Cessna 182 1973 Owner'S Manual Download Page 69 | Manualshive

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PERFORMANC

LEAN MIXTURE

Standard Conditions

\_

Zero

Wind

\_

Gross

Weight-

2950

Pounds

15,000

FEET

]

60 GAL(NO

RESERVE)

|

79

GAL(NO

RESERVE)

%

TAS! |GAL/|

ENDR.

RANGE

ENDR.

RANGE

RPM

|

MP

|

BH

MPH

[HOUR|

HOURS

MILES

HOURS

MILES

250

|

16

54

|

145

|

10.4

5.8

835

7.6

1100

15

50

139

|

9.8

6.1

850

8.1

1120

14

|

46

126

|

9.2

6.5

820

8.6

1080

2300

|

16

50

|

139

|

9.6

6.2

870

8.2

1145

15

a

|

1s

|

oe

6.6

865

8.7

1135

14

42

|

13

|

85

m1

800

9.3

1050

2200

16

a

|

11

|

et

6.6

865

8.7

1135

15

44

|

120

|

8.6

7.0

835

9.2

1100

14

40

106

8.0

7.5

795

9.9

1045

2000

16

40

|

106

|

7.8

77

815

10.1

1075

15

37

971

|

7.3

8.2

795

10.8

1050

Figure

6-4 (Sheet

5

of 5).

6-8

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Summary of Contents for 182 1973

Page 1: ... EssnA MORE PEOPLE BUY AND FLY CESSNA AIRPLANES THAN ANY OTHER MAKE 1973 WORLD S LARGEST PRO DUCER OF GENERAL AVIATION AIRCRAFT SINCE 1956 MODEL 185 A ITN ID SKYLANE OWNERS MANUAL ...

Page 2: ...NG LOADING Pounds Sq Foot a a 08 POWER LOADING Pounds HP FUEL CAPACITY Total Standard Tanks o o ww Optional Long Range Tanks OIL CAPACITY Total PROPELLER Constant Speed Diameter Ee ENGINE Continental Engine vw mow EEE 230 rated BHP at 2600 RPM NOTE Performance data is shown for the Skylane which is 2 to 3 mph faster than a standard equipped Model 182 without speed fairings is a corresponding diffe...

Page 3: ......

Page 4: ...alers world wide d Best in the industry Specific benefits and provisions of the warranty plus other important benefits for you are contained in your Customer Caré Program boak supplied with your aircraft Warranty service is available to you at any authorized Cessna Dealer throughout the world upon presentation of your Customer Care Card which establishes your eligibility under the warranty FACTORY...

Page 5: ...aximum height of airplane with nose gear depressed all tires and nose strut properly inflated and optional flashing beacon installed ying span of airplane with optional strobe lights installed PRINCIPAL DIMENSIONS ...

Page 6: ...ECTION V CARE OF THE AIRPLANE ____ 5 1 OWNER FOLLOW UP SYSTEM5 12 SECTION Vi OPERATIONAL DATA 6 1 SECTION VIiI OPTIONAL SYSTEMS __________ 7 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 optional on the Model 182 Much of this equipment is standard on the Skylane model i...

Page 7: ...ed check list covering the Before Take Off and Before Landing phases of aircraft operation is provided on a plastic card and normally stowed in the map compartment This abbreviated check list is a convenient reference of key items to be rechecked immediately prior to taxiing into position for take off and before entering the final approach for landing The flight operational characteristics of your...

Page 8: ...ntain no internal accumulations of ice or debris If night flight is planned check operation of all lights and make sure a flashlight is available a Remove control wheel lock b Check ignition switch OFF Turn on master switch and check fuel quantity indicators then turn master switch OFF d Check fuel selector valve handle on BOTH e Check baggage door for security Lock with key if children are to occ...

Page 9: ...nnect tie down rope Check oil level Do not operate with less than nine quarts Fill to twelve quarts for extended flight Before first flight of day and after each refueling pull out strainer drain knob for about four seconds to clear fuel strain er of possible water and sediment Check strainer drain clos ed If water is observed there is a possibility that the wing tank sumps contain water Thus the ...

Page 10: ... engine fires but not longer than 30 seconds release when engine starts NOTE If engine has been overprimed start with throttle open 1 4 to 1 2 full open Reduce throttle to idle when en gine fires NOTE After starting check for oil pressure indication within 30 seconds in normal temperatures and 60 seconds in cold temperatures If no indication appears shut off engine and investigate BEFORE TAKE OFF ...

Page 11: ...aise nose wheel at 60 MPH 5 Climb Speed 90 MPH until all obstacles are cleared then set up climb speed as shown in NORMAL CLIMB check list MAXIMUM PERFORMANCE TAKE OFF 1 Wing Flaps 20 2 Carburetor Heat Cold 3 Brakes Apply 4 Power Full throttle and 2600 RPM 5 Brakes Release 6 Elevator Control Maintain slightly tail low attitude 7 Climb Speed 60 MPH until all obstacles are cleared then set up climb ...

Page 12: ...per as required Elevator and Rudder Trim Adjust Mixture Lean LET DOWN 1 2 3 Mixture Rich Power As desired Carburetor Heat Apply if carburetor icing conditions exist BEFORE LANDING Fuel Selector Valve Handle BOTH Mixture Rich Propeller High RPM Cowl Flaps CLOSED Carburetor Heat Apply before closing throttle Airspeed 80 to 90 MPH flaps retracted Wing Flaps 0 to 40 below 110 MPH Airspeed 70 to 80 MPH...

Page 13: ...ing Roll Lower nose wheel gently 3 Braking Minimum required AFTER LANDING 1 Cowl Flaps OPEN 2 Wing Flaps Retract 3 Carburetor Heat Cold SECURING AIRCRAFT 1 Parking Brake Set 2 Radios and Electrical Equipment OFF 3 Mixture Idle cut off pulled full out NOTE Do not open throttle as engine stops since this actuates the accelerator pump 4 Ignition and Master Switch OFF 5 Control Lock Installed 1 7 ...

Page 14: ...Opt 16 Flight Hour Recorder Opt 17 Optional Radio and Instrument Space 18 Map Compartment 19 Cabin Heat Cabin Air and Defroster Control Knobs 20 Cigar Lighter 21 Tachometer 22 Wing Flap Switch and Position Indicator 23 Mixture Control Knob 24 Propeller Control Knob 25 Rudder Trim Control Wheel Figure 2 1 Economy Mixture Indicator Opt 12 Cowl Flap Control Handle Microphone Opt Fuel Selector Valve H...

Page 15: ...o a selector valve De pending upon the setting of the selector valve fuel from the left right or both tanks flows through a fuel strainer and carburetor to the engine induction system The fuel selector valve should be in the BOTH position for take off climb landing and maneuvers that involve prolonged slips or skids Operation from either LEFT or RIGHT tank is reserved for cruising flight NOTE When...

Page 16: ...el capacity during refueling place the fuel selector valve handle in either LEFT or RIGHT position to prevent crossfeeding FUEL SYSTEM FUEL STRAINER ENGINE PRIMER CODE THROTTLE FUEL SUPPLY CARBURETOR C2 vent T a MECHANICAL LINKAGE f petit om MIXTURE TO CONTROL KNOB ENGINE v Figure 2 2 2 2 ...

Page 17: ...utomatically activated to open the circuit to the electronics bus Isolating the electronic circuits in this manner prevents harmful transient voltages from damaging the transistors in the electronics equipment MASTER SWITCH The master switch is a split rocker type switch labeled MASTER and is ON in the up position and OFF in the down position The right half of the switch labeled BAT controls all e...

Page 18: ...LARE SHIELD MOUNTED MAP LIGHT OPTIONAL CONTROL WHEEL MAP LIGHT TO TRANSMITTER RELAY OPT TO HEATED PITOT STALL WARNING SYSTEM OFT TO FUEL OUANTITY INDICATORS CYLINDER HEAD TEMP GAGE OPTIONAL CARBURETOR AIR TEMPERATURE GAGE TO IGNITION STARTER SWITCH TO ELECTROLUMINESCENT LIGHTING TO INSTRUMENT LIGHTING COMPASS LIGHT AND OPTIONAL OXYGEN LIGHTING TO OPTIONAL POST LIGHTING TO DOME AND OPTIONAL COURTES...

Page 19: ...ack on again If the warning light does not illuminate normal alternator charging has resumed however if the light does illuminate again a malfunction has occurred and the flight should be terminated as soon as practical The over voltage warning light may be tested by momentarily turning off the ALT portion of the master switch and leaving the BAT portion turned on CIRCUIT BREAKERS AND FUSES Most o...

Page 20: ...witch and control panel The courtesy lights are operated by a switch on the aft side of the left rear door post The flashing beacon should not be used when flying through clouds or overcast the flashing light reflected from water droplets or particles in the atmosphere particularly at night can produce vertigo and loss of orientation The two high intensity strobe lights will enhance anti collision...

Page 21: ...ed by the ENG RADIO control knob For informa tion concerning radio selector switch lighting refer to Section VII The control pedestal and optional overhead oxygen console are lighted separately by post lights This lighting is controlled by the ENG RADIO control knob Map lighting may be provided by three different sources standard overhead console map lights a standard glare shield mounted map ligh...

Page 22: ...hen the CABIN HEAT knob is out This action increases the airflow through the system increasing efficiency and blends cool out side air with the exhaust manifold heated air thus eliminating the possibility of overheating the system ducting The rotary type DEFROST knob regulates the airflow for windshield defrosting Front cabin heat and ventilating air is supplied by outlet holes spaced across a cab...

Page 23: ...rmit the occupant to lean forward enough to sit completely erect but is tight enough to prevent excessive forward movement and contact with objects during sudden deceleration Also the pilot will want the freedom to reach all controls easily Releasing and removing the shoulder harness is accomplished by pulling upward on the narrow release strap and removing the harness stud from the slot in the se...

Page 24: ...AKE OFF WARM UP Since the engine is closely cowled for efficient in flight cooling pre cautions should be taken to avoid overheating on the ground Full throttle checks on the ground are not recommended unless the pilot has good reason to suspect that the engine is not turning up properly MAGNETO CHECK The magneto check should be made at 1700 RPM as follows Move ignition switch first to R position ...

Page 25: ...H WING AND DOWN ELEVATO USE DOWN AILERON i ON RH WING AND i LT CODE NOTE Strong quartering tail winds require caution WIND DIRECTION Avoid sudden bursts of the throttle and sharp braking when the airplane is in this attitude Use the steerable nose wheel and rudder to maintain direction Figure 2 4 ...

Page 26: ... pulled into it Most engine wear occurs from improper operation before the engine is up to normal operating temperatures and operating at high powers and RPM s For this reason the use of maximum power for take off climb should be limited to that absolutely necessary for safety Whenever possible reduce take off power to normal climb power Normal take offs are accomplished with wing flaps 0 to 20 co...

Page 27: ...n addition this type of climb provides bet ter engine cooling less engine wear and more passenger comfort due to lower noise level If it is necessary to climb rapidly to clear mountains or reach favor able winds at high altitudes the best rate of climb speed should be used with maximum power This speed is 89 MPH at sea level decreasing 2 MPH for each 5000 feet above sea level If an obstruction ahe...

Page 28: ... then enrich mixture slightly from this point Any change in altitude power or carburetor heat will require a change in the lean mixture setting Application of full carburetor heat may enrich the mixture to the point of engine roughness To avoid this lean the mixture as instructed in the preceding paragraph The use of full carburetor heat is recommended during flight in very heavy rain to avoid the...

Page 29: ...ently to the runway after the speed has diminished to avoid unnecessary nose gear load This procedure is especially im portant in rough field landings SHORT FIELD LANDING For short field landings make a power off approach at 69 MPH with 40 flaps and land on the main wheels first Immediately after touch down lower the nose gear to the ground and apply heavy braking as re quired For maximum brake ef...

Page 30: ...weather the use of an external preheater for both the engine and battery and an external power source is recommended whenever possible to obtain positive starting and to re duce wear and abuse to the engine and the electrical system Pre heat will thaw the oil trapped in the oil cooler which probably will be con gealed prior to starting in extremely cold temperatures When using an external power so...

Page 31: ...o BOTH when engine starts 7 Continue to prime the engine until it is running smoothly or alternately pump the throttle rapidly over the first 1 4 of total travel 8 Oil pressure Check 9 Pull carburetor heat on after engine has started Leave on until the engine is running smoothly 10 Lock primer NOTE If the engine does not start during the first few attempts or if engine firing diminishes in strengt...

Page 32: ...ended The following procedures are indicated as a guideline 1 Use carburetor heat during engine warm up and ground check Full carburetor heat may be required for temperatures below 10 F whereas partial heat could be used in temperatures between 10 F and 40 F 2 Use the minimum carburetor heat required for smooth operation in take off climb and cruise NOTE When operating in sub zero temperatures car...

Page 33: ...ction VII for discussion of additional cold weather equip ment HOT WEATHER OPERATION The general warm temperature starting information on page 2 9 is appropriate Avoid prolonged engine operation on the ground 2 19 ...

Page 34: ...so cause malfunctions Problems of this nature constitute an electrical emergency and should be dealt with immediately Electrical power malfunctions usually fall into two categories excessive rate of charge and insufficient rate of charge The paragraphs below describe the recommended remedy for each situa tion EXCESSIVE RATE OF CHARGE After engine starting and heavy electrical usage at low engine s...

Page 35: ...minated as soon as practical ROUGH ENGINE OPERATION OR LOSS OF POWER SPARK PLUG FOULING A slight engine roughness in flight may be caused by one or more spark plugs becoming fouled by carbon or lead deposits This may be verified by turning the ignition switch momentarily from BOTH to either the L or R position An obvious power lossin single ignition operation is evidence of spark plug or magneto t...

Page 36: ...INE POWER Before attempting an off airport landing one should drag the land ing area at a safe but low altitude to inspect the terrain for obstructions and surface conditions proceeding as follows 1 Perform before landing check 2 Drag over selected field with flaps 20 and 75 MPH airspeed noting the preferred area for touchdown for the next landing approach Then retract flaps upon reaching a safe a...

Page 37: ... Mayday message on 121 5 MHz giving location and intentions 1 Plan approach into wind if winds are high and seas are heavy With heavy swells and light wind land parallel to swells 2 Approach with flaps 40 and sufficient power for a 300 ft min rate of descent at 70 MPH 3 Unlatch the cabin doors 4 Maintain a continuous descent until touchdown in level attitude Avoid a landing flare because of diffic...

Page 38: ...ding primarily with skidding motions rather than rolling motions so that the compass will read more ac curately 5 Maintain altitude and airspeed by cautious application of elevator control Avoid overcontrolling by keeping the hands off the control wheel andsteering only with rudder EMERGENCY LET DOWNS THROUGH CLOUDS If possiBle obtain radio clearance for an emergency descent through clouds To guar...

Page 39: ...ed rudder force if present 6 Apply carburetor heat 7 Clear engine occasionally but avoid using enough power to dis turb the trimmed glide 8 Upon breaking out of clouds apply normal cruising power and resume flight FIRES ENGINE FIRE DURING START ON GROUND Improper starting procedures such as pumping the throttle during a difficult cold weather start can cause a backfire which could ignite fuel that...

Page 40: ...d in paragraph Emergency Landing Without Engine Power Do not attempt to restart the engine ELECTRICAL FIRE IN FLIGHT The initial indication of an electrical fire is the odor of burning in sulation The immediate response should be to turn the master switch OFF Then close off ventilating air as much as practicable to reduce the chances of a sustained fire If an oxygen system is available in the airc...

Page 41: ...by carburetor ice or air intake filter ice 6 Plan a landing at the nearest airport With an extremely rapid ice build up select a suitable off airport landing site 7 With an ice accumulation of one quarter inch or more on the wing leading edges be prepared for significantly higher stall speed 8 Leave wing flaps retracted With a severe ice build up on the horizontal tail the change in wing airflow d...

Page 42: ...is any information in this section which contradicts the FAA approved markings and placards itis to be disregarded MANEUVERS NORMAL CATEGORY The airplane is certificated in the normal category The normal category is applicable to airplanes intended for non aerobatic operations These include any maneuvers incidental to normal flying stalls except whip stalls and turns in which the angle of bank is ...

Page 43: ...eed at which you may use abrupt control travel AIRSPEED INDICATOR MARKINGS The following is a list of the certificated calibrated airspeed markings CAS for theairplane Never Exceed glide or dive smooth air 198 MPH red line Caution Range 160 198 MPH yellow arc Normal Operating Range 68 160 MPH green arc Flap Operating Range 63 110 MPH white arc ENGINE OPERATION LIMITATIONS Power andSpeed 230 BHP at...

Page 44: ...l Operating Range 15 23 in Hg green arc CARBURETOR AIR TEMPERATURE GAGE E LOET Icing Range 15 to 5 C yellow arc SUCTION GAGE GYRO SYSTEM Normal Operating Range 4 6 5 4 in Hg green arc WEIGHT AND BALANCE The following information will enable you to operate your Cessna within the prescribed weight and center of gravity limitations To figure the weight and balance for your particular airplane use the...

Page 45: ... station of the item being loaded must be made if the position of the load is different from that shown on the Loading Graph Total the weights and moments 1000 and plot these values on the Center of Gravity Moment Envelope to determine whether the point falls within the envelope and if the loading is acceptable BAGGAGE AND CARGO TIE DOWN A nylon baggage net having six tie down straps is provided a...

Page 46: ...maximum allowable cabin floor loading of the rear cabin area is 200 pounds square foot however when items with small or sharp support areas are carried the installation of a 1 4 plywood floor is recommended to protect the air craft structure The maximum rated load weight capacity for each of the seven tie downs is 140 pounds and for the two seat rail tie downs is 100 pounds Rope strap or cable use...

Page 47: ...198usssed Jo v vo1y odedsed 9 sora WE GW Ys wR 8 dmg eg useg seas Moy puodeg Juioerdey odie 2 62 ove cor 4c sre g198uassBd MOY puodag g 9 21 ove 0g 03 gg uOlEIg 193ussSSEJ JUOLT PUR JOTld F CTeD 9 18 TED 6L a8ury 3uoT Tend LT 09 Co UTRD 49 1B IED 09 PIBPUEIS ONG 0 44 0 44 owen ogg wa suotye nores Ie 10 pasn aq Kew 10 n JO yBlom ayy SID GI TO 2 1 09 FILT suerdary ordweg yStom Adwy pasusory T 0001 0...

Page 48: ...qelsnlpe uo A1AvIS JO Iejued 1a3uassed Jess Juoly pur J0Tid smoys 5 ess aiqejsnlpe Jurjuasaidss aur 1 SHLON SHHONI ANNO 000T LNANON VOT 0g 92 V4 ST or g 0 XVIN sg 08 u VEYY HDVDOVE LAV 08 XVIN SET 021 WWu VEYY LVES S aIIHO NO 001 HAONESSYA YO AOVHOVE 0ST HdVYd9 DNIAvOT 002 088 00g QUVANVLS o XVIN TVD 09 7 088 SANNOd THOIAM VOT 00 SINVL ZONVE DNOT 05 XVI TVD 6L 009 4 7 ...

Page 49: ...STHONI ANNOJ 000T LNAWOW LA VEOHIV AIAVO T 021 GIT OIF SOT O00T G6 06 98 08 S OL 9 IdOTIANT LNINWOW ALIAVYDO 40 Y3LN3D 09 S081 0061 0002 0012 0022 0062 002 0052 009 0042 0082 0062 0862 SAQNNOd LHOIAM LIVHOWV QIAVOT 4 8 ...

Page 50: ...angle of 29 either side of center or dam age to the gear will result If the airplane is towed or pushed over a rough surface during hangaring watch that the normal cushioning action of the nose strut does not cause excessive vertical movement of the tail and the resulting contact with low hangar doors or structure A flat nose tire or deflated strut will also increase tail height MOORING YOUR AIRPL...

Page 51: ...o not rub the plastic with a dry cloth since this builds up an electrostatic charge which attracts dust Waxing with a good commercial wax will finish the cleaning job A thin even coat of wax polished out by hand with clean soft flannel cloths will fill in minor scratches and help prevent further scratching Do not use a canvas cover on the windshield unless freezing rain or sleef is anticipated sin...

Page 52: ...wax on the leading edges of the wings and tail and on the engine nose cap and propeller spinner will help reduce the abrasion encountered in these areas When the airplane is parked outside in cold climates and it is neces sary to remove ice before flight care should be taken to protect the paint ed surfaces during ice removal with chemical liquids A 50 50 solution of isopropyl alcohol and water wi...

Page 53: ...ting the fabric If your airplane is equipped with leather seating cleaning of the seats is accomplished using a soft cloth or sponge dipped in mild soap suds The soap suds used sparingly will remove traces of dirt and grease The soap should be removed with a clean damp cloth The plastic trim headliner instrument panel and control knobs need only be wiped off with a damp cloth Oil and grease on the...

Page 54: ...y from your Dealer he will perform the initial inspection before delivery of the airplane to you If you pick up the airplane at the factory plan to take it to your Dealer reasonably soon after you take delivery on it This will permit him to check it over and to make any minor adjustments that may appear necessary Also plan an inspection by your Dealer at 100 hours or 180 days whichever comes first...

Page 55: ... carried in the aircraft at all times 1 Weight and Balance and associated papers latest copy of the Repair and Alteration Form FAA Form 337 if applicable 2 Aircraft Equipment List C To be made available upon request 1 Aircraft Log Book 2 Engine Log Book NOTE Cessna recommends that these items plus the Owner s Manual Power Computer Pilot s Check List Customer Care Program book and Customer Care Car...

Page 56: ...plate located on the left forward doorpost A Finish and Trim Plate contains a code describing the interior color scheme and exterior paint combination of the aircraft The code may be used in conjunction with an applicable Parts Catalog if finish and trim information is needed This plate is located at the bottom of the left forward door post 5 7 ...

Page 57: ...fuel strainer of possible water and sediment Check strainer drain closed If water is observed there is a possibility that the wing tank sumps contain water Thus the wing tank sump drain plugs and fuel selector valve drain plug should be removed to check for the presence of water OIL FILLER When preflight check shows low oil level service with aviation grade engine oil SAE 50 above 40 F and SAE 10W...

Page 58: ...arts If optional oil filter is installed one additional quart is required when the filter element is changed OXYGEN CYLINDER AND FILLER VALVE OPT Check oxygen pressure gage for anticipated requirements before each flight Use filler valve on left side of rear baggage com partment wall to refill cylinder with aviator s breathing oxygen Spec No MIL 0 27210 Maximum pressure cylinder tem perature stabi...

Page 59: ...filter element If optional oil filter is not installed change oil and clean the oil pressure screen every 25 hours Change engine oil at least every four months even though less than the recommended hours have accumu lated Reduce periods for prolonged operation in dusty areas cold cli mates or when short flights and long idle periods result in sludging condi tions CARBURETOR AIR FILTER Clean or rep...

Page 60: ...e offs and landings are made VACUUM SYSTEM AIR FILTER OPT Replace filter element Re place sooner if suction gage reading drops to 4 6 in Hg AS REQUIRED NOSE GEAR SHOCK STRUT Keep filled with hydraulic fluid and in flated with air to 55 60 psi ADDITIONAL SERVICE AND TEST REGULATIONS Servicing Intervals of items in the preceding check list are recommended by The Cessna Aircraft Company Govern ment r...

Page 61: ...y you with fast efficient low cost service PUBLICATIONS Various publications and flight operation aids are furnished in the air craft when delivered from the factory These items are listed below e OWNER S MANUALS FOR YOUR AIRCRAFT ELECTRONICS AND AUTOPILOT POWER COMPUTER SALES AND SERVICE DEALER DIRECTORY DO S AND DON TS ENGINE BOOKLET The following additional publications plus many other supplies...

Page 62: ...f climb etc You must estimate these variables for yourself and make allowances accordingly Speeds shown in the Cruise Performance charts reflect performance of the Skylane con figuration these speeds are 2 to 3 MPH faster than the Model 182 Remember that the charts contained herein are based on standard day conditions For more precise power fuel consumption and endur ance information consult the P...

Page 63: ...STALL SPEEDS MPH CAS ANGLE OF BANK CONDITION 02s faango 60 FLAPS UP 64 69 91 2950 LBS GROSS FLAPS 20 59 63 83 WEIGHT FLAPS 40 57 61 81 POWER OFF AFT CG Figure 6 2 6 2 ...

Page 64: ... VES Iv Viva ghiTD d0 3 LVH WNKWIXVYIN 3 08 TTD 03 HOY Puk Un punoas y 2auB1 219TISGO 33 0 TBS D 03 EI0Y BY JO Gh 4 210TISQ0 106 S2OULISIP 85TLIOU KBAUNI SST 41p UO Tonwrado 103g OPTIRIE Teron ed 10j 2ameaadiie ARDUTIS SA0QE J G7 YOES 105350 SOUEISIP OSEAN STLON SIS id S0z Sg 091 SSE 081 90 S01 02 bk cee 029 SLT 0 g 2 09 1 ot 0s 0002 S001 008 898 STF ShL ose cag 62 S18 08 08k 00g 088 s g 08 S81 02...

Page 65: ... 63 144 12 0 5 0 720 6 6 950 2300 23 1 151 13 1 4 6 690 6 0 910 22 67 148 12 2 4 9 730 6 5 960 21 62 143 11 5 5 2 T45 6 9 980 20 59 140 11 0 5 5 765 7 2 1005 2200 23 67 148 12 1 5 0 735 6 5 965 22 63 144 11 4 5 3 760 6 9 1000 21 59 140 10 8 5 6 780 7 3 1025 20 55 135 10 2 5 9 795 TT 1045 2000 20 47 123 8 7 6 9 850 9 1 1115 19 43 117 8 2 7 3 855 9 6 1125 18 39 110 7 5 8 0 880 10 5 1160 117 35 101 7...

Page 66: ...0 65 149 12 2 4 9 735 6 5 965 2300 23 73 157 13 4 4 5 705 5 9 925 22 69 152 12 6 4 8 725 6 3 955 21 64 148 11 9 5 0 745 6 6 985 20 60 144 11 2 5 4 0 a 1015 2200 23 68 151 12 4 4 8 730 6 4 960 22 64 148 11 7 5 1 760 6 8 1000 21 60 144 11 0 5 5 185 7 2 1035 20 57 139 10 5 5 7 795 1 5 1045 2000 20 48 128 9 0 6 7 855 8 8 1125 19 45 121 8 5 71 855 9 3 1125 18 41 114 7 9 71 6 865 10 0 1140 17 37 105 7 3...

Page 67: ...8 58 144 11 0 5 5 785 7 2 1035 2300 21 66 153 12 2 4 9 750 6 5 990 20 62 149 11 6 5 2 770 6 8 1015 19 58 144 11 0 5 5 785 7 2 1035 18 54 139 10 5 5 7 95 7 5 1045 2200 21 62 149 11 4 5 3 785 6 9 1035 20 58 144 10 7 5 6 805 7 4 1065 19 54 139 10 2 5 9 820 7 7 1075 18 51 133 9 7 6 2 825 8 1 1085 2000 20 50 132 9 2 6 5 860 8 6 1135 19 41 126 8 7 6 9 870 9 1 1145 18 43 118 8 1 7 4 875 9 8 1150 17 39 10...

Page 68: ...65 16 51 137 10 0 6 0 820 7 9 1080 2300 19 60 149 11 1 5 4 805 7 1 1060 18 56 144 10 5 5 7 825 7 5 1085 17 51 137 9 8 6 1 840 8 1 1105 16 47 130 9 2 6 5 850 8 6 1115 2200 19 56 144 10 4 5 8 830 1 6 1095 18 52 138 9 8 6 1 845 8 1 1110 17 49 132 9 3 6 5 850 8 5 1120 16 45 124 8 7 6 9 855 9 1 1125 2000 19 48 130 8 9 6 17 875 8 9 1155 18 44 123 8 4 7 1 880 9 4 1155 17 40 115 7 8 7 7 885 10 1 1165 16 3...

Page 69: ... HOURS MILES 250 16 54 145 10 4 5 8 835 7 6 1100 15 50 139 9 8 6 1 850 8 1 1120 14 46 126 9 2 6 5 820 8 6 1080 2300 16 50 139 9 6 6 2 870 8 2 1145 15 a 1s oe 6 6 865 8 7 1135 14 42 13 85 m1 800 9 3 1050 2200 16 a 11 et 6 6 865 8 7 1135 15 44 120 8 6 7 0 835 9 2 1100 14 40 106 8 0 7 5 795 9 9 1045 2000 16 40 106 7 8 77 815 10 1 1075 15 37 971 7 3 8 2 795 10 8 1050 Figure 6 4 Sheet 5 of 5 6 8 ...

Page 70: ...Jomod puis 0197 UO POSE BIT UMOYS SSOUEISIT SELON S661 ovZ S0SL 089 OEVL o 9 0S lL 06S 69 0562 SEO Ld 08 840 Id 0S sd0 Ld 09 S90 1d 0 UVHTO OL TIOH VITIO OL 108 VVITO OL T1008 VAIO OL TTOH HAW SaNnoda TVLOL annoy TVLOL annoys TVLOL aNnouan TVLIOL aNnoEdn SVI LEOITM HOVOdddv SSoud d 28 B LATA 00SL 4 17 B LEA 0008 d 08 LEAL 005 J 6 B THAT VES AVMNNY Q3DV4aNS QYVH NO SdV1d oOF HLM 3DNVISIA ONIANVT 37...

Page 71: ...AS MAXIMUM GLIDE PROPELLER WINDMILLING FLAPS UP ZERO WIND eo SS a 18 000 16 000 14 000 12 000 10 000 8000 6000 4000 2000 HEIGHT ABOVE TERRAIN FEET 0 5 10 15 20 25 30 35 GROUND DISTANCE STATUTE MILES ee 1 Figure 6 6 6 10 ...

Page 72: ...nge When these tanks are installed the total usable fuel for all flight conditions is 79 gallons COLD WEATHER EQUIPMENT 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 ...

Page 73: ... type or bat tery cart the master switch should be turned ON The ground service plug receptacle circuit incorporates a polarity re versal protection Power from the external power source will flow only if the ground service plug is correctly connected to the airplane If the plug is accidentally connected backwards no power will flow to the airplane s electrical system thereby preventing any damage ...

Page 74: ...are planned installation of optional wick type static dischargers is recommended to improve radio communications during flight through dust or various forms of precipitation rain freez ing rain snow or ice crystals Under these conditions the build up and discharge of static electricity from the trailing edges of the wings rud der elevators propeller tips and radio antennas can result in loss of us...

Page 75: ...mbinations of switches are interlocked to prevent more than one system from being utilized at the same time Depressing one interlocked switch automatically disengages the others All of the selector switches are lighted anytime the navigation light switch is turned on When a switch is depressed its light becomes brighter This light intensity of a depressed switch can be controlled with the rheostat...

Page 76: ...n SPEAKER PHONE SWITCHES The speaker phone switches such as COM 1 NAV 1 400 series radios or REC 1 REC 2 300 series radios determine whether the output of the receiver in use is fed to the headphones or through the audio amplifier to the speaker Depress the switch for the desired receiver to obtain speaker operation or release it if headphone operation is desired AUTOPILOT OMNI SWITCH When a Nav O...

Page 77: ...dicators A remote shutoff valve control located adjacent to the pilot s oxygen outlet is used to shut off the supply of oxygen to the system when not in use The control is mechanically connected to the shutoff valve at the cylinder With the exception of the shutoff function the system is com pletely automatic and requires no manual regulation for change of altitude OXYGEN SYSTEM OPERATION Prior to...

Page 78: ...ITY 1800 1600 1400 nv 00 1000 800 600 GAGE PRESSURE PSl 400 200 7 Hii Ger Fe BC gE IF osl8 9 OXYGEN DURATION HOURS NOTE This chart is based on a pilot with an orange color coded oxygen line fitting and passengers with green color coded line fittings Figure 7 2 ...

Page 79: ...nect the mask lead to the adapter cord and plug the cord into the auxiliary microphone jack In aircraft that are equipped with the optional boom micro phone it will be necessary to disconnect the boom micro phone lead from the auxiliary microphone jack so that the adapter cord from the oxygen mask microphone can be plugged into the jack A switch is incorporated on the left hand control wheel to op...

Page 80: ... NOTE The Oxygen Duration Chart is based on a standard con figuration oxygen system having one orange color coded hose assembly for the pilot and green color coded hoses for the passengers If orange color coded hoses are provided for pilot and passengers it will be necessary to compute new oxygen duration figures due to the greater consumption of oxygen with these hoses This is accom plished by co...

Page 81: ...e airspeed indicator has a cali brated rotatable ring which works in conjunction with the airspeed indi cator dial in a manner similar to the operation of a flight computer TO OBTAIN TRUE AIRSPEED rotate ring until pressure altitude is aligned with outside air temperature in degrees Fahrenheit Then read true airspeed on rotatable ring opposite airspeed needle NOTE Pressure altitude should not be c...

Page 82: ...sh 65 power in level flight at 2450 RPM and part throttle 2 Carefully lean to peak EGT This is the reference EGT FLIGHT POWER CONDITION SETTING Ee REMARKS TAKE OFF Full throtfle 200 richer than Use FULL RICH mixture AND CLIMB and 2600 RPM REFERENCE EGT below 3000 NORMAL 23 MP and 125 richer than Above 10 000 use CLIMB 2450 RPM REFERENCE EGT BEST POWER mixture MAXIMUM CRUISE Peak minus 125 F BEST P...

Page 83: ...asible orduring the ground roll NOTE Enrichen mixture during climb if excessive cylinder head temperatures occur When leaning the mixture under some cruise conditions engine roughness may occur before peak EGT is reached In this case use the EGT corresponding to the onset of roughness as the reference point in stead of peak EGT Changes in altitude or power setting require the EGT to be rechecked M...

Page 84: ...he left side of the instrument panel to turn the system on and off A ROLL TRIM control knob on the Turn Coordinator is used for manual roll trim control to compensate for asymmetrical loading of fuel and passengers and to optimize system performance in climb cruise and let down OPERATING CHECK LIST TAKE OFF 1 WING LVLR Control Knob Check in off position full in CLIMB 1 Adjust elevator and rudder t...

Page 85: ... to turn the system off 2 It is recommended that the system not be engaged during take off and landing Although the system can be easily overpowered servo forces _could significantly alter the manual feel of the aileron control especially should a malfunction occur FUEL TANK QUICK DRAIN VALVE KIT Two fuel tank quick drain valves and a fuel sampler cup are available as a kit to facilitate daily dra...

Page 86: ...range where carburetor icing can occur a placard on the gage reads KEEP NEEDLE OUT OF YELLOW ARC DURING POSSI BLE ICING CONDITIONS Visible moisture or high humidity can cause carburetor ice formation especially in idle or low power conditions Under cruising conditions the formation of ice is usually slow providing time to detect the loss of manifold pressure caused by the ice Carburetor icing duri...

Page 87: ...ors Specification MHS 24A MUST BE USED CAPACITY OF ENGINE SUMP 12 Quarts Do not operate on less than 9 quarts To minimize loss of oil through breather fill to 10 quart level for normal flights of less than 3 hours For extended flight fill to 12 quarts The above quantities refer to oil dipstick level readings HYDRAULIC FLUID MIL H 5606 Hydraulic Fluid OXYGEN AVIATOR S BREATHING OXYGEN Spec No MIL 0...

Page 88: ... EssNA TAKE YOUR CESSNA HOME FOR SERVICE AT THE SIGN OF THE CESSNA SHIELD CESSNA AIRCRAFT COMPANY es WICHITA KANSAS ...

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