Cessna SKYLANE RG R182 Pilot Operating Handbook Download

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Summary of Contents for SKYLANE RG R182

Page 1: ...E RG 1978 MODEL R182 R18200450 Serial No _ Registration No 1 113 3_B_h _ THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY CAR PART 3 COPYRIGHT 1977 CESSNA AIRCRAFT COMPANY...

Page 2: ...tion affected by the revision is indicated by a vertical line in the outer margin of the page Dates of issue for original and revised pages are Original 0 10 October 1977 THE TOTAL NUMBER OF PAGES IN...

Page 3: ...ssna Dealers worldwide Specific benefits and provisions of warranty plus other important benefits for you are contained in your Customer Care Program book supplied with your airplane Warrantv service...

Page 4: ...er 50 Ft Obstacle STALL SPEED CAS Flaps Up Power Off Flaps Down Power Off MAXIMUM WEIGHT Ramp Takeoff or Landing STANDARD EMPTY WEIGHT Skylane RG Skylane RG II MAXIMUM USEFUL LOAD Skylane RG Skylane R...

Page 5: ...GENERAL 1 LIMITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 4 PERFORMANCE 5 WEIGHT BALANCE EQUIPMENT LIST 6 AIRPLANE SYSTEMS DESCRIPTIONS 7 AIRPLANE HANDLING SERVICE MAINTENANCE 8 SUPPLEMENTS Opt...

Page 6: ...ficated Weights 1 5 Standard Airplane Weights 1 5 Cabin And Entry Dimensions 1 5 Baggage Space And Entry Dimensions 1 5 Specific Loadings 1 5 Symbols Abbreviations And Terminology 1 0 General Airspeed...

Page 7: ...h nrobe lights Installed MaxImum height 5hown With nose gear jepressed all tires and nose strut properly inflated and Hashing inst IIE1d 3 Wheel base length is 65 4 Propeller ground clearance is il 11...

Page 8: ...Engine Model Number 0 540 J3C5D Engine Type Normally aspirated direct drive air cooled horizontally opposed carburetor equipped six cylinder engine with 541 5 cu in displacement Horsepower Rating and...

Page 9: ...otal of 50 hours has accumulated or oil consumption has stabilized NOTE The airplane was delivered from the factory with a corro sion preventive aircraft engine oil This oil should be drained after th...

Page 10: ...baggage areas A and B is 200 lbs STANDARD AIRPLANE WEIGHTS Standard Empty Weight Skylane RG 1734 lbs Skylane RG II 1794 lbs Maximum Useful Load Skylane RG 1378 lbs Skylane RG II 1318 lbs CABIN AND EN...

Page 11: ...use abrupt control travel Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position Maximum Landing Gear Extended Speed is the maximum speed at wh...

Page 12: ...tric scale h ts been set to 29 92 inches of mercury 1013 mb ENGINE POWER TERMINOLOGY BHP RPM MP Brake Horsepower is the power de oped by the engine Revolutions Per Minute is engine S c ed Manifold Pre...

Page 13: ...is the product of the weight of an item multiplied by its arm Moment divided by the constant 1000 is used in this handbook to simplify balance calculations by reduc ing the number of digits Center of...

Page 14: ...p fuel Gross Loaded Weight is the loaded weight of the airplane Maximum Takeoff Weight is the maximum weight approved for the start of the takeoff run Maximum Landing Weight is the maximum weight appr...

Page 15: ...d Indicator Markings Power Plant Limitations Power Plant Instrument Markings Weight Limits Center Of Gravity Limits Maneuver Limits Flight Load Factor Limits Kinds Of Operation Limits Fuel Limitations...

Page 16: ...E The 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 shown in Section 5 with the normal stati...

Page 17: ...550 Pounds 100 101 control movements above 2000 Pounds 89 89 this speed V FE Maximum Flap Extended I Speed To 100 Flaps 137 140 Do not excetd these speeds 10 40 Flaps 94 95 with the give l flap settin...

Page 18: ...T J l t J r With j I I j d Line 182 I McJxrlllurn speed for ail H rdtlons Figure 2 2 Airspeed Indicator Markings POWER PLANT LIMITATIONS Engine Manufacturer A vco Lycoming Engine Model Number 0 540 J3...

Page 19: ...245 F 245 F Cy II nder Head 200 500 F 500 F Temperature Fuel Pressure 0 5 psi 0 5 8 0 psi 8 0 psi 011 Pressure 25 psi 60 90 psi 100 psi Car buretor Air 15 to SoC Temperature Figure 2 3 Power Plant Ins...

Page 20: ...ental to normal flying stalls except whip stalls lazy eights chandelles and steep turns in which the angle of bank is not more than 600 Aerobatic maneuvers including spins are not approved FLIGHT LOAD...

Page 21: ...gallons Usable Fuel all flight conditions 75 U S gallons Unusable Fuel 5 0 U S gallons NOTE CESSNA MODEL R182 To ensure maximum fuel capacity when refueling place the fuel selector valve in either LE...

Page 22: ...tions as stated in the form of placards markings and manuals MAXIMUMS GROSS WEIGHT FLIGHT LOAD FACTOR Flaps Up Flaps Down 3100 Ibs 3 8 1 52 2 0 No acrobatic maneuvers including spins approved Altitude...

Page 23: ...IGHT 37 GAL LEVEL FLIGHT ONLY 5 On the baggage door 120 POUNDS MAXIMUM BAGGAGE AND OR AUXILIARY PASSENGER FORWARD OF BAGGAGE DOOR LATCH AND 80 POUNDS MAXIMUM BAGGAGE AFT OF BAGGAGE DOOR LATCH MAXIMUM...

Page 24: ...VIA TION GRADE GASOLINE CAPACITY 30 5 GAL Forward of fuel tank filler cap long range tanks SERVICE THIS AIRPLANE WITH 100LL l00 MIN AVIA TION GRADE GASOLINE CAPACITY 40 0 GAL 8 Near gear hand pump MAN...

Page 25: ...ng 3 5 Fires 3 5 During Start On Ground 3 5 Engine Fire In Flight 3 6 Electrical Fire In Flight 3 6 Cabin Fire 3 7 Wing Fire 3 7 Icing 3 7 Inadvertent Icing Encounter 3 7 Static Source Blockage Errone...

Page 26: ...ns Static Source Blocked Spins Rough Engine Operation Or Loss Of Power Carburetor Icing Spark Plug Fouling Magneto Malfunction Engine Driven Fuel Pump Failure Low Oil Pressure Landing Gear Malfunction...

Page 27: ...ould be considered and applied as necessary to correct the problem Emergency procedures associated with ELT and other optional systems can be found in Section 9 AIRSPEEDS FOR EMERGENCY OPERATION Engin...

Page 28: ...WITHOUT ENGINE POWER 1 Airspeed 70 KIAS flaps UP 65 KIAS flaps DOWN 2 Mixture IDLE CUT OFF 3 Fuel Selector Valve OFF 4 Ignition Switch OFF 5 Landing Gear DOWN UP if terrain is rough or soft 6 Wing Fla...

Page 29: ...PARALLEL TO SWELLS NOTE If no power is available approach at 70 KIAS with flaps up or at 65 KIAS with 100 flaps 7 Cabin Doors UNLATCH 8 Touchdown LEVEL ATTITUDE AT ESTABLISHED DESCENT 9 Face CUSHION a...

Page 30: ...f fire is not extinguished increase glide speed to find an airspeed which will provide an incombustible mixture 6 Forced Landing EXECUTE as described in Emergency Landing Without Engine Power ELECTRIC...

Page 31: ...to keep the flames away from the fuel tank and cabin and land as soon as possible using flaps only as required for final approach and touchdown ICING INADVERTENT ICING ENCOUNTER 1 Turn pitot heat swi...

Page 32: ...necessary for improved visibility 11 Approach at 85 to 95 KIAS depending upon the amount of ice accumulation 12 Perform a landing in level attitude STATIC SOURCE BLOCKAGE Erroneous Instrument Reading...

Page 33: ...nding Check COMPLETE 2 Approach NORMAL full flap 3 Landing Gear and Gear Pump Circuit Breakers IN 4 Landing TAIL LOW as smoothly as possible 5 Braking MINIMUM necessary 6 Taxi SLOWLY 7 Engine SHUTDOWN...

Page 34: ...e on good wheel as required ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS OVER VOLTAGE LIGHT ILLUMINATES 1 Avionics Power Switch OFF 2 Master Switch OFF both sides 3 Master Switch ON 4 Over Voltage Ligh...

Page 35: ...rn necessary to return to the runway The checklist procedures assume that adequate time exists to secure the fuel and ignition systems prior to touchdown After an engine failure in flight the best gli...

Page 36: ...til a landing is assured Premature deactivation of the switches will disable the encoding altimeter and airplane electrical sys tems LANDING WITHOUT ELEVATOR CONTROL Trim for horizontal flight with an...

Page 37: ...the miniature airplane 4 Check accuracy of the turn by observing the compass heading which should be the reciprocal of the original heading 5 If necessary adjust heading primarily with skidding motio...

Page 38: ...d to 80 KIAS 4 Adjust the elevator trim control to maintain an 80 KIAS glide 5 Keep hands off the control wheel using rudder control to hold a straight heading Use rudder trim to relieve unbalanced ru...

Page 39: ...variations in this configuration are 2 knots or less SPINS Intentional spins are prohibited in this airplane Should an inadvert ent spin occur the following recovery procedure should be used 1 RETARD...

Page 40: ...recommended lean setting for cruising flight If the problem does not clear up in several minutes determine if a richer mixture setting will produce smoother operation If not proceed to the nearest air...

Page 41: ...them at the same time to check for open dimming shutters A b ned out bulb can be replaced in flight by using the bulb from the rem ling gear position indicator light RETRACTION MALFUNCTIONS If the lan...

Page 42: ...larding gear lever to GEAR UP and push the LDG GEAR and GEAR PUMP circuit breakers in to allow the landing gear to swing into the gear wells at touchdown Then proceed in accordance with the checklist...

Page 43: ...he avionics power switch off then 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 light will go off Th...

Page 44: ...g Left Wing Leading Edge Left Wing Trailing Edge Before Starting Engine Starting Engine Before Takeoff Takeoff Normal Takeoff Short Field Takeoff Enroute Climb Normal Climb Maximum Performance Climb C...

Page 45: ...ower Check 4 15 Wing Flap Settings 4 16 Crosswind Takeoff 4 16 Landing Gear Retraction 4 16 Enroute Climb 4 17 Cruise 4 17 Leaning With A Cessna Economy Mixture Indicator EGT 4 19 Stalls 4 20 Before L...

Page 46: ...to the particular weight must be used 75 KIAS 112 KIAS 101 KIAS 89 KIAS 18 KNOTS 70 80 KIAS 65 75 KIAS 63 KIAS 70 80 KIAS 55 KIAS 90 100 KIAS 88 KIAS 74 KIAS 64 KIAS 66 InAS Takeoff Normal Climb Out S...

Page 47: ...snow from wing tail and control surfaces Also make sure that control surfaces contain no internal accumulations of ice or debris Prior to flight check that pitot heater if installed is warm to touch w...

Page 48: ...es CHECK freedom of movement and security G RIGHT WING Trailing Edge 1 Aileron CHECK freedom of movement and security RIGHTWING 1 Wing Tie Down DISCONNECT 2 Main Wheel Tire CHECK for proper inflation...

Page 49: ...ling use sampler cup and drain small quantity of fuel from fuel tank sump quick drain valve to check for water sediment and proper fuel grade 3 Fuel Quantity CHECK VISUALLY for desired level 4 Fuel Fi...

Page 50: ...t Controls FREE and CORRECT 4 Flight Instruments SET 5 Fuel Selector Valve BOTH 6 Mixture RICH 7 Auxilary Fuel Pump ON check for rise in fuel pressure then OFF NOTE In flight gravity feed will normall...

Page 51: ...el is lifted the gear motor may run 1 2 seconds to restore hydraulic pressure 5 Climb Speed 70 KIAS flaps 20 80 KIAS flaps UP 6 Brakes APPLY momentarily when airborne 7 Landing Gear RETRACT in climb o...

Page 52: ...er 15 23 INCHES Hg 2100 2400 RPM no more than 75o c power 2 Elevator and Rudder Trim ADJUST 3 Mixture LEAN 4 Cowl Flaps CLOSED DESCENT 1 Power AS DESIRED 2 Carburetor Heat AS REQUIRED to prevent carbu...

Page 53: ...HEEL GENTLY 7 Braking MINIMUM REQUIRED SHORT FIELD LANDING 1 Airspeed 70 80 KIAS flaps UP 2 Wing Flaps 40 below 95 KIAS 3 Airspeed MAINTAIN 63 KIAS 4 Trim ADJUST 5 Power REDUCE to idle as obstacle is...

Page 54: ...RMAL PROCEDURES 1 Parking Brake SET 2 Throttle IDLE 3 Avionics Power Switch Electrical Equipment OFF 4 Mixture IDLE CUT OFF pulled full out 5 Ignition Switch OFF 6 Master Switch OFF 7 Control Lock INS...

Page 55: ...nders begin to fire open the throttle slightly to keep it running If prolonged cranking is necessary allow the starter motor to cool at frequent intervals since excessive heat may damage the armature...

Page 56: ...TOR USE DOWN AILERON ON LH WING AND DOWN ELEVATOR USE DOWN AlLERON ON RH WING AND DOWN ELEVATOR fJL N r CODE NOTE WIND DIRECTION Strong quartering tail winds require caution Avoid sudden bursts of the...

Page 57: ...M differen tial between magnetos If there is a doubt concerning operation of the ignition system RPM checks at higher engine speeds will usually confirm whether a deficiency exists An absence of RPM d...

Page 58: ...wing flaps are used for takeoff they should be left down until all obstacles are cleared and a safe flap retraction speed of 75 KIAS is reached To clear an obstacle with wing flaps 20 an obstacle clea...

Page 59: ...is 88 KIAS at sea level decreasing to 74 KIAS at 10 000 feet If an obstruction ahead requires a steep climb angle a best angle of climb speed should be used with landing gear and flaps up and maximum...

Page 60: ...wer that will provide smooth engine operation The cowl flaps should be opened if necessary to ulaintain the cylinder head temperature at approximately two thirds of the normal operating range green ar...

Page 61: ...shown on the optional Cessna Economy Mixture Indicator may be used as an aid for mixture leaning in cruising flight at 75 power or less To adjust the mixture using this indicator lean to establish the...

Page 62: ...arded below 12 inches of manifold pressure and or the wing flaps extended beyond 25 and visual inspection of the main gear position Should the gear indicator light fail to illuminate the light should...

Page 63: ...nd to break loose or limber the oil thus conserving battery energy 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 eith...

Page 64: ...rapidly to full open four times Return to 1 2 inch open position 6 Ignition Switch START 7 Release ignition switch to BOTH when engine starts 8 Continue to prime engine until it is running smoothly o...

Page 65: ...ration of the engine in cold weather the appropriate use of carburetor heat may be necessary The following procedures are indicated as a guideline 1 Use the minimum carburetor heat required for smooth...

Page 66: ...ing departure from or approach to an airport climb after takeoff and descent for landing should be made so as to avoid prolonged flight at low altitude near noise sensitive areas NOTE The above recomm...

Page 67: ...Climb Maximum Figure 5 6 Time Fuel And Distance To Climb Maximum Rate Of Climb Time Fuel And Distance To Climb Normal Climb Figure 5 7 Cruise Performance 2000 Feet Cruise Performance 4000 Feet Cruise...

Page 68: ...opeller condition and air turbulence may account for variations of 107c or more in range and endurance Therefore it is important to utilize all available information to estimate the fuel required for...

Page 69: ...akeoff distance informacion presented for a weight of 3100 pounds pressure altitude of 2000 feet and a temperature of 30 C should be used and results in the following Ground roll Total distance to cle...

Page 70: ...shows a corresponding 5 5 hours Using th s information the estimated distance can be determined for the expected _ knot headwind at 7500 feet as follows Range zero wind Decrease in range due to wind...

Page 71: ...above standard the correction would be 16 C lO0 C x 10 16 Increase With this factor included the fuel estimate would be calculated as follows Fuel to climb standard temperature Increase due to non sta...

Page 72: ...ing fuel required to complete the trip with ample reserve LANDING A procedure similar to takeoff should be used for estimating the landing distance at the destination airport Figure 5 10 presents land...

Page 73: ...FLAPS UP KIAS 50 60 70 80 90 100 110 120 130 140 150 160 170 KCAS 60 66 73 81 90 99 109 118 128 137 146 155 165 FLAPS 20 KIAS 40 50 60 70 80 90 95 KCAS 54 59 65 73 81 90 95 FLAPS 40 KIAS 40 50 60 70 8...

Page 74: ...95 ALTERNATE KIAS 51 62 73 84 94 99 FLAPS 40 NORMAL KIAS 40 50 60 70 80 90 95 I ALTERNATE KIAS 39 51 62 73 82 92 96 HEATER VENTS OPEN AND WINDOWS CLOSED FLAPS UP I JORMAL KIAS 60 70 80 90 100 110 120...

Page 75: ...SECTION 5 PERFORMANCE CESSNA MODEL R182 TEMPERATURE CONVERSION CHART DEGREES CELSIUS Figure 5 2 Temperature Conversion Chart 5 10...

Page 76: ...ANGLE OF BANK WEIGHT FLAP 0 30 45 60 LBS DEFLECTION KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS UP 40 54 43 58 48 64 57 76 3100 20 38 51 41 55 46 61 55 72 40 35 50 38 54 43 59 52 71 MOST FORWARD CENTER OF...

Page 77: ...grass runway increase distances by 15 of the ground roll figure TAKEOFF OOC 10 C 20 C 30 C 40 C SPEED PRESS WEIGHT KIAS ALT TOTAL TOTAL TOTAL TOTAL TOTAL LBS LIFT AT FT GRND TO CLEAR GRND TO CLEAR GRN...

Page 78: ...20 4000 820 1585 885 1705 950 1835 1020 1975 1095 2125 5000 900 1745 970 1880 1040 2025 1120 2185 1200 2355 6000 985 1925 1060 2080 1140 2250 1225 2430 1315 2630 7000 1080 2140 1165 2315 1255 2510 135...

Page 79: ...y be leaned above 3000 feet for increased power CESSNA MODEL R182 WEIGHT PRESS CLIMB RATE OF CLIMB FPM ALT SPEED LBS FT KIAS 20 C OOC 20 C 40 C 3100 S L 88 1270 1195 1120 1045 2000 85 1110 1035 960 89...

Page 80: ...for each lOoC above standard temperature 4 Distances shown are based on zero wind PRESSURE CLIMB RATE OF FROM SEA LEVEL WEIGHT TEMP ALTITUDE c SPEED CLIMB TIME FUEL USED DISTANCE LBS FT KIAS FPM MIN G...

Page 81: ...ase time fuel and distance by 10 for each lOoC above standard temperature 4 Distances shown are based on zero wind PRESSURE RATE OF FROM SEA LEVEL WEIGHT ALTITUDE TEMP CLIMB LBS FT c FPM TIME FUEL USE...

Page 82: ...9 146 12 4 21 69 140 12 4 67 141 12 0 64 142 11 6 20 64 136 11 6 62 137 11 3 60 138 10 9 2300 23 75 145 13 5 72 146 13 1 70 147 12 6 22 71 141 12 7 68 142 12 3 66 143 11 9 21 66 137 11 9 64 138 11 5 6...

Page 83: ...1 150 12 8 21 71 144 12 8 69 145 12 4 66 146 12 0 20 66 140 12 0 64 141 11 6 62 142 11 2 2300 23 77 149 14 0 75 150 13 5 72 151 13 0 22 73 145 13 1 70 147 12 7 68 148 12 2 21 68 142 12 3 66 143 11 9 6...

Page 84: ...2 7 68 151 12 3 20 69 145 12 3 66 146 11 8 64 147 11 5 19 64 140 11 5 61 141 11 1 59 142 10 8 2300 23 77 155 13 9 74 156 13 4 22 75 150 13 5 72 151 13 0 70 152 12 6 21 70 146 12 7 68 IJ7 12 2 66 148 1...

Page 85: ...0 71 149 12 7 68 150 12 3 66 151 11 9 19 66 145 11 9 63 146 11 5 61 147 11 1 18 61 140 11 1 59 141 10 7 57 142 10 3 2300 21 73 151 13 1 70 152 12 6 68 153 12 2 20 68 147 12 2 65 148 11 8 63 149 11 4 1...

Page 86: ...2 19 68 149 12 2 65 150 11 8 63 151 11 4 18 63 145 11 4 60 145 11 0 58 146 10 6 17 58 140 10 6 56 140 10 2 54 141 9 9 2300 20 70 151 12 6 7 152 12 2 65 153 11 8 19 65 147 11 8 63 18 11 4 61 19 1 0 18...

Page 87: ...KTAS GPH BHP BHP BHP 2400 18 65 149 11 7 62 150 11 3 60 151 10 9 17 60 144 10 9 57 145 10 5 55 145 10 1 16 55 138 10 0 53 139 9 7 51 139 9 4 15 50 132 9 2 48 132 8 8 46 132 8 6 2300 18 62 147 11 3 60...

Page 88: ...Zero Wind SECTION 5 PERFORMANCE NOTES 1 This chart allows for the fuel used for engine start taxi takeoff and climb and the distance during a normal climb as shown in figure 5 6 2 Reserve fuel is base...

Page 89: ...This chart allows for the fuel used for engine start taxi takeoff and climb and the distance during a normal climb as shown in figure 5 6 2 Reserve fuel is based on 45 minutes at 45 BHP and is 6 3 gal...

Page 90: ...Cruise Standard Temperature SECTION 5 PERFORMANCE NOTES 1 This chart allows for the fuel used for engine start taxi takeoff and climb and the time during a normal climb as shown in figure 5 6 2 Reserv...

Page 91: ...d the time during a normal climb as shown in figure 5 6 2 Reserve fuel is based on 45 minutes at 45 BHP and is 6 3 gallons ce t uJ 3 O l t 0 j l j I i 8 9 j T I 1 1 I t 6 7 ENDURANCE HOURS 5 S L 4 400...

Page 92: ...L TOTAL TOTAL TOTAL KIAS FT GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR GRND TO CLEAR ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OBS ROLL 50 FT OSS 3100 63 S L 570 1270 590 13...

Page 93: ...N 6 WEIGHT BALANCE EQUIPMENT LIST SECTION 6 WEIGHT BALANCE EQUIPMENT LIST TABLE OF CONTENTS Page Introduction Airplane Weighing Procedures Weight And Balance Baggage Tie Down Equipment List 6 3 6 3 6...

Page 94: ...sliding seats to the most forward position e Raise flaps to the fully retracted position f Place all control surfaces in neutral position 2 Leveling a Place scales under each wheel minimum scale capa...

Page 95: ...Left Wheel L Right Wheel R Nose Wheel N Sum of Net Weights As Weighed W x ARM A N x 8 X W x IN Item Weight Lbs Moment l 000 X C G Arm In Lbs In Airplane Weight From Item 5 page 6 3 Add Oil 9 Qts at 7...

Page 96: ...ce SAMPLE WEIGHT AND BALANCE RECORD f t I I AI RP1LAN E J S E RIA L NUMBE R __ WEIGHT CHANGE t IT EM NO OESC RIPTI ON i A O O E O t j R E M O V E O 1 OATE OF ARTICLE OR MOOIFiCATiON in Out Wt Arm Mome...

Page 97: ...ied then list these on the loading problem NOTE Loading Graph information for the pilot passengers and baggage is based on seats positioned for average occu pants and baggage items loaded in the cente...

Page 98: ...of the wheel well and slightly inboard of each sidewall approximately at station 124 When the cabin floor Baggage A only is utilized for baggage the four eyebolts located on the cabin floor may be us...

Page 99: ...arenthesis indicate forward and aft limits of occupant center of gravity range Baggage area center of gravity NOTE The aft baggage wall approximate station 134 can be used as a convenient interior ref...

Page 100: ...BOTTOM FRONT CABINDOOR 1 32 I 36 1 h 41 BAGGAGEDOOR 15 15 3 1 22 HEIGHT R EAR 38 1 1 20 Iii WIDTH e LWR WINDOW LI N E CABIN FLOOR I J 0 i I I I I 20 30 40 50 60 70 80 90 100 110 65 3 CABIN WIDTH MEASU...

Page 101: ...lot and Front Passenger Sta 32 to 50 340 12 6 4 Second Row Passengers 340 25 2 5 Baggage Area A or Passenger on Child s Seat Station 82 to 110 120 Lbs Maximum 120 11 6 6 Baggage Aft Area B Station 110...

Page 102: ...ding Graph 100 50 LOADING GRAPH 5 10 15 20 25 30 35 LOAD MOMENT lOOO POUND INCHES NOTE Line rf fJresentillg adjuslJble seats shows the pilot and front seat passenger center of gravity on adjustable se...

Page 103: ..._ _ r I G rt t V 1 2800 t t t t t h lI oI _ _ _ _ t y n 2700 h lf _ i f 1 1200 I 2600 t t t t _ _ _ _ _ _A__ r ___ _ _ _ _ t 1150 G w 2500 t _ _ _ _ b f ff JI Il It t v jV e 1100 ii 2400 t t t t t bi...

Page 104: ...I 40 41 42 43 44 45 INCHES AFT OF DATUM STA 0 0 MILLIMETERS AFT OF DATUM iSTA 0 0 1000 1050 1100 1150 I I CENTER OF GRAVITY LIMITS Figure 6 8 Center of Gravity Limits 1 AIHPLANE CG LOCATION 900 950 I...

Page 105: ...00450 WORef 50158 WB Date 10 Jan 2000 Previous data taken from document dated 27 Jan 1995 Previous useful load 1223 45 Model I Part NO ITEMS REMOVED Description Previous data Weight CG Arrtl 1876 55 3...

Page 106: ...P AM FM S t i 0 y r O 7 I Fr1C t ED 1 2 ea KX 170B Nav Com 2a KMA 20 Audio F anel 3 KLN 30B I iF S 4 KR 86 KA 448 ADF 5 KT 7G Transponder NElrJ DATA NEW EMPTY WEIGHT REG NO N1338W lrJE I GHT 187 1 5 1...

Page 107: ...7 135 229 5 Panels 2 5 11 7 29 25 car stereo 3 17 51 0 ITOTAL REMOVED 24 34 45 85343468 1116 0726 NEW EQUIPMENT WEIGHT ARM MOMENT Stec 55X comp 2 7 15 40 5 roll servo 2 9 30 87 Ipitch servo 29 136 394...

Page 108: ...5 standard equipment items 0 optional equipment items replacing required or standard items A optional equipment items which are in addition to required or standard items A reference drawing column pro...

Page 109: ...T 1 1 K AL T fPNATlJP E VlL T 60 I MP fllL L nL H OIL FILTeR Pp 1P L L FK 1 C ALJ LEY f 2f 3 4C 2 14 9 OU H R t l GOVUHJCR Pf llPf LLEy MCCAlJU 02S0 J Ti61 SPII If JEP II STt LL ATIli PPLPELlfC SPINN...

Page 110: ...AR JlNC SW ITCH LISt TS INST LMEI T PUST PANEL LIGHTS E LEC T O LU I t F SCUd L I GH S Cn UP Tf SY N ETC t AN E FUEL P UM P AU CETECTnPS NAvIGATIP l LIGHT SET CF Zl l MN I FL ASH NG bE ACU N LI GH T L...

Page 111: ...I IRF Ie G r 11 SYSHM Ii Tl J l TC PI U T f IRE CT1L AL INI IC lITUR AlTITUDE I I IC6TCF t 05fS FITlINGS S E CLAIJPS tTC Gnr SYSTE It STL FlR f f v C M TIr 300t AUTlP1LC1T elF t CT I 1N1 L I I I 111...

Page 112: ...iF L ttl lI E S 4 T CC V R S f f T C 1 NGU fJPENAEL E F f i eM 1 DC R v I NU I f r T CHAf GEJ W I 1J U S 1 VE HAn CAH I N TCP NET CHANG EI VEf 1 TIL TIl r S i Sl M 2 f J f r h SE ATI f l CUP lLl P PU...

Page 113: ...Gq 2 4 T AI L I 1 ELI FT t A LJ LE S eTC F 2 I n rsT V G F I G S D E L LE I 1 1 SH LLED CCl H C S I r p rlr F I G I NTH f L STt TIC DISCH H E S SeT OF 10 ST 8ILIlH Ar Rt STO j GOinS TrJ IfAP Cl IKC A...

Page 114: ...P ECElVi R 4 E 11 0 3312 400 Af H mA IN STl 3960133 1 0 2 188 0 PACIO DOL It G 11 STL 3930152 7 0 1 6 5 0 If IN G 3950136 0 8 7 1 2 HJ4 A 2 CES SN A 400 OM f INS TL 3910167 18 14 8 104 4 u SE n wI1H S...

Page 115: ...LA VE 0 3910 1 5 7 5 38 4 I S I t STL 3930195 1 5 2f 14 0 IN 0 ICA TUf 1 469li 2000 it 9 CuN T 41038 0000 0 5 VOf LUC CONVEFzHF INSTL 3940252 1 1 1 132 1 rm VEl TEF 4 7240 DJOJ 0 1 r lCu T 43270 0 OCJ...

Page 116: ...P STL v IF 11 G CE Si jt 4 J FAi SP l lJ R Sl lF iS ITF H1u A l F CEPT 1 C1 lt hT SC A XC ik li STL f f P L CE S 3 C1 2 1 5 N f C T CHAN GE r I ST CC r AV LCJ 7 0 Cf ANMl cc R UJC C ECt I V t TP t S 1...

Page 117: ...SECllNC C NAIy U 720 CHAf C VC LC RE fIV TP NSMITTEP Rl 385AI VOF LJC I OIU TrF IN 385A f 37 A Sr lND rue INSH ITEMS II C L T Xl SEreNe 400 Nt CUM 72C CHAI C M VCR lCC P CEIVEQ TRtNSMITTEP t T 4d5A V...

Page 118: ...S TL NIl I 5 E F I L TER INS TL i 1 t 1 ANT HJ 5 TL VI F AN T INS 1t to UC I en NTR I L PM r L U S TL EACP t NE I f 51 L FL Sr t Ol DEP U S TL Turf K 1NE INS Tl Af TENN 1 J Lr PTOP INSTL F I f S T rj...

Page 119: ...CO ADf R 546E f 1C A I CF SSN 3 CO TR At SpeND ER P n 5 9 A f 22 A l FIFST 3CC NAv CO RT 385Al t 2E A l E IfPG f jC LOU TeR TRAI SMITTER l A l C SSf JA 2COA ALTO PILeT NAV P t C S t YL II ERG I I 0 LY...

Page 120: ...gency Hand Pump 7 12 Landing Gear Warning System 7 13 Baggage Compartment 7 13 Seats 7 13 Seat Belts And Shoulder Harnesses 7 14 Seat Belts 7 15 Shoulder Harnesses 7 15 Integrated Seat Belt Shoulder H...

Page 121: ...ting System Pitot Static System And Instruments Airspeed Indicator Rate Of Climb Indicator Altimeter Vacuum System And Instruments Attitude Indicator Directional Indicator Suction Gage Stall Warning S...

Page 122: ...ng nose wheel The externally braced wings containing the fuel tanks are con structed of a front and rear spar with formed sheet metal ribs doublers and stringers The entire structure is covered with a...

Page 123: ...SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS AILERON CONTROL SYSTEM RUDDER AND RUDDER TRIM CONTROL SYSTEMS CESSNA MODEL R182 Figure 7 1 FHght Control and Trim Systems Sheet 1 of 2 7 4...

Page 124: ...CESSNA MODEL R182 SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS ELEVATOR CONTROL SYSTEM ELEVATOR TRIM CONTROL SYSTEM Figure 7 1 Flight Control and Trim Systems Sheet 2 of 2 7 5...

Page 125: ...o 2 3 4 6 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27...

Page 126: ...arker Beacon Indicator 42 Fuel Selector Light I S l Lights and Switches 43 Elevator Trim Control Wheel J 15 Rear View Mirror 44 Control Pedestal Light t 16 Audio Control Panel 45 Landing Gear Lever Z...

Page 127: ...ls They consist of a rudder pedal face two spacers and two spring clips To install an exten sion place the clip on the bottom of the extension under the bottom of the rudder pedal and snap the top cli...

Page 128: ...bin heat cabin air and defroster control knobs and the cigar lighter A pedestal extending from the switch and control panel to the floorboard contains the elevator and rudder trim control wheels cowl...

Page 129: ...e bulkhead just forward of the horizontal stabilizer to raise the nose wheel off the ground WING FLAP SYSTEM The wing flaps are of the single slot type see figure 7 3 and are extended or retracted by...

Page 130: ...right side of the power pack adjacent to the motor mounting flange The system should be checked at 25 hour intervals and anytime a hydraulic failure in the system requires the use of the emergency ha...

Page 131: ...osition During a normal cycle the gear locks up or down limit switches close and the indicator light comes on amber for up and green for down indicating completion of the cycle After indicator light i...

Page 132: ...he landing gear retracted BAGGAGE COMPARTMENT The baggage compartment consists of the area from the back of the rear passenger seats to the aft cabin bulkhead A baggage shelL above the wheel well exte...

Page 133: ...r support The seat backs will also fold full forward The rear passengers seats consist of a fixed one piece seat bottom with individually adjustable seat backs Two adjustment levers on the left and ri...

Page 134: ...he window line and is stowed behind a stowage s ath above the cabin door To stow the harness fold it and place it behind he sheath When rear seat shoulder harnesses are furnished they are a tched adja...

Page 135: ...H IL ll Ecici 11 11 T HU 1 1 1 11 J ltl T JIIIK lust IH 1 I s lilulclt r I n l pulj 1l1 1 I irrll s 1 JWll I lelt llICh h 1 I 1 1 1 Hler 1I 11 ldF1St lhk 1 1 1 I II t tl ilt Jl IIUl UlEHII r i l U ECT...

Page 136: ...airplane is accomplished through either of two entry doors one on each side of the cabin at the front seat positions refer to Section 6 for cabin and cabin door dimensions The doors incorporate a rece...

Page 137: ...ow are of the fixed type and cannot be opened CONTROL LOCKS A control lock is provided to lock the ailerons and elevator control surfaces in a neutral position and prevent damage to these systems by w...

Page 138: ...eration is monitored by the following instruments oil pressure gage oil temperature gage cylinder head temperature gage tachometer manifold pressure gage and fuel pressure gage An economy mixture EGT...

Page 139: ...sures exhaust gas temperature and transmits it to the indicator The indicator serves as a vi sual aid to the pilot in adjusting the mixture during climb or cruise as described in Section 4 Exhaust gas...

Page 140: ...op of the crankcase near the front of the engine The dipstick and oil filler are accessible through doors on the engine cowling The engme should not be operated on less than five quarts of oil To mini...

Page 141: ...round the left muffler through a duct to a valve in the a irbox operated by the carburetor heat control on the cnstrument panel Heated air from the muffler shroud is obtained from unfiltered air insid...

Page 142: ...n Anytime the lever is repositioned it must first be moved to the right While in cruise flight cowl flaps should be adjusted to keep the cylinder head temperature at approximately two thirds of the no...

Page 143: ...fuel pump and carburetor Refer to figure 7 5 for fuel quantity data for both systems Fuel flows by gravity from the two wing tanks to a four position selector valve labeled BOTH RIGHT LEFT and OFF Wit...

Page 144: ...INE PRIMEH TO E GINE CYUNTIEW FUEL SELECTOR VALVE FeEL STR I EH THROTTLE IJXTeRE CONTROL KNOB fh l _ uY t __ L XlLIAHY FeEL peMP SWITCH LEFT FUEL TANK L1 TJ l llSun Jtl LX1 nUlll fUl l dunJl n fut lil...

Page 145: ...his gage is not indicating an electrical malfunction has occurred The auxiliary fuel pump switch is located on the left side of the switch and control panel and is a rocker type switch It is laoeled A...

Page 146: ...to the pump and other components in the system The electrical portion of the power pack is protected by a 30 amp push pull type circuit breaker switch labeled GEAR PUMP on the left switch and control...

Page 147: ...i 1 LL f T NIJ HlliHT MAIN lil AI I JV N I CK Figure 7 7 Hydraulic System I H 1 I i DOWN lOtT ACTUA lOll nm vN lICK AL I UA 1UI CONUI ltlt II I L I I ur jHOUNU If i n ANI Ill CiHICAI P f Oil I I X II...

Page 148: ...d of immediate attention If during taxi or landing roll braking action decreases let up on the pedals and then re apply the brakes with heavy pressure If the brakes become spongy or pedal travel incre...

Page 149: ...SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS CESSNA MODEL R182 1 00 f G T tU Figure 7 8 Electrical System 7 30...

Page 150: ...the right side of the avionics circuit breaker panel and is 01 1 c he up positlOn and OFF r the down position With the switch in the OFF r osition no electrical p ver vei il be applied to the avionic...

Page 151: ...e BAT portion turned on CIRCUIT BREAKERS AND FUSES Most of the electrical circuits in the a irplane are protected by push to reset circuit breakers mounted on the lower left side of the switch and con...

Page 152: ...thereby preventing any damage to electrical equipment The battery and external power circuits have been designed to com pletely eliminate the need to jumper across the battery contactor to close it fo...

Page 153: ...rside of the antiglare shield and two red flood lights in the forward part of the overhead console The lights are utilized by adjusting light intensity with the large outer control knob of the concent...

Page 154: ...light intensity is controlled by the FLOOD large outer control knob The pilot s control wheel map light if installed illuminates the lower portion of the cabin in front of the pilot and is used for ch...

Page 155: ...E RAM AIR FLOW VENTILATING AIR HEATED AIR BLENDED AIR MECHANICAL CONNECTION AIRFLOW ADJUSTMENT WHEELS J7 ADJUSTABLE AIH OUTLETS 8 ADJUSTABLE VENTILATORS 0 0 r REARCABIN tf J AIR OUTLETS CABIN HEAT DEF...

Page 156: ...t farther maximum heat is available with the CABIN HEAT knob pulled out and the CABIN AIR knob pushed full in Separate adjustable ventilators supply additional ventilation air to the cabin One near ea...

Page 157: ...reen arc 42 to 143 knots yellow arc 143 to 182 knots and a red line 182 knots If a true airspeed indicator is installed it is equipped with a rotatable ring which works in conjunction with the airspee...

Page 158: ...tch and roll attitudes are presented by a miniature airplane in relation to the horizon bar A knob at the bottom of the instrument is provided for in flight adjustment of the miniature airplane to the...

Page 159: ...0 0 o 0 0 0 o 0 0 o 0 0 0 0 0 0 0 VACUUM SYSTEM AIR FILTER t OVERBOARD VENT LI NE I VACUUM PUMP VACUUM RELIEF VALVE t I DI RECTIONAL INDICATOR i i ATTITUDE II IDICATOR CODE c J INLET AIR E VAC UUM DIS...

Page 160: ...perational if the warning horn sounds as the vane is pushed upward AVIONICS SUPPORT EQUIPMENT The airplane may at the owner s discretion be equipped with various types of avionics support equipment su...

Page 161: ...1 2 3 NAV COM ADF AUTO 1 2 3 1 2 0 0 Q 00FF XMTR L r PH ONE 1 TRANSMITTE R 5 EL I SE LECTOR SWITCH AUTOMATIC AUDIO SELECTOR SWITCH AUDIO SELECTOR SWITCH TYPICAL As illustrated the number 1 transmitter...

Page 162: ...lect any transmitter and its associated NAV COM receiver audio simultaneously with the transmitter selector switch If automatic audio selection is not desired the AUTO selector switch should be placed...

Page 163: ...ing other control operations to handle a hand held micr Jphone Also pas sengers need not listen to all communications The microphone and headset jacks are located near the lower left corner of tlh ins...

Page 164: ...rogressive Care Cessna Customer Care Program Pilot Conducted Preventive Maintenance Alterations or Repairs Ground Handling Towing Parking Tie Down Jacking Leveling Flyable Storage Servicing Engine Oil...

Page 165: ...te Number PC and Type Certificate Number TC i 2an be found on the Identification Plate located on the left forward doorpc st Located adjacent to the Identification Plate is a Finish and Trim Plate 7hi...

Page 166: ...ll available items many of which he keeps on hand He will be happy to place an order for any item which is not in stock AIRPLANE FILE There are miscellaneous data information and licenses that are a p...

Page 167: ...spection every 100 hours of operation The FAA may require other inspections by the issuance of airworthi ness directives applicable to the airplane engine propeller and compo nents It is the responsib...

Page 168: ...nel accomplish all required FAA inspections and most of the manufacturer recommended inspections CESSNA CUSTOMER CARE PROGRAM Specific benefits and provisions of the CESSNA WARRANTY plus other importa...

Page 169: ...which must be accomplished by appropriately licensed personnel ALTERATIONS OR REPAIRS It is essential that the FAA be contacted prior to any alterations on the airplane to ensure that airworthiness of...

Page 170: ...ecure to a ramp tie down 5 Install a pitot tube cover JACKING When a requirement exists to jack one or both ma in gear the entire airplane should be jacked by using the wing jack points Refer to the S...

Page 171: ...ut off position and the airplane is secured before rotating the propeller by hand Do not stand within the arc of the propeller blades while turning the propeller After 30 days the airplane should be f...

Page 172: ...corrosion preven tive aircraft engine oil This oil should be drained after the first 25 hours of operation and the following oils used as specified for the average ambient air temperature in the opera...

Page 173: ...ORS 100LL Grade Aviation Fuel Blue 100 Formerly 100 130 Grade Aviation Fuel Green CAPACITY EACH STANDARD TANK 30 5 Gallons CAPACITY EACH LONG RANGE TANK 40 0 Gallons NOTE To ensure maximum fuel capaci...

Page 174: ...require no polishing or buffing Approximately 15 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 In the e...

Page 175: ...solvent LANDING GEAR CARE Cessna Dealer s mechanics have been trained in the proper adjustment and rigging procedures on the airplane hydraulic system To assure trouble free gear operation have your...

Page 176: ...upholstery and carpet may be cleaned with foam type deter gent used according to the manufacturer s instructions To minimize wetting the fabric keep the foam as dry as possible and remove it with a va...

Page 177: ...pe ASB 125 Cessna 400 Nav Com Type RT 485A Cessna 400 Nav Com Type RT 485A With Cessna 400 Area Navigation System Type RN 478A Cessna 400 Area Navigation System Type RN 478A Cessna 400 ADF Type R 446A...

Page 178: ...m which may be installed in the airplane Each supplement contains a brief description and when applicable operating limitations emergency and normal procedures and performance Other routinely installe...

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Cessna SKYLANE RG R182, Pilot Operating Handbook

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