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Cessna 182T 2001, Pilot Operating Handbook

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Cessna 182T 2001 Pilot Operating Handbook Download Page 232

SECTION 8

CESSNA

HANDLING, SERVICE & MAINTENANCE

MODEL 182T

IDENTIFICATION PLATE

All correspondence regarding your airplane should include the

Serial Number. The Serial Number, Model Number, Production
Certificate Number (PC) and Type Certificate Number (TC) can be
found on the Identification Plate, located on the aft left tailcone.  A
secondary Identification Plate is also installed on the lower part of
the left forward doorpost. Located adjacent to the secondary
Identification Plate is the Finish and Trim Plate which contains a
code describing the exterior paint combination of the airplane. The
code may be used in conjunction with an applicable Illustrated Parts
Catalog if finish and trim information is needed.

CESSNA OWNER ADVISORIES 

Cessna Owner Advisories are sent to Cessna Aircraft FAA

Registered owners of record at no charge to inform them about
mandatory and/or beneficial aircraft service requirements and
product changes.  Copies of the actual bulletins are available from
Cessna Service Stations and Cessna Customer Service.

8-4

Apr 30/01

Summary of Contents for 182T 2001

Page 1: ...required to be furnished to the pilot by FAR Part 23 and constitutes the FAA Approved Airplane Flight Manual COPYRIGHT 2001 Cessna Aircraft Company Wichita Kansas USA Original Issue 23 February 2001...

Page 2: ...PROVIDED FOR THE AIRPLANE IDENTIFIED ON THE TITLE PAGE ON _____________ SUBSEQUENT REVISIONS SUPPLIED BY CESSNA AIRCRAFT COMPANY MUST BE PROPERLY INSERTED ___________________ Cessna Aircraft Company A...

Page 3: ...ART NUMBER MODEL 182T Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Serial Numbers 18280945 and On Original Issue 23 February 2001 Revision 1 30 April 2001 PART NUMBER 182TPHUS01...

Page 4: ......

Page 5: ...re contained in the Customer Care Program Handbook supplied with your airplane The Customer Care Card assigned to you at delivery will establish your eligibility under warranty and should be presented...

Page 6: ...ime 5 4 HRS 75 Power at 8000 Ft Range 813 NM 87 Gallons Usable Fuel Time 5 8 HRS Max Range at 10 000 Ft 55 Power Range 930 NM 87 Gallons Usable Fuel Time 7 6 HRS RATE OF CLIMB AT SEA LEVEL 924 FPM SER...

Page 7: ...NE Textron Lycoming IO 540 AB1A5 230 BHP at 2400 RPM PROPELLER Diameter 3 Blade 79 IN NOTE The above performance figures are based on the indicated weights standard atmospheric conditions level hard s...

Page 8: ...are individual documents and may be issued or revised without regard to revision dates which apply to the POH itself These supplements contain their own Log of Effective Pages which should be used to...

Page 9: ...age within the POH At original issue all pages will contain the same date As revisions to the POH occur these dates will change on effected pages When two pages display the same page number the page w...

Page 10: ...hat requires extensive revision revision bars will appear the full length of text New art added to an existing section will be identified by a single pointing hand indicator adjacent to the figure tit...

Page 11: ...3 Apr 30 01 1 4 Apr 30 01 1 5 Apr 30 01 1 6 Apr 30 01 1 7 Apr 30 01 1 8 Apr 30 01 1 9 Apr 30 01 1 10 Apr 30 01 1 11 Apr 30 01 1 12 Apr 30 01 1 13 Apr 30 01 1 14 Apr 30 01 1 15 Apr 30 01 Revision Leve...

Page 12: ...01 5 4 Apr 30 01 5 5 Apr 30 01 5 6 Apr 30 01 5 7 Apr 30 01 5 8 Apr 30 01 5 9 Apr 30 01 5 10 Apr 30 01 5 11 Apr 30 01 5 12 Apr 30 01 PAGE DATE 3 7 Feb 23 01 3 8 Feb 23 01 3 9 Feb 23 01 3 10 Feb 23 01...

Page 13: ...Apr 30 01 7 21 Apr 30 01 7 22 Apr 30 01 7 23 Apr 30 01 7 24 Apr 30 01 7 25 Apr 30 01 7 26 Apr 30 01 7 27 Apr 30 01 7 28 Apr 30 01 PAGE DATE 5 13 Apr 30 01 5 14 Apr 30 01 5 15 Apr 30 01 5 16 Apr 30 01...

Page 14: ...8 19 Apr 30 01 8 20 Apr 30 01 8 21 Apr 30 01 8 22 Apr 30 01 8 23 Apr 30 01 8 24 Apr 30 01 9 1 Apr 30 01 9 2 Blank Apr 30 01 PAGE DATE 7 29 Apr 30 01 7 30 Apr 30 01 7 31 Apr 30 01 7 32 Apr 30 01 7 33...

Page 15: ...OF CONTENTS SECTION GENERAL 1 LIMITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 4 PERFORMANCE 5 WEIGHT BALANCE EQUIPMENT LIST 6 AIRPLANE SYSTEMS DESCRIPTION 7 HANDLING SERVICE MAINTENANCE 8 SUPPL...

Page 16: ......

Page 17: ...ensions 1 7 Specific Loadings 1 7 Symbols Abbreviations and Terminology 1 8 General Airspeed Terminology And Symbols 1 8 Meteorological Terminology 1 9 Engine Power Terminology 1 9 Airplane Performanc...

Page 18: ...SECTION 1 CESSNA GENERAL MODEL 182T Figure 1 1 Three View Normal Ground Attitude Sheet 1 of 2 79 MAX 36 0 11 8 9 0 1 2 Apr 30 01...

Page 19: ...OTE 1 WING SPAN SHOWN WITH STANDARD STROBE LIGHTS INSTALLED NOTE 2 WHEEL BASE LENGTH IS 66 1 2 NOTE 3 PROPELLER GROUND CLEARANCE IS 10 7 8 NOTE 4 WING AREA IS 174 SQUARE FEET NOTE 5 MINIMUM TURNING RA...

Page 20: ...VE DATA ENGINE Number of Engines 1 Engine Manufacturer Textron Lycoming Engine Model Number IO 540 AB1A5 Engine Type Normally aspirated direct drive air cooled horizontally opposed fuel injected six c...

Page 21: ...ve concentrations shall not exceed 1 for isopropyl alcohol or 0 10 to 0 15 for DiEGME Refer to Section 8 for additional information Fuel Capacity Total Capacity 92 0 U S gallons Total Usable 87 0 U S...

Page 22: ...22851 or SAE J1899 Aviation Grade Ashless Dispersant Oil Oil conforming to Textron Lycoming Service Instruction No 1014 and all revisions and supplements thereto must be used after first 50 hours or o...

Page 23: ...d weight capacity for baggage in areas A B and C is 200 pounds The maximum allowable weight capacity for baggage in areas B and C is 80 pounds STANDARD AIRPLANE WEIGHTS Standard Empty Weight 1918 lbs...

Page 24: ...and temperature VA Maneuvering Speed is the maximum speed at which full or abrupt control movements may be used VFE Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a p...

Page 25: ...5 C at sea level Temperature pressure altitude and decreases by 2 C for each 1000 feet of altitude Pressure Pressure Altitude is the altitude read from an Altitude altimeter when the altimeter s barom...

Page 26: ...l Usable Fuel is the fuel available for flight planning Unusable Unusable Fuel is the quantity of fuel that can not be Fuel safely used in flight GPH Gallons Per Hour is the amount of fuel consumed pe...

Page 27: ...pended Its distance C G from the reference datum is found by dividing the total moment by the total weight of the airplane C G Center of Gravity Arm is the arm obtained by Arm adding the airplane s in...

Page 28: ...ff Weight is the maximum weight Takeoff approved for the start of the takeoff roll Weight Maximum Maximum Landing Weight is the maximum weight Landing approved for the landing touchdown Weight Tare Ta...

Page 29: ...ert U S measurement supplied with the Pilot s Operating Handbook into metric and imperial measurements The standard followed for measurement units shown is the National Institute of Standards Technolo...

Page 30: ...6 100 220 46 222 67 224 87 227 08 229 28 231 49 233 69 235 90 238 10 240 30 POUNDS INTO KILOGRAMS LIVRES EN KILOGRAMMES lb 0 1 2 3 4 5 6 7 8 9 kg kg kg kg kg kg kg kg kg kg 0 0 454 0 907 1 361 1 814 2...

Page 31: ...CESSNA SECTION 1 MODEL 182T GENERAL Figure 1 2 Weight Conversions Sheet 2 of 2 0585T1027 Kilograms 2 205 Pounds Pounds 454 Kilograms Units 10 100 etc Apr 30 01 1 15...

Page 32: ...8 56 301 84 305 12 308 40 311 68 314 96 318 24 321 52 324 80 100 328 08 331 36 334 64 337 93 341 21 344 49 347 77 351 05 354 33 357 61 FEET INTO METERS PIEDS EN METRES ft 0 1 2 3 4 5 6 7 8 9 m m m m m...

Page 33: ...CESSNA SECTION 1 MODEL 182T GENERAL Meters 3 281 Feet Feet 305 Meters Units 10 100 etc Figure 1 3 Length Conversions Sheet 2 of 2 Apr 30 01 1 17...

Page 34: ...100 39 370 39 764 40 157 40 551 40 945 41 339 41 732 42 126 42 520 42 913 INCHES INTO CENTIMETERS POUCES EN CENTIMETRES in 0 1 2 3 4 5 6 7 8 9 cm cm cm cm cm cm cm cm cm cm 0 2 54 5 08 7 62 10 16 12 7...

Page 35: ...CESSNA SECTION 1 MODEL 182T GENERAL Figure 1 4 Length Conversions Sheet 2 of 2 0585T1028 Centimeters 394 Inches Inches 2 54 Centimeters Units 10 100 etc Apr 30 01 1 19...

Page 36: ...stance Conversions 0585T1029 Statute Miles 1 609 Kilometers Kilometers 622 Statute Miles Statute Miles 869 Nautical Miles Nautical Miles 1 15 Statute Miles Nautical Miles 1 852 Kilometers Kilometers 5...

Page 37: ...21 338 21 558 21 778 100 21 998 22 218 22 438 22 658 22 878 23 098 23 318 23 537 23 757 23 977 IMPERIAL GALLONS INTO LITERS GALLONS IMPERIAL EN LITRES IG 0 1 2 3 4 5 6 7 8 9 Lt Lt Lt Lt Lt Lt Lt Lt L...

Page 38: ...SECTION 1 CESSNA GENERAL MODEL 182T Figure 1 6 Volume Conversions Sheet 2 of 3 0585T1032 Units 10 100 etc 1 22 Apr 30 01...

Page 39: ...CESSNA SECTION 1 MODEL 182T GENERAL Figure 1 6 Volume Conversions Sheet 3 of 3 0585T1033 Units 10 100 etc Apr 30 01 1 23...

Page 40: ...SECTION 1 CESSNA GENERAL MODEL 182T Figure 1 7 Temperature Conversions 0585T1034 1 24 Apr 30 01...

Page 41: ...SECTION 1 MODEL 182T GENERAL Figure 1 8 Volume to Weight Conversion 0585T1030 AVGAS Specific Gravity 72 Liters X 72 Kilograms Kilograms X 1 389 Liters Liters X 1 58 Pounds Pounds X 633 Liters Apr 30 0...

Page 42: ...SECTION 1 CESSNA GENERAL MODEL 182T Figure 1 9 Quick Conversions 0585T1031 1 26 Apr 30 01...

Page 43: ...ions 2 4 Airspeed Indicator Markings 2 5 Powerplant Limitations 2 5 Powerplant Instrument Markings 2 6 Weight Limits 2 7 Center Of Gravity Limits 2 7 Maneuver Limits 2 8 Flight Load Factor Limits 2 8...

Page 44: ......

Page 45: ...Section 9 of this Handbook for amended operating limitations operating procedures performance data and other necessary information for airplanes equipped with specific options NOTE The airspeeds liste...

Page 46: ...NO Maximum Structural Cruising Speed 136 140 Do not exceed this speed except in smooth air and then only with caution VA Maneuvering Speed 3100 Pounds 2600 Pounds 2100 Pounds 108 100 91 110 101 91 Do...

Page 47: ...perature 500 F 260 C Maximum Oil Temperature 245 F 118 C Oil Pressure Minimum 20 PSI Maximum 115 PSI Fuel Grade See Fuel Limitations MARKING KIAS VALUE OR RANGE SIGNIFICANCE White Arc 41 100 Full Flap...

Page 48: ...Model Number B3D36C431 80VSA 1 Propeller Diameter 79 inches Propeller Blade Angle at 30 Inch Station Low 14 9 High 31 7 POWERPLANT INSTRUMENT MARKINGS Powerplant instrument markings and their color c...

Page 49: ...NOTE The maximum allowable combined weight capacity for baggage in areas A B and C is 200 pounds The maximum combined allowable weight capacity for baggage in areas B and C is 80 pounds CENTER OF GRAV...

Page 50: ...1 52g Flaps Down 2 0g The design load factors are 150 of the above and in all cases the structure meets or exceeds design loads KINDS OF OPERATION LIMITS The airplane as delivered is equipped for day...

Page 51: ...ground attitude definition Takeoff and land with the fuel selector valve handle in the BOTH position Operation on either LEFT or RIGHT tank limited to level flight only With 1 4 tank or less prolonged...

Page 52: ...be complied with when operating this airplane in the Normal Category Other operating limitations which must be complied with when operating this airplane in this category are contained in the Pilot s...

Page 53: ...M OF FILLER INDICATOR TAB 5 On flap control indicator 0 to 10 140 KIAS Partial flap range with blue color code also mechanical detent at 10 10 to 20 120 KIAS Light blue color code also mechanical dete...

Page 54: ...AGGAGE DOOR LATCH MAXIMUM 200 POUNDS COMBINED FOR ADDITIONAL LOADING INSTRUCTIONS SEE WEIGHT AND BALANCE DATA 7 A calibration card must be provided to indicate the accuracy of the magnetic compass in...

Page 55: ...WILL DAMAGE ELECTRICAL COMPONENTS 12 On the Upper Right Side of the Aft Cabin Partition EMERGENCY LOCATOR TRANSMITTER INSTALLED AFT OF THIS PARTITION MUST BE SERVICED IN ACCORDANCE WITH FAR PART 91 2...

Page 56: ......

Page 57: ...re Immediately After Takeoff 3 4 Engine Failure During Flight Restart Procedures 3 4 Forced Landings 3 5 Emergency Landing Without Engine Power 3 5 Precautionary Landing With Engine Power 3 6 Ditching...

Page 58: ...tor Control 3 16 Fires 3 17 Emergency Operation In Clouds Total Vacuum System Failure 3 17 Executing A 180 Turn In Clouds 3 17 Emergency Descent Through Clouds 3 18 Recovery From Spiral Dive In The Cl...

Page 59: ...good judgment when unexpected weather is encountered However should an emergency arise the basic guidelines described in this section should be considered and applied as necessary to correct the prob...

Page 60: ...T 4 Mixture IDLE CUT OFF 5 Ignition Switch OFF 6 Master Switch OFF ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF 1 Airspeed 75 KIAS flaps UP 70 KIAS flaps DOWN 2 Mixture IDLE CUT OFF 3 Fuel Selector Valve...

Page 61: ...tch OFF NOTE If the fuel flow indication immediately drops to zero signifying an engine driven fuel pump failure return the auxiliary fuel pump switch to ON FORCED LANDINGS EMERGENCY LANDING WITHOUT E...

Page 62: ...11 Touchdown SLIGHTLY TAIL LOW 12 Mixture IDLE CUT OFF 13 Ignition Switch OFF 14 Brakes APPLY HEAVILY DITCHING 1 Radio TRANSMIT MAYDAY on 121 5 MHz giving location and intentions and SQUAWK 7700 if i...

Page 63: ...ine If engine starts 2 Power 1700 RPM for a few minutes 3 Engine SHUTDOWN and inspect for damage If engine fails to start 4 Throttle FULL OPEN 5 Mixture IDLE CUT OFF 6 Cranking CONTINUE 7 Fuel Selecto...

Page 64: ...er Switch OFF 2 Vents Cabin Air Heat CLOSED 3 Fire Extinguisher ACTIVATE if available 4 Avionics Master Switch OFF 5 All Other Switches except ignition switch OFF AFTER DISCHARGING FIRE EXTINGUISHER A...

Page 65: ...TILATE THE CABIN 4 Vents Cabin Air Heat Open when it is ascertained that fire is completely extinguished 5 Land the airplane as soon as possible to inspect for damage WING FIRE 1 Landing Taxi Light Sw...

Page 66: ...required for any change in power settings 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 1 4 inch...

Page 67: ...tion 5 LANDING WITH A FLAT MAIN TIRE 1 Approach NORMAL 2 Wing Flaps FULL DOWN 3 Touchdown GOOD MAIN TIRE FIRST hold airplane off flat tire as long as possible with aileron control 4 Directional Contro...

Page 68: ...ES DURING FLIGHT Ammeter Indicates Discharge NOTE Illumination of VOLTS on the annunciator panel may occur during low RPM conditions with an electrical load on the system such as during a low RPM taxi...

Page 69: ...Nonessential Radio and Electrical Equipment OFF 9 Flight TERMINATE as soon as practical VACUUM SYSTEM FAILURE Left Vacuum Annunciator L VAC or Right Vacuum Annunciator VAC R Illuminates IF VACUUM IS N...

Page 70: ...owledge of procedures fresh ENGINE FAILURE If an engine failure occurs during the takeoff roll the most important thing to do is stop the airplane on the remaining runway Those extra items on the chec...

Page 71: ...peed as shown in Figure 3 1 should be established as quickly as possible While gliding toward a suitable landing area an effort should be made to identify the cause of the failure If time permits an e...

Page 72: ...entions and squawk 7700 Avoid a landing flare because of difficulty in judging height over a water surface The checklist assumes the availability of power to make a precautionary water landing If powe...

Page 73: ...UDS Total Vacuum System Failure If both the vacuum pumps fail in flight the directional indicator and attitude indicator will be disabled and the pilot will have to rely on the turn coordinator if he...

Page 74: ...esterly heading to minimize compass card swings due to changing bank angles In addition keep hands off the control wheel and steer a straight course with rudder control by monitoring the turn coordina...

Page 75: ...ruising flight INADVERTENT FLIGHT INTO ICING CONDITIONS Flight into icing conditions is prohibited and extremely dangerous An inadvertent encounter with these conditions can best be handled using the...

Page 76: ...the direction of rotation the symbolic airplane in the turn coordinator may be referred to for this information ROUGH ENGINE OPERATION OR LOSS OF POWER SPARK PLUG FOULING A slight engine roughness in...

Page 77: ...taining adequate fuel In the event of an engine driven fuel pump failure immediately turn the auxiliary fuel pump switch ON to restore the engine power In this event the flight should be terminated wh...

Page 78: ...RATE OF CHARGE After engine starting and heavy electrical usage at low engine speeds such as extended taxiing the battery condition will be low enough to accept above normal charging during the initi...

Page 79: ...resume and the low voltage annunciator VOLTS will go off The avionics master switch may then be turned back on If the annunciator illuminates again a malfunction is confirmed In this event the flight...

Page 80: ......

Page 81: ...in 4 7 Empennage 4 8 Right Wing Trailing Edge 4 8 Right Wing 4 8 Nose 4 9 Left Wing 4 10 Left Wing Leading Edge 4 11 Left Wing Trailing Edge 4 11 Before Starting Engine 4 11 Starting Engine With Batte...

Page 82: ...RMAL PROCEDURES Preflight Inspection 4 18 Starting Engine 4 19 Starting General 4 19 Taxiing 4 20 Before Takeoff 4 22 Warm Up 4 22 Magneto Check 4 22 Alternator Check 4 22 Elevator Trim 4 23 Landing L...

Page 83: ...ontinued Page Landing 4 29 Normal Landing 4 29 Short Field Landing 4 29 Crosswind Landing 4 30 Balked Landing 4 30 Cold Weather Operation 4 30 Starting 4 31 Winterization Kit 4 32 Hot Weather Operatio...

Page 84: ......

Page 85: ...70 80 KIAS Short Field Takeoff Flaps 20 Speed at 50 Feet 60 KIAS Enroute Climb Flaps Up Normal Sea Level 85 95 KIAS Best Rate of Climb Sea Level 82 KIAS Best Rate of Climb 10 000 Feet 77 KIAS Best Ang...

Page 86: ...Use of the refueling steps and assist handles will simplify access to the upper wing surfaces for visual checks and refueling operations In cold weather remove even small accumulations of frost ice or...

Page 87: ...IF THE IGNITION SWITCH WERE ON DO NOT STAND NOR ALLOW ANYONE ELSE TO STAND WITHIN THE ARC OF THE PROPELLER SINCE A LOOSE OR BROKEN WIRE OR A COMPONENT MALFUNCTION COULD CAUSE THE PROPELLER TO ROTATE...

Page 88: ...arning horn with the Master Switch on will confirm system operation 20 Pitot Heat OFF 21 Master Switch OFF 22 Trim Controls Neutral 23 Baggage Door CHECK lock with key 2 EMPENNAGE 1 Rudder Gust Lock i...

Page 89: ...ND SYSTEM PURGED BY QUALIFIED MAINTENANCE PERSONNEL ALL EVIDENCE OF CONTAMINATION MUST BE REMOVED BEFORE FURTHER FLIGHT 5 Fuel Quantity CHECK VISUALLY for desired level 6 Fuel Filler Cap SECURE and VE...

Page 90: ...blockage 6 LEFT WING 1 Fuel Quantity CHECK VISUALLY for desired level 2 Fuel Filler Cap SECURE and VENT UNOBSTRUCTED 3 Fuel Tank Sump Quick Drain Valves DRAIN at least a cupful of fuel using sampler c...

Page 91: ...f movement and security 2 Flap CHECK for security and condition BEFORE STARTING ENGINE 1 Preflight Inspection COMPLETE 2 Passenger Briefing COMPLETE 3 Seats Seat Belts Shoulder Harnesses ADJUST and LO...

Page 92: ...6 7 and 8 above 9 Ignition Switch START release when engine starts 10 Mixture ADVANCE smoothly to RICH when engine fires NOTE If engine floods place mixture in idle cut off open throttle 1 2 to full a...

Page 93: ...en engine fires advance mixture to full rich and retard throttle promptly 12 Oil Pressure CHECK 13 External Power DISCONNECT from airplane receptacle Secure external power door 14 Ammeter CHECK See ch...

Page 94: ...DESIRED 17 Radios and Avionics SET 18 NAV GPS Switch if installed SET 19 Autopilot if installed OFF 20 Wing Flaps SET for takeoff 0 TO 20 21 Cowl Flap OPEN 22 Brakes RELEASE TAKEOFF NORMAL TAKEOFF 1 W...

Page 95: ...ORMANCE CLIMB 1 Airspeed 82 KIAS at sea level to 77 KIAS at 10 000 feet 2 Power FULL THROTTLE and 2400 RPM 3 Mixture LEAN in accordance with Maximum Power Fuel Flow placard value 4 Cowl Flaps OPEN 5 F...

Page 96: ...S 3 Airspeed 60 70 KIAS flaps FULL 4 Power REDUCE to idle as obstacle is cleared 5 Trim ADJUST 6 Touchdown MAIN WHEELS FIRST 7 Landing Roll LOWER NOSE WHEEL GENTLY 8 Braking MINIMUM REQUIRED SHORT FIE...

Page 97: ...SECURING AIRPLANE 1 Parking Brake SET 2 Throttle IDLE 3 Electrical Equipment Avionics Master Switch Autopilot if installed OFF 4 Mixture IDLE CUT OFF pulled full out 5 Ignition Switch OFF 6 Master Swi...

Page 98: ...ision lights damage to nose wheel as a result of exceeding tow limits and avionics antennas Outside storage for long periods may result in dust and dirt accumulation on the induction air filter obstru...

Page 99: ...be inspected for obstructions ice or water especially after exposure to cold wet weather STARTING ENGINE STARTING GENERAL In cooler weather the engine compartment temperature drops off rapidly follow...

Page 100: ...y cold weather stop the engine and investigate Lack of oil pressure can cause serious engine damage NOTE Additional details concerning cold weather starting and operation may be found under COLD WEATH...

Page 101: ...ON LH WING AND DOWN ELEVATOR USE DOWN AILERON ON RH WING AND DOWN ELEVATOR USE UP AILERON ON LH WING AND NEUTRAL ELEVATOR NOTE Strong quartering tail winds require caution Avoid sudden bursts of the t...

Page 102: ...on either magneto or show greater than 50 RPM differential between magnetos If there is a doubt concerning operation of the ignition system RPM checks at higher engine speeds will usually confirm whet...

Page 103: ...for discontinuing the takeoff If this occurs you are justified in making a thorough full throttle static runup before another takeoff is attempted The engine should run smoothly and turn approximately...

Page 104: ...e performed with the minimum flap setting necessary for the field length to minimize the drift angle immediately after takeoff With the ailerons partially deflected into the wind the airplane is accel...

Page 105: ...practicable until a total of 50 hours has accumulated or oil consumption has stabilized Operation at this higher power will ensure proper seating of the rings and is applicable to new engines and eng...

Page 106: ...follows 1 Lean the mixture slowly until the EGT peaks and begins to drop 2 Enrichen as needed to ensure operation at peak 3 If engine operation is rough at peak EGT further enrichen for smooth operat...

Page 107: ...T setting FUEL SAVINGS PROCEDURES FOR NORMAL OPERATIONS For best fuel economy during normal operations the following procedures are recommended 1 After engine start and for all ground operations set t...

Page 108: ...ggravated by the fact that the engine fuel flows are lower at idle and taxi engine speeds When vapor occurs as evidenced by idle engine speed and fuel flow fluctuations the following procedures are re...

Page 109: ...ed for braking in the landing roll The nose wheel is lowered to the runway gently after the speed has diminished to avoid unnecessary nose gear loads This procedure is especially important in rough or...

Page 110: ...cleared and a safe altitude and airspeed are obtained the wing flaps should be retracted COLD WEATHER OPERATION Special consideration should be given to the operation of the airplane fuel system durin...

Page 111: ...nserving battery energy When air temperatures are below 20 F 6 C the use of an external preheater and an external power source are recommended whenever possible to obtain positive starting and to redu...

Page 112: ...M If the engine accelerates smoothly and the oil pressure re mains normal and steady the airplane is ready for takeoff WINTERIZATION KIT A winterization kit is provided and may be utilized when cold w...

Page 113: ...n though flight at a lower level may be consistent with the provisions of government regulations 2 During departure from or approach to an airport climb after takeoff and descent for landing should be...

Page 114: ......

Page 115: ...10 Figure 5 2 Altimeter Correction 5 11 Figure 5 3 Temperature Conversion Chart 5 12 Figure 5 4 Stall Speeds 5 13 Figure 5 5 Crosswind Components 5 14 Figure 5 6 Short Field Takeoff Distance 3100 Lbs...

Page 116: ......

Page 117: ...bulence may account for variations of 10 or more in range and endurance Therefore it is important to utilize all available information to estimate the fuel required for the particular flight and to fl...

Page 118: ...nd temperature For example in this particular sample problem the takeoff distance information presented for a weight of 3100 pounds pressure altitude of 2000 feet and a temperature of 30 C should be u...

Page 119: ...racteristics presented in Figure 5 9 the range profile chart presented in Figure 5 10 and the endurance profile chart presented in Figure 5 11 The relationship between power and range is illustrated b...

Page 120: ...e may be made as noted on the climb chart The approximate effect of a non standard temperature is to increase the time fuel and distance by 10 for each 10 C above standard temperature due to the lower...

Page 121: ...se is 3 6 hours X 10 7 gallons hour 38 5 Gallons A 45 minute reserve requires 45 60 X 10 7 gallons hour 8 0 Gallons The total estimated fuel required is as follows Engine start taxi and takeoff 1 7 Cl...

Page 122: ...round roll 540 Feet Total distance to clear a 50 foot obstacle 1280 Feet A correction for the effect of wind may be made based on Note 2 of the landing chart using the same procedure as outlined for t...

Page 123: ...maximum power descent Figure 5 1 Airspeed Calibration Sheet 1 of 2 FLAPS UP KIAS 55 60 70 80 90 100 110 120 130 140 150 160 KCAS 61 65 73 82 90 99 108 117 126 136 146 156 FLAPS 20 KIAS 40 50 60 70 80...

Page 124: ...ION Power required for level flight or maximum power descent Figure 5 1 Airspeed Calibration Sheet 2 of 2 FLAPS UP KIAS 55 60 70 80 90 100 110 120 130 140 150 160 ALT KIAS 53 58 70 81 91 101 111 121 1...

Page 125: ...are less than 50 feet Figure 5 2 Altimeter Correction CONDITION FLAPS UP CORRECTION TO BE ADDED FEET KIAS alternate static source ON 60 80 100 120 140 160 S L 30 10 20 30 50 50 2000 ft 30 10 20 30 50...

Page 126: ...SECTION 5 CESSNA PERFORMANCE MODEL 182T Figure 5 3 Temperature Conversion Chart TEMPERATURECONVERSIONCHART 5 12 Apr 30 01...

Page 127: ...much as 250 feet 2 KIAS values are approximate Figure 5 4 Stall Speeds FLAP SETTING ANGLE OF BANK 0 KIAS KCAS 30 KIAS KCAS 45 KIAS KCAS 60 KIAS KCAS UP 20 FULL 50 43 40 54 50 49 54 46 43 58 54 53 59 5...

Page 128: ...SECTION 5 CESSNA PERFORMANCE MODEL 182T Figure 5 5 Crosswind Components NOTE Maximum demonstrated crosswind velocity is 15 knots not a limitation 5 14 Apr 30 01...

Page 129: ...se distances by 15 of the ground roll figure Figure 5 6 Short Field Takeoff Distance Sheet 1 of 3 Press Alt In Feet 0 C Grnd Roll Ft Total Ft To Clear 50 Ft Obst 10 C Grnd Roll Ft Total Ft To Clear 50...

Page 130: ...tances by 15 of the ground roll figure Figure 5 6 Short Field Takeoff Distance Sheet 2 of 3 Press Alt In Feet 0 C Grnd Roll Ft Total Ft To Clear 50 Ft Obst 10 C Grnd Roll Ft Total Ft To Clear 50 Ft Ob...

Page 131: ...ay increase distances by 15 of the ground roll figure Figure 5 6 Short Field Takeoff Distance Sheet 3 of 3 Press Alt In Feet 0 C Grnd Roll Ft Total Ft To Clear 50 Ft Obst 10 C Grnd Roll Ft Total Ft To...

Page 132: ...Fuel Flow placard Cowl Flaps Open Figure 5 7 Maximum Rate of Climb PRESS ALT FT CLIMB SPEED KIAS RATE OF CLIMB FPM 20 C 0 C 20 C 40 C S L 80 1055 980 905 835 2000 79 945 875 805 735 4000 78 840 770 7...

Page 133: ...value for smooth engine operation and increased power 3 Increase time fuel and distance by 10 for each 10 C above standard temperature 4 Distances shown are based on zero wind Figure 5 8 Time Fuel an...

Page 134: ...leaned to Maximum Power Fuel Flow placard value for smooth engine operation and increased power 3 Increase time fuel and distance by 10 for each 10 C above standard temperature 4 Distances shown are...

Page 135: ...3 2 74 135 12 8 23 74 129 12 8 71 130 12 4 69 131 12 1 22 69 126 12 1 67 127 11 7 65 127 11 4 21 65 122 11 4 62 122 11 1 60 123 10 8 20 60 118 10 7 58 118 10 4 56 118 10 2 2300 27 84 141 14 5 26 82 13...

Page 136: ...EMP 35 C BHP KTAS GPH 2100 27 82 133 14 2 79 135 13 7 76 136 13 2 26 78 131 13 4 75 133 13 0 73 134 12 6 25 74 129 12 8 71 130 12 4 69 130 12 0 24 70 126 12 1 67 127 11 8 65 127 11 4 23 66 123 11 5 63...

Page 137: ...136 14 1 79 138 13 6 76 139 13 2 23 77 133 13 3 74 134 12 8 71 135 12 4 22 72 130 12 5 69 131 12 1 67 131 11 7 21 67 126 11 8 65 126 11 4 63 127 11 1 20 62 122 11 0 60 122 10 7 58 122 10 5 2300 26 82...

Page 138: ...1 C BHP KTAS GPH 20 C ABOVE STANDARD TEMP 31 C BHP KTAS GPH 2100 26 80 135 13 9 77 137 13 4 75 138 12 9 25 76 133 13 1 73 134 12 7 71 134 12 3 24 72 130 12 5 69 131 12 1 67 131 11 7 23 68 127 11 8 65...

Page 139: ...5 83 146 14 4 24 84 140 14 6 81 142 14 0 78 143 13 6 23 79 138 13 7 76 139 13 2 74 139 12 8 22 74 134 12 9 72 135 12 5 69 135 12 1 21 70 130 12 1 67 131 11 7 65 131 11 4 20 65 126 11 4 62 126 11 1 60...

Page 140: ...3 C BHP KTAS GPH STANDARD TEMPERATURE 7 C BHP KTAS GPH 20 C ABOVE STANDARD TEMP 27 C BHP KTAS GPH 2100 25 78 137 13 5 75 138 13 0 73 138 12 6 24 74 134 12 8 71 135 12 4 69 135 12 0 23 70 131 12 2 67 1...

Page 141: ...19 62 126 11 0 60 126 10 7 58 125 10 4 2300 23 79 140 13 6 76 141 13 1 73 141 12 7 22 74 136 12 8 71 137 12 4 69 137 12 0 21 69 132 12 1 67 133 11 7 64 133 11 4 20 65 128 11 4 62 128 11 0 60 128 10 7...

Page 142: ...20 69 134 12 1 67 135 11 7 65 135 11 4 19 64 130 11 4 62 130 11 0 60 130 10 7 18 59 125 10 6 57 124 10 3 55 124 10 1 2300 21 72 136 12 5 69 137 12 0 67 137 11 7 20 67 132 11 7 64 132 11 3 62 132 11 0...

Page 143: ...C BHP KTAS GPH 2400 20 72 139 12 5 69 139 12 1 67 139 11 7 19 67 134 11 7 64 134 11 3 62 134 11 0 18 62 129 11 0 59 129 10 6 57 128 10 3 2300 21 74 141 12 8 71 141 12 4 69 142 12 0 20 69 136 12 1 66...

Page 144: ...29 C BHP KTAS GPH STANDARD TEMPERATURE 9 C BHP KTAS GPH 20 C ABOVE STANDARD TEMP 11 C BHP KTAS GPH 2400 18 64 133 11 3 61 133 10 9 59 133 10 6 17 59 127 10 5 56 127 10 2 54 126 10 0 16 53 121 9 8 51 1...

Page 145: ...lation purposes only 2 For best economy operate at peak EGT Figure 5 9 Cruise Performance Sheet 11 of 11 RPM MP 20 C BELOW STANDARD TEMP 33 C BHP KTAS GPH STANDARD TEMPERATURE 13 C BHP KTAS GPH 20 C A...

Page 146: ...formance Climb with Placard Mixture Recommended Lean Mixture for Cruise Standard Temperature Zero Wind NOTE This chart allows for the fuel used for engine start taxi takeoff and climb cruise at the de...

Page 147: ...formance Climb with Placard Mixture Recommended Lean Mixture for Cruise Standard Temperature Zero Wind NOTE This chart allows for the fuel used for engine start taxi takeoff and climb cruise at the de...

Page 148: ...mance Climb with Placard Mixture Recommended Lean Mixture for Cruise Standard Temperature Zero Wind NOTE This chart allows for the fuel used for engine start taxi takeoff and climb cruise at the desig...

Page 149: ...mance Climb with Placard Mixture Recommended Lean Mixture for Cruise Standard Temperature Zero Wind NOTE This chart allows for the fuel used for engine start taxi takeoff and climb cruise at the desig...

Page 150: ...er distances Figure 5 12 Short Field Landing Distance Press Alt In Feet 0 C Grnd Roll Ft Total Ft To Clear 50 Ft Obst 10 C Grnd Roll Ft Total Ft To Clear 50 Ft Obst 20 C Grnd Roll Ft Total Ft To Clear...

Page 151: ...DEL 182T WEIGHT BALANCE EQUIPMENT LIST SECTION 6 WEIGHT BALANCE EQUIPMENT LIST TABLE OF CONTENTS Page Introduction 6 3 Airplane Weighing Procedures 6 3 Weight And Balance 6 5 Baggage Tie Down 6 7 Feb...

Page 152: ......

Page 153: ...IRPLANE IS LOADED PROPERLY OPERATION OUTSIDE OF PRESCRIBED WEIGHT AND BALANCE LIMITATIONS COULD RESULT IN AN ACCIDENT AND SERIOUS OR FATAL INJURY AIRPLANE WEIGHING PROCEDURES 1 Preparation a Inflate t...

Page 154: ...SECTION 6 CESSNA WEIGHT BALANCE EQUIPMENT LIST MODEL 182T Figure 6 1 Airplane Weighing Form Sheet 1 of 2 07851022 AIRPLANE WEIGHING FORM 6 4 Apr 30 01...

Page 155: ...and C G can be determined 6 Basic Empty Weight may be determined by completing Figure 6 1 WEIGHT AND BALANCE The following information will enable you to operate your Cessna within the prescribed wei...

Page 156: ...SECTION 6 CESSNA WEIGHT BALANCE EQUIPMENT LIST MODEL 182T Figure 6 2 Sample Weight and Balance Record 0585C1009 6 6 Feb 23 01...

Page 157: ...ndard equipment to secure baggage in the area aft of the rear seat baggage areas A B and C Eight eyebolts serve as attaching points for the net A placard on the baggage door defines the weight limitat...

Page 158: ...uare 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 airplane structure The maximum rated load weight capaci...

Page 159: ...ats positioned for average occupant Numbers in parentheses indicate forward and aft limits of occupant center of gravity range Arms measured to the center of the areas shown NOTES 1 The usable fuel C...

Page 160: ...ION 6 CESSNA WEIGHT BALANCE EQUIPMENT LIST MODEL 182T Figure 6 4 Internal Cabin Dimensions Sheet 1 of 2 07851019 CABIN HEIGHT MEASUREMENTS DOOR OPENING DIMENSIONS FIREWALL AFT BAGGAGE AREA 6 10 Feb 23...

Page 161: ...DEL 182T WEIGHT BALANCE EQUIPMENT LIST Figure 6 4 Internal Cabin Dimensions Sheet 2 of 2 07851020 CABIN WIDTH MEASUREMENTS INSTRUMENT PANEL REAR DOORPOST BULKHEAD TIE DOWN RINGS 10 CABIN STATIONS C G...

Page 162: ...2 to 109 120 Lbs Max 100 9 7 6 Baggage Area B Station 109 to 124 80 Lbs Max 23 2 7 7 Baggage Area C Station 124 to 134 80 Lbs Max 8 RAMP WEIGHT AND MOMENT 3110 135 3 9 Fuel allowance for engine start...

Page 163: ...Loading Problem Sheet 2 of 2 NOTE When several loading configurations are representative of your operations it may be useful to fill out one or more of the above columns so specific loadings are avail...

Page 164: ...ng Graph 0785C1008 NOTE Line representing adjustable seats shows pilot and front seat passenger center of gravity on adjustable seats positioned for an average occupant Refer to the Loading Arrangemen...

Page 165: ...CESSNA SECTION 6 MODEL 182T WEIGHT BALANCE EQUIPMENT LIST Figure 6 7 Center of Gravity Moment Envelope 0785C1009 Feb 23 01 6 15...

Page 166: ...SECTION 6 CESSNA WEIGHT BALANCE EQUIPMENT LIST MODEL 182T Figure 6 8 Center of Gravity Limits 0785C1010 6 16 Feb 23 01...

Page 167: ...pment for FAA certification S standard equipment items O optional equipment items replacing required or standard items A optional equipment items which are in addition to required or standard items In...

Page 168: ...8 KS 271C ROLL SERVO INSTALLATION 3940432 1 3 6 54 2 CABLE ASSY ROLL SERVO 3924137 2 0 7 66 0 CABLE ASSY KC 140 AUTOPILOT 3924132 1 4 7 85 1 KMC 100 CONFIGURATION MODULE 071 00073 5000 0 1 12 0 23 COM...

Page 169: ...ER VINYL COVER 0719031 1 34 3 41 5 25 03 S SEAT FRONT PASSENGER ADJUSTABLE CLOTH VINYL COVER 0719012 2 33 8 41 5 25 04 O SEAT FRONT PASSENGER ADJUSTABLE LEATHER VINYL COVER 0719031 2 34 3 41 5 25 05 S...

Page 170: ...TENSIONS REMOVABLE SET OF 2 STOWED INSTALLED ARM SHOWN 0501082 1 2 9 8 0 28 FUEL 28 01 R FUEL QUANTITY INDICATORS LEFT RIGHT S3317 3 0 7 16 0 28 02 R AUXILIARY FUEL PUMP A8160 D 1 9 12 0 31 INDICATING...

Page 171: ...37 01 S 0706009 1 7 8 11 0 DIRECTIONAL GYRO INDICATOR S3330 2 2 8 15 2 ATTITUDE GYRO INDICATOR S3326 1 2 1 14 0 HOSE AND MISC HARDWARE 0706009 2 2 9 4 5 34 08 S TURN COORDINATOR INDICATOR S3291 1 1 2...

Page 172: ...LTER INSTALLATION 1201075 2 0 3 12 5 VACUUM RELIEF VALVE 2H3 48 0 5 2 1 MANIFOLD 1H5 25 0 5 3 0 VACUUM GAUGE AMMETER S3280 1 0 6 15 6 53 FUSELAGE 53 01 S REFUELING STEPS AND HANDLE INSTL 0701127 1 1 7...

Page 173: ...AVIONICS PACKAGE OPTIONS 98 01 S STANDARD AVIONICS PACKAGE 3900029 1 46 8 81 6 22 01 S KAP 140 DUAL AXIS AUTOPILOT 20 0 106 7 23 02 S KX 155A NAV COM WITH GLIDE SLOPE 10 4 83 4 23 04 S KMA 28 AUDIO IN...

Page 174: ...ANGE OVER STANDARD 3900031 1 38 6 59 5 34 13 A STORMSCOPE INSTALLATION 5 5 119 5 34 14 A HSI INSTALLATION 3900008 1 13 6 98 5 CIRCUIT BRKR PNL EXCHNG CHNG OVER NAV 1 0 4 16 5 MD41 233 EXCHANGE FOR MD4...

Page 175: ...12 Center Pedestal Layout 7 12 Ground Control 7 12 Wing Flap System 7 13 Landing Gear System 7 14 Baggage Compartment 7 14 Seats 7 14 Integrated Seat Belt Shoulder Harness 7 15 Entrance Doors And Cabi...

Page 176: ...32 Fuel Drain Valves 7 32 Brake System 7 32 Electrical System 7 33 Annunciator Panel 7 33 Master Switch 7 36 Avionics Master Switch 7 37 Ammeter 7 38 Low Voltage Annunciation 7 38 Circuit Breakers And...

Page 177: ...7 Low Vacuum Annunciation 7 47 Clock O A T Indicator 7 49 Stall Warning System 7 49 Standard Avionics 7 50 Avionics Support Equipment 7 50 Avionics Cooling Fan 7 50 Microphone And Headset Installation...

Page 178: ......

Page 179: ...l fuel tanks are constructed of a front and rear spar with formed sheet metal ribs doublers and stringers The entire structure is covered with aluminum skin The front spars are equipped with wing to f...

Page 180: ...rudder brake pedals for the rudder The elevator control system is equipped with downsprings which provide improved stability in flight TRIM SYSTEMS A manually operated rudder and elevator trim is prov...

Page 181: ...SNA SECTION 7 MODEL 182T AIRPLANE SYSTEMS DESCRIPTION Figure 7 1 Flight Control and Trim Systems Sheet 1 of 2 07851017 07851023 AILERON CONTROL SYSTEM RUDDER AND RUDDER TRIM CONTROL SYSTEMS Apr 30 01...

Page 182: ...SECTION 7 CESSNA AIRPLANE SYSTEMS DESCRIPTION MODEL 182T Figure 7 1 Flight Control and Trim Systems Sheet 2 of 2 07851018 07851024 ELEVATOR CONTROL SYSTEM ELEVATOR TRIM CONTROL SYSTEM 7 8 Apr 30 01...

Page 183: ...ch contains a left right fuel quantity indicator an oil temperature oil pressure indicator a vacuum gauge ammeter an EGT CHT indicator a digital clock OAT indicator and manifold pressure gauge fuel fl...

Page 184: ...SCRIPTION MODEL 182T Figure 7 2 Instrument Panel Sheet 1 of 2 0585C1015 25 26 17 16 19 18 24 31 13 32 43 37 40 28 27 14 15 12 11 10 9 8 6 5 4 3 2 1 52 33 35 7 49 50 48 51 47 42 45 46 30 29 38 36 21 39...

Page 185: ...Speed Indicator 37 Throttle Control 12 Altimeter 38 Rudder Trim 13 Annunciator Panel 39 Cowl Flap Control Lever 14 Course Deviation and Glide Slope Indicators 40 12 Volt Power Port 15 GPS Annunciator...

Page 186: ...ch is connected to the nose gear and to the rudder bars will turn the nose wheel through an arc of approximately 11 each side of center By applying either left or right brake the degree of turn may be...

Page 187: ...p or down in a slotted panel that provides mechanical stops at the 10 and 20 positions To change flap setting the flap lever is moved to the right to clear mechanical stops at the 10 and 20 positions...

Page 188: ...For baggage area and door dimensions refer to Section 6 SEATS The seating arrangement consists of two vertically adjusting crew seats for the pilot and front seat passenger and an infinitely adjustab...

Page 189: ...sitive restraint for the user In the front seats the inertia reels are located on the centerline of the upper cabin area In the rear seats the inertia reels are located outboard of each passenger in t...

Page 190: ...Shoulder Harnesses 0514T1004 LIFT TO RELEASE LATCH STANDARD INTEGRATED SEATBELT SHOULDER HARNESS WITH INTERTIA REEL PUSH BUTTON RELEASE BUCKLE NON ADJUSTABLE FORE AND AFT ADJUSTMENT LEVER SEAT BACK A...

Page 191: ...oors incorporate a recessed exterior door handle a conventional interior door handle a key operated door lock left door only a door stop mechanism and openable windows in both the left and right doors...

Page 192: ...the window outward and hold it there If required either window may be opened at any speed up to 175 KIAS The rear side windows and rear windows are of the fixed type and cannot be opened CONTROL LOCKS...

Page 193: ...full aft position A friction lock which is a round knurled knob is located at the base of the throttle and is operated by rotating the lock clockwise to increase friction or counterclockwise to decre...

Page 194: ...t of the engine case to the rear engine baffle At the baffle the oil pressure line is connected to a transducer This transducer produces an electrical signal which translates into a pressure reading a...

Page 195: ...does current flow This change in current flow registers on the indicator as a change in temperature Although the EGT gauge contains no red lines or operating range marks it is useful in establishing...

Page 196: ...cruise power settings NEW ENGINE BREAK IN AND OPERATION The engine run in was accomplished at the factory and is ready for the full range of use It is however suggested that cruising be accomplished a...

Page 197: ...and control panel The switch is labeled clockwise OFF R L BOTH and START The engine should be operated on both magnetos BOTH position except for magneto checks The R and L positions are for checking p...

Page 198: ...ol unit induction air is delivered to the cylinders through the intake manifold tubes and metered fuel is delivered to a fuel manifold flow divider The fuel manifold through spring tension on a diaphr...

Page 199: ...tting introduced into the governor with the propeller control establishes the propeller speed and thus the engine speed to be maintained The governor then controls flow of engine oil boosted to high p...

Page 200: ...s a flexible fuel hose assembly between the servo and the firewall Aluminum fuel lines return the fuel to the top portion of the selector valve and then to the aircraft integral tanks One drain is add...

Page 201: ...unit metered fuel goes to a fuel distribution valve flow divider located on top of the engine From the fuel distribution valve individual fuel lines are routed to air bleed type injector nozzles locat...

Page 202: ...SECTION 7 CESSNA AIRPLANE SYSTEMS DESCRIPTION MODEL 182T Figure 7 6 Fuel System Schematic 7 28 Apr 30 01...

Page 203: ...ge will read L LOW FUEL If the right tank transmitter has failed the message will read LOW FUEL R If both tanks transmitters have failed the message will read L LOW FUEL R Fuel flow is measured by use...

Page 204: ...r example if the fuel selector is positioned to use fuel from the left hand tank the fuel return system is returning fuel to the left hand tank only FUEL VENTING Fuel system venting is essential to sy...

Page 205: ...the heavy wing NOTE It is not practical to measure the time required to consume all of the fuel in one tank and after switching to the opposite tank expect an equal duration from the remaining fuel Th...

Page 206: ...y applying pressure to the top of either the left pilot s or right copilot s set of rudder pedals which are interconnected When the airplane is parked both main wheel brakes may be set by utilizing th...

Page 207: ...nics master switch are in the ON position PRIOR TO TURNING THE MASTER SWITCH ON OR OFF STARTING THE ENGINE OR APPLYING AN EXTERNAL POWER SOURCE THE AVIONICS MASTER SWITCH LABELED AVIONICS MASTER SHOUL...

Page 208: ...SECTION 7 CESSNA AIRPLANE SYSTEMS DESCRIPTION MODEL 182T 0585C2001 Figure 7 7 Electrical Schematic Sheet 1 of 2 7 34 Apr 30 01...

Page 209: ...CESSNA SECTION 7 MODEL 182T AIRPLANE SYSTEMS DESCRIPTION Figure 7 7 Electrical Schematic Sheet 2 of 2 0585C2001 Apr 30 01 7 35...

Page 210: ...the Master Switch is turned ON some annunciators will flash for approximately 10 seconds before illuminating steadily When the annunciator panel switch is toggled up and held in the TST position all a...

Page 211: ...ics Bus 2 is supplied through Primary circuit breakers A rocker switch located between the primary and avionics buses controls current flow to the avionics buses Placing the rocker switch in the up ON...

Page 212: ...g steadily The pilot cannot turn off the annunciator In the event an overvoltage condition occurs the alternator control unit automatically pops the ALT FLD circuit breaker removing alternator field c...

Page 213: ...tacle is gained by opening the access door The ground service plug receptacle provides the power that will close the external power contactor and battery contactor only if the master switch is turned...

Page 214: ...ced prior to flight LIGHTING SYSTEMS EXTERIOR LIGHTING Exterior lighting consists of navigation lights on the wing tips and on the aft stinger a dual landing taxi lights located in the left wing leadi...

Page 215: ...light is individually rotatable providing directional lighting for the pilot and front passenger The rear dome light is a fixed position light and provides for general illumination in the rear cabin...

Page 216: ...he pilot s lap area To operate the light first turn on the NAV light switch then adjust the map light intensity with the knurled rheostat knob Rotating the dimmer clockwise increases light intensity a...

Page 217: ...erefore the temperature of the defrosting air is the same as heated cabin air A rotating control knob labeled DEFROST regulates the volume of air to the windshield Turn the knob clockwise to ON and co...

Page 218: ...ATER VALVE VENTILATING AIR DOOR DEFROSTER OUTLET CABIN FLOOR AIR OUTLET FORWARD CABIN UPPER AIR OUTLETS REAR CABIN VENTILATING AIR OUTLETS CODE RAM AIR FLOW VENTILATING AIR HEATED AIR BLENDED AIR MECH...

Page 219: ...ion 5 for the configuration applicable to the use of the alternate static source and the correction charts AIRSPEED INDICATOR The airspeed indicator is calibrated in knots and miles per hour It incorp...

Page 220: ...mp a vacuum relief valve a vacuum system air filter vacuum operated instruments a vacuum gauge low vacuum warning on the annunciator and a manifold with check valves to allow for normal vacuum system...

Page 221: ...ent panel It is calibrated in inches of mercury and indicates vacuum available for operation of the Attitude and Directional Indicators The desired vacuum range is 4 5 to 5 5 inches of mercury Normall...

Page 222: ...em Schematic 0785C1013 CODE VACUUM INLET AIR DISCHARGE AIR LOW VACUUM TRANSDUCERS CONNECTED TO ANNUNCIATOR PANEL OVERBOARD VENT LINES ENGINE DRIVEN VACUUM PUMPS MANIFOLD CHECK VALVE VACUUM SYSTEM AIR...

Page 223: ...th a vane type stall warning system consisting of an inlet in the leading edge of the left wing which is electrically connected to a stall warning horn located in the headliner above the left cabin do...

Page 224: ...left side of the interior firewall The system utilizes a single electric fan and associated ductwork to force cool the center stack radios Power to the electric fan is supplied through the AVN FAN ci...

Page 225: ...en transmitting with the handheld microphone always hold it as closely as possible to the lips then key the microphone and speak directly into it Avoid covering opening on back side of microphone for...

Page 226: ...strument panel for control of the ELT from the flight crew station The annunciator which is in the center of the rocker switch illuminates when the ELT transmitter is transmitting The ELT emits an omn...

Page 227: ...a side to side sweeping motion VENTILATE THE CABIN PROMPTLY AFTER SUCCESSFULLY EXTINGUISHING THE FIRE TO REDUCE THE GASES PRODUCED BY THERMAL DECOMPOSITION 3 Anticipate approximately eight seconds of...

Page 228: ......

Page 229: ...ners 8 5 Publications 8 5 Airplane File 8 6 Airplane Inspection Periods 8 7 FAA Required Inspections 8 7 Cessna Inspection Programs 8 8 Cessna Customer Care Program 8 8 Pilot Conducted Preventive Main...

Page 230: ...ump 8 14 Oil and Oil Filter Change 8 14 Fuel 8 15 Approved Fuel Grades and Colors 8 15 Fuel Capacity 8 16 Fuel Additives 8 16 Fuel Contamination 8 20 Landing Gear 8 21 Cleaning And Care 8 21 Windshiel...

Page 231: ...l changes are necessary as well as other seasonal and periodic services The airplane should be regularly inspected and maintained in accordance with information found in the airplane maintenance manua...

Page 232: ...Located adjacent to the secondary Identification Plate is the Finish and Trim Plate which contains a code describing the exterior paint combination of the airplane The code may be used in conjunction...

Page 233: ...isories please complete and return an Owner Advisory Application Receipt of a valid Owner Advisory Application will establish your Cessna Owner Advisory service for one year after which you will be se...

Page 234: ...l which is lost or destroyed may be replaced by contacting your local Cessna Service Station An affidavit containing the owner s name airplane serial number and reason for replacement must be included...

Page 235: ...ents Cessna recommends that these items plus the Pilot s Checklists Customer Care Program Handbook and Customer Care Card be carried in the airplane at all times AIRPLANE INSPECTION PERIODS FAA REQUIR...

Page 236: ...hours whichever occurs first the airplane undergoes a complete Phase 3 inspection Regardless of the inspection method selected the owner should keep in mind that FAR Part 43 and FAR Part 91 establishe...

Page 237: ...tenance that may be performed by pilots A Maintenance Manual must be obtained prior to performing any preventive maintenance to ensure that proper procedures are followed Your local Cessna Service Sta...

Page 238: ...d strut will also increase tail height PARKING When parking the airplane head into the wind and set the parking brake Do not set the parking brake during cold weather when accumulated moisture may fre...

Page 239: ...ACES WHEN PUSHING ON THE TAILCONE ALWAYS APPLY PRESSURE AT A BULKHEAD TO AVOID BUCKLING THE SKIN If nose gear maintenance is required the nose wheel may be raised off the ground by pressing down on a...

Page 240: ...ane should be flown for 30 minutes or a ground runup should be made just long enough to produce an oil temperature within the lower green arc range Excessive ground runup should be avoided Engine runu...

Page 241: ...ry requirements owners should check with local aviation officials where the airplane is being operated For quick and ready reference quantities materials and specifications for frequently used service...

Page 242: ...ts the engine should be filled to capacity OIL AND OIL FILTER CHANGE After the first 25 hours of operation drain the engine oil sump and replace the filter Refill sump with straight mineral oil and us...

Page 243: ...should be checked for freedom of movement through their full range security of attachment and evidence of wear Inspect wiring for security chafing burning defective insulation loose or broken terminal...

Page 244: ...solution in the gasoline it will normally be consumed and go unnoticed in the operation of the engine One exception to this can be encountered when operating under the combined effect of 1 use of cert...

Page 245: ...llons of fuel which now reside in the tank Alcohol if used is to be blended with the fuel in a concentration of 1 by volume Concentrations greater than 1 are not recommended since they can be detrimen...

Page 246: ...SECTION 8 CESSNA HANDLING SERVICE MAINTENANCE MODEL 182T Figure 8 1 Fuel Mixing Ratio 0585C1001 8 18 Apr 30 01...

Page 247: ...NK AND SEALANT AND DAMAGE TO O RINGS AND SEALS USED IN THE FUEL SYSTEM AND ENGINE COMPONENTS A CONCENTRATION OF LESS THAN THAT RECOMMENDED 0 10 BY TOTAL VOLUME MINIMUM WILL RESULT IN INEFFECTIVE TREAT...

Page 248: ...epeated sampling evidence of contamination still exists the airplane should not be flown Tanks should be drained and system purged by qualified maintenance personnel All evidence of contamination must...

Page 249: ...and rub with moderate pressure until all dirt oil scum and bug stains are removed Allow the cleaner to dry then wipe it off with soft flannel cloths NEVER USE GASOLINE BENZENE ALCOHOL ACETONE FIRE EX...

Page 250: ...asive soaps or detergents which cause corrosion or scratches should never be used Remove stubborn oil and grease with a cloth moistened with Stoddard solvent Take special care to make sure that the ex...

Page 251: ...Small nicks on the propeller particularly near the tips and on the leading edges should be dressed out as soon as possible since these nicks produce stress concentrations and if ignored may result in...

Page 252: ...en spot clean the area Oily spots may be cleaned with household spot removers used sparingly Before using any solvent read the instructions on the container and test it on an obscure place on the fabr...

Page 253: ...pplicable supplements have been placed in the Pilot s Operating Handbook POH Supplements may be removed from the POH provided the equipment is not installed on the airplane If equipment is installed o...

Page 254: ......

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