminate if the charge voltage reaches approximately 16 volts. Assuming that the malfunction was only momentary, an attempt should be made to reactivate the alternator system. To do this, turn both sides of the master switch off and then on again. If the problem no longer exists, normal alternator charging will resume and the warning 11ght will go off.
  • Page 39 LOW OIL PRESSURE. If low oil pressure is accompanied by normal oil temperature, there is a possibility the oil pressure gage or relief valve is malfunctioning. A leak in the line to the gage is not necessarily cause for an immediate precautionary landing because an orifice in this line will prevent a sudden loss of oil from the engine sump.
  • Page 40 If all attempts to restart the engine fail. and a forced landing is im­ minent. select a suitable field, and prepare for the landing as follows: Pull mixture control to idle cut-off position. Turn f uel selector valve handle "OFF". Turn off all switches except master switch.
  • Page 41 latter two instruments is available. EXECUTING A 1800 TURN IN CLOUDS. Upon entering the clouds, an immediate plan should be made to turn back as follows: Note the time of the minute hand and observe the position of the sweep second hand on the clock. When the sweep second hand indicates the nearest half-minute, initiate a standard rate left turn, holding the turn coordinator sym­...
  • Page 42 RECOVERY FROM A SPIRAL DIVE. If a spiral is encountered, proceed as follows: Close the throttle. stop the turn by using coordinated aileron and rudder control to align the symbolic airplane in the turn coordinator with the horizon reference line. Cautiously apply elevator back pressure to slowly reduce the in­...
  • Page 43 ENGINE FIRE IN FLIGHT. Although engine fires are extremely rare in flight, the following steps should be taken if one is encounte . r ed: Pull mixture control to idle cut-off. Turn fuel selector valve handle "OFF." Turn off master switch. Establish a MPH glide.
  • Page 44 icing encounter should be handled as follows: Turn pitot heat switch "ON" installed). Turn back or change altitude to obtain an outside air temperature that is less conducive to icing. Pull cabin heater control full out and rotate defroster control clockwise to obtain windshield defroster airflow.
  • Page 45 TRANSMIT 0>< SW !tC "f AUTO 'QPF RA.y'i ON "' "f 1" ..Opf RAT lON CONTROL WI P( pr.",nt. It .. I>lur: PANEL COVER - Removable for acc ess to battery. FUNCTION SELECTOR SWITCH (3-position toggle switch): - Activates transmitter instantly. Used for test purposes and if "g"...
  • Page 46 ELT FAILURE: If "g" switch actuation is questioned following a minor crash landing, gain access to the ELT and place the function selector switch in the ON position. PRIOR T O SIGHTING RESCUE AmCRAFT: Conserve aircraft battery. Do not activate Nav /Com transceiver. AFTER SIGHTING RESCUE AmCRAFT: Place ELT function se­...
  • Page 47 Cessna Model No. The airplane may be equipped for day, night, VFR, or IFR operation. Your Cessna Dealer will be happy to assist you in selecting equipment best suited to your needs. Your airplane must be operated in accordance with all FAA-approved markings and placards in the airplane.
  • Page 48 AIRSPEED LIMITATIONS (CAS). The following is a list o f the certificated calibrated airspeed (CAS) limitations for the airplane. Never Exceed Speed (glide or dive, smooth air) . 198 MPH Maximum Structural Cruising Speed . . 160MPH Maximum Speed, Flaps Extended Flaps 10°...
  • Page 49 OIL PRESSURE GAGE. 10 psi (red line) Idling Pressure • 30-60 psi (green arc) Normal Operating Range • • 100 psi (red line) Maximum Pressure FUEL QUANTITY INDICATORS. Empty ....E ( red line) •...
  • Page 50 on revised weight and balance records, and are included in the aircraft file. In addition to the licensed empty weight and moment noted on these records, the c. g. arm (fuselage station) is also shown, but need not be used on the Sample Loading Problem.
  • Page 51 optional cargo tie-down kit consisting of nine tie-down att achments (and is aVailable if it is desired to remove the rear seat child's seat, if installed) and utilize the rear c abin area to haul cargo. T wo tie-down at­ tachments clamp to the aft end of the two outboard front seat rails and are locked in place by a bolt which must be tightened to a minimum fifty...
  • Page 55 It is wise to follow a planned schedule of lubricat i on and preventive main­ tenance based on climatic and flying conditions encountered in your lo­ cality. Keep in touch with your Cessna Dealer, and take advantage of his knowledge and ex perience. Be knows yqur airplane and how to maintain Be will remind you when lubrications and oil changes are necessary, and about other s easonal and periodic services.
  • Page 56 ALUMINUM SURFACES. The clad aluminum surfaces of your Cessna may be washed with clear water to remove dirt; oil and grease may be removed with gasoline, naphtha, carbon tetrachloride or other non-alkaline solvents.
  • Page 57 PAINTED SURFACES. The painted exterior surfaces of your new Cessna have a durable, long lasting finish and, under normal conditions, require no polishing or buffing. Approximately days are required for the paint to cure com­ pletely; in most cases, the curing period will have been completed prior to delivery of the airplane.
  • Page 58 INTERIOR CARE. To remove dust and loose dirt from the upholstery and carpet, clean the interior regularly with a vacuum cleaner. Blot up any spilled liquid promptly with cleansing tissue rags. Don't pat the spot; press the blotting material firmly and hold it for several seconds.
  • Page 59 OYlners of exported aircraft should check with their own aviation officials to determine their individual requirements. Cessna recommends that these items, plus the Owner's Manual, Power Computer, Pilot's Check List, Customer Care Program book and Customer Care Card, be carried in the aircraft at all times.
  • Page 60 The CESSNA PROGRESSIVE CARE PROGRAM has been developed to provide a modern progressive inspection schedule that satisfies the com­ plete aircraft inspection requirements of both the 100 HOUR and ANNU AL...
  • Page 61 While these important inspections will be performed for you by any Cessna Dealer, in mos t cases you will prefer to have the Dealer from whom you purchased the aircraft accomplish this work.
  • Page 62 Your Cessna Dealer will be glad to supply you with details concerning these follow-up programs, and stands ready, through his Service Department, to supply you with fast, efficient, low-cost service.
  • Page 63 S ALES AND SERVICE DEALER DffiECTORY • DO'S AND DON'TS ENGINE BOOKLET The following additional publications, plus many other supplies that are applicable to your aircraft, are available from your Cessna Dealer. • SERVICE MANUALS AND PARTS CATALOGS FOR YOUR AIRCRAFT...
  • Page 65 SectioB f/ OPERATIONAL DATA The operational data charts on the following pages are presented for two purposes; first, so that you may know what to expect from your air­ plane under various conditions, and second, to enable you to plan your flights in detail and with reasonable accuracy.
  • Page 66 STALL SPEEDS ... MPH CAS ANGLE OF BANK 6 0° 0° CONDITION FLAPS UP 64 2950 LBS. 20° FLAPS GROSS 59 83 WEIGHT FLAPS 40° 81 57 POWER OFF - AFT CG Figure 6-2.
  • Page 68 EXTENDED RANGE MIXTURE 2950 Standard Conditions Zero Wind Gross Weight- Pounds 2500 FEET GAL(NO RESERVE) GAL (NO RESERVE) TA S ENDR. RANGE ENDR. RANGE HOURS HOURS MILES IlHP MILES 2450 14.2 5. 9 13.4 12.7 12.0 2300 13.1 12.2 11.5 11.0 5.
  • Page 69 EXTENDED RANGE MIXTURE 2950 Sta"dard Co"ditio"s Zero Wi"d Gross Weight- Pou"ds 5000 FEET GAL {NO RESERVEI GAL{NO RESERVE) E NDR. GALl ENDR. RANGE RANGE MILES HOURS MILES MPH HOUR HOURS 660 2450 2 3 78 160 14.5 870 22 157 13.6 695 910...
  • Page 70 EXTENDED RANGE MIXTURE Standard Conditions Zero Wind Gross Weight- 2950 Pounds 7500 FEET 60 GAL(NO RESERVE) 79 GAL (NO RESERVE) lA S GALl ENDR. ENDR. RANGE RANGE MILES HOURS MILES HOURS 2450 13.1 12.4 74 5 11.7 1005 11.0 1035 99 0 2300 12.2...
  • Page 71 EXTENDED RANGE MIXTURE Stanclarcl Conclitions Zero Wincl Gross Weight- 2950 Pouncls 10,000 FEET GAL(NO RESERVE) GAL (NO RESERVE) lAS GALl ENOl. ENDR. RANGE RANGE HOURS HOURS MILES MILES 2450 1020 11.9 5. 4 11.2 1050 7. 5 10.6 1065 7. 9 10.0 1080 11.1...
  • Page 72 EXTENDED RANGE MIXTURE Standard Conditions Zero Wind Groll Weieht. 2950 Pounds 15,000 FEET 60 GAL(NO RESERVE) 79 GAL (NO RESERVE) TA S ENDR. RANGE ENDR. RANGE MILES HOURS MILES HOURS 2450 10.4 1100 1120 9. 2 1080 114 5 2300 9.
  • Page 74 • SPEED 80 MPH (lAS) MA.XIMUM GLIDE • PROPELLER WINDMILLING • • ZERO WIND flAPS UP 18,000 16,000 &AI &AI - 14,000 12,000 10,000 8000 > 6000 <ICC 4000 2000 GROUND DISTANCE (STATUTE MILES) Figure 6-6. 6-10...
  • Page 75 WINTERIZATION KIT AND NON-CONGEALING OIL COOLER. For continuous operation in temperatures conSistently below 20°F, the Cessna winterization kit and non-congealing oil cooler should be in­ stalled to improve engine operation. The winterization kit consists of two shields to partially cover the cowl nose cap opening, one shield to cover the carburetor air intake, and insulation for the crankcase breather line.
  • Page 76 tenance work on the airplane electrical system (with the exception of elec­ tronic equipment). NGrE Electrical power for the airplane electrical circuits is pro­ vided through a split bus bar having all electronic circuits on one side of the bus and other electrical circuits on the other side of the bus.
  • Page 77 However, cabin pressures will vary With open cabin ventilators or win­ dows. The most adverse combinations will result in airspeed and alti­ meter variations of no more than 6 MPH and 50 feet respectively. In climb and cruising flight, the airspeed and altimeter will read high.
  • Page 78 RADIO SELECTOR SWITCHES RADIO SELECTOR SWITCH OPERA nON. Operation of the radio equipment is normal as covered in the respec­ tive radio manuals. When more than one radio is installed, an audio Switching system is necessary. Audio SWitching is accomplished by a series of selector switches located at the top-center of the instrument panel.
  • Page 79 "TR 1" selects the upper transmitter and "TR 2" selects the lower transmitter. The installa tion of Cessna radio equipment provides certain audio back-up capabilities and transmitter selector switch functions that the pilot should be familiar with. When the transmitter selector switch labeled "TR 1"...
  • Page 80 Supplemental oxygen should be used by all occupants when cruising above 10,000 feet. As described in the Cessna booklet "Man At Altitude," it is often advisable to use oxygen at altitudes lower than 10, 000 feet under conditions of night flying, fatigue, or periods of physiological or emotional disturbances.
  • Page 81 OXYGEN DURATION CHART (48 CUBIC FEET CAPACITY) 1800 1600 1400 ..1200 I1J 1000 (I) I1J Q. I1J CJ OXYGEN DURATION - HOURS NOTE. This chart is based on a pilat with an orange calor-coded oxygen line fitting and passengers with green color-coded line fittings.
  • Page 82 NOTE For safety reasons, no smoking should be allowed in the aircraft while oxygen is being used. When ready to use the oxygen system, proceed as follows: Select mask and hose. NOTE The hose provided for the pilot is of a higher flow rate than those for the passengers;...
  • Page 83 OXYGEN DURATION CALCULATION. 7-2) The Oxygen Duration Chart (figure should be u sed in determin­ ing the usable duration (in hours) of the oxygen supply in your airplane. The following procedure outlines the method of finding the duration from the chart. Note the availa ble oxygen pressure shown on the pressure gage.
  • Page 84 IMPORTANT Oil, grease, or other lubricants in contact with oxygen create a serious fire hazard, and such contact must be avoided when handling oxygen equipment. AMBIENT FILLING FILLING AMBIENT TEMPERATURE PRESSURE TEMPERATURE PRESSURE PSIG PSIG 1600 1825 1650 1875 1700 1925 1725 1975...
  • Page 85 CESSNA ECONOMY MIXTURE INDICATOR The Cessna Economy Mixture Indicator is an exhaust gas temperature (EGT) sensing device which visually aids the pilot in adjusting the cruise mixture. Exhaust gas temperature varies with fuel-to-air ratio, power and RPM. However, the difference between the peak EGT and the EGT at the cruise mixture setting is essentially constant and this provides a useful leaning aid.
  • Page 86 OIL QUICK-DRAIN VALVE An oil quick-drain valve is optionally offered to replace the drain plug in the oil sump drain port. The valve provides a quicker and clean­ er method of draining engine oil. To drain the oil with this valve instal­ led, slip a hose over the end of the valve and route the hose to a suitable container, then push upward on the end of the valve until it snaps into the open pOSition.
  • Page 87 1-7 4 -4 Center of Gravity Moment "Airspeed Correction Table, 6-1 Envelope, 4-8 Airspeed Indicator, True, 7-10 Cessna Customer Care Program, Airspeed Indicator Markings, 4-2 5- 7 Airspeed Limitations, 4-2 Alternate Source Valve, Static Cessna Progressive Care, 5-7 Pressure, 7-2...
  • Page 88 Emergency Locator Transmitter (ELT), 3-8 Diagram, ELT operation, 3-9 electrical system, 2-4 Empty Weight, inside front cover exterior inspection, 1-2 Engine, fuel system, 2-2 before starting, 1-4 instrument panel, 1-8 instrument markings, 4-2 loading arrangements, 4-5 oil, inside back cover maximum glide, 6-10 operation limitations, 4-2 principal dimensions, ii...
  • Page 89 balked, 1-6 2-17 schematic, 2-2 before, 1-6 Fuses and Circuit Breakers, 2-5 crosswind, 2-17 distance table, 6-9 forced, 3-3 normal, 1-7 2-17 precautionary with power, 3-3 Graph, Loading, 4-7 Gross Weight, inside front cover short field, 2-17 Ground Handling, 5-1 Landing Gear Servicing, inside back cover Ground Service Plug Receptacle,...
  • Page 90 Mooring Your Airplane, 5-1 inside front cover Precautionary Landing with Engine Power, 3-3 Principal Dimensions Diagram, ii Noise Abatement, 2-21 Progressive Care, Cessna, 5-7 N on-Congealing Oil Cooler, 7-1 Propeller, Normal Category Maneuvers, 4-1 care, 5-3 Normal Climb, 1-5 Publications, 5-9...
  • Page 91 fuel, inside back cover Tachometer, 4-3 landing gear, inside back cover Take-Off, 1-5, 2-12 Short Field Landing, 2-17 before, 1-4, 2-10 Shoulder Harnesses , 2-6 data chart, 6-3 Spark Plug Fouling, 3-2 maximum perform ance, 1-5 Speaker-Phone S witches, 7-5 normal, 1-5 Spins, 2-16 Taxiing, 2-10...
  • Page 94 Detergent or dispersant oil, con­ forming to Continental Motors Specification MHS-24A, must be used. NOTE Your Cessna was delivered from the factory with a cor­ rosion preventive aircraft engine oil. If oil must be added during the first 25 hours, use only aviation grade straight mineral oil (non-detergent) conforming to Speci­...

  • Page 95: Landing Gear

    SERVICING REQUIREMENTS FUEL: G RADE -- 80/87 Minimum Grade Aviation Fuel. 100/130 low lead aviation fuel with a lead content limited to 2 c. c. per gallon is approved. also CAPACITY EACH STANDARD TANK -- 32.5 Gallons. CAPACITY EACH LONG RANGE TANK -- 42.0 Gallons. NOTE To ensure maximum Iuel capacity during refueling, place the fuel selector valve handle in either "LEFT"...
  • Page 96 "TAKE YOUR CESSNA HOME FOR SERVICE AT THE SIGN OF THE CESSNA SHiElD". CESSNA AIRCRAFT COMPANY WICHITA, KANSAS...