Pilot's Operating Handbook and FAA Approved Airplane Flight Manual

registration number shown on the Title Page. This handbook is applicable to 182T airplanes equipped with the Nav Ill Avionics Option. All information is based on data available at the time of publication. I This handbook consists of nine sections that cover all operational aspects of a standard -equipped airplane. Following Section 8 are the Supplements, Section 9, which provide expanded operational procedures for the avionics equipment (both standard and optional), and provides information on special operations. Supplements are individual documents and may be issued or revised without regard to revision dates which apply to the POH litself. These supplements contain a Log of-Effective Pages, which should be used to determine the status of each supplement. ORIGINAL ISSUE AND REVISIONS This Pilot's Operating Handbook and FAA Approved Airplane Flight Manual is comprised of the original issue and any subsequent (revisions. To make sure that information in this manual is current, the revisions must be incorporated as they are issued. As revisions lare issued, they will be noted in the Log of Effective Pages. The part number of this manual has also been designed to further aid the ownerloperator in determining the revision level of any POH. Refer to the example below for a breakdown: 84062 182T PHAUS -00 TLRevision Level (Revision 0 , Original Issue) M a n u a l (Pilot's Operating Handbook, NAV Ill, U.S.) Airplane Model (18 2 7 (Continued Next Page) I v i U.S. CESSNA MODEL 182T NAV Ill ORIGINAL ISSUE AND REVISIONS (Continued) It is the responsibility of the owner to maintain this handbook in a current status when it is being used for operational purposes. Owners should contact their local Cessna Service Station whenever1 the revision status of their handbook is in question. Revisions are distributed to owners of U.S. Registered aircraft according to FAA records at the time of revision issuance and to Internationally Registered aircraft according to Cessna Owner Advisory records at the time of issuance. Revisions should be read carefully upon receipt and incorporated into this POH. REVISION FILING INSTRUCTIONS REGULAR REVlSlONS Pages to be removed or inserted in the Pilots' Operating Handbook and FAA Approved Airplane Flight Manual are determined by the Log of Effective Pages located in this section. This log contains the page number and revision level for each page within the POH. As revisions to the POH occur, the revision level on effected pages is updated. When two pages display the same page number, the page with the latest revision level shall be inserted into the POH. The revision level on the Log Of Effective Pages shall also agree with the revision level of the page in question. TEMPORARY REVISIONS Under limited circumstances, temporary revisions to the POH may be issued. These temporary revisions are to be filed in the applicable section in accordance with filing instructions appearing on the first page of the temporary revision. The recession of a temporary revision is accomplished by incorporation into the POH at revision time or by a superseding temporary revision. In order to accurately track the status of temporary revisions as they pertain to a POH, a Temporary Revision List will be located previous to this section when required. This list will indicate the date the temporary revision was incorporated into the POH, thus authorizing the recession of the temporary revision. 1182TPHAUS - 02 U.S. vii INTRODUCTION CESSNA MODEL 182T NAV III IDENTIFYING REVISED MATERIAL I A bar located in the outer margin adjacent to the applicable text will extend the full length of new pages and deleted, new, or revised text added on new or presently existing pages. I A bar in the footer will indicate a revision to the headerlfooter, a new page, format or spellinglgrammar changes andlor that information has slipped to or from that page. IA bar located adjacent to the figure number in the outer margin will be used to indicate that the figure number only has changed. A miniature pointing hand W will be used to indicate that an illustration has been revised or is all new material. The miniature hand will point to the figure number. All revised pages will carry the revision number opposite the page number on the applicable page. A list of revisions is located at the beginning of the Log Of Effective Pages. WARNINGS, CAUTIONS AND NOTES Throughout the text, warnings, cautions and notes pertaining to airplane handling and operations are utilized. These adjuncts to the text are used to highlight or emphasize important points. WARNING OPERATING PROCEDURES, TECHNIQUES, ETC., WHICH WlLL RESULT IN PERSONAL INJURY OR LOSS OF LIFE IF NOT CAREFULLY FOLLOWED. CAUTION OPERATIOIV PROCEDURES, TECHNIQUES, ETC., WHICH WlLL RESULT IN DAMAGE TO EQUIPMENT IF NOT CAREFULLY FOLLOWED. NOTE An operating procedure, technique, etc., which is considered essential to emphasize. viii U.S. CESSNA MODEL 182T NAV Ill INTRODUCTION LOG OF EFFECTIVE PAGES Use this page to determine the currency and applicability of your - POH. Pages affected by the current revision are indicated by an asterisk (*) preceding the pages listed under the Page Number column. Revision Number Date Revision Number Dlte - Original 3 June 2004 Revision 3 19 July 2005 Revision 1 24 June 2004 Revision 4 22 December 2005 Revision 2 27 June 2005 Page Number * Title Assignment Record * i/ii iii thru vii * viii thru xilxii xiiilxiv 1 - 111 - 2 thru 1 - 26 * 1 - 27 thru 1 - 28 * 2-112-2 thru 2 - 4 2 - 5 * 2 - 6 thru 2 - 9 2 - 10 2 - 11 * 2 - 12 2 - 13 * 2 - 14 thru 2 - 20 2-2112-22 Page Status Revised Revised Revised Revised Revised Revised Original Revised Revised Original Revised Revised Revised Revised Revised Revised Added (Continued Next Page) Revision Number U.S. ix INTRODUCTION CESSNA MODEL 182T NAV Ill LOG 0F EFFECTIVE PAGES (Continued) Page Number Page Status Revision Number 3 - 1 3 - 2 thru 3-313-4 3 - 5 * 3 - 6 thru 3 - 21 3 - 22 * 3 - 23 3 - 24 thru 3 - 25 * 3- 26 thru 3 - 31 3 - 32 thru 3 - 33 * 3 - 34 3-35 * 3 - 36 Revised Revised Revised Revised Revised Revised Revised Revised Revised Revised Revised Revised * 4- 1 thru 4 - 48 Revised * 4- 49 thru 4-5114-52 Added 5- 1 15-2 thru 5 - 36 Original 6-116-2 thru 6 - 24 Revised 6-2516-26 Added * 7 - 1 thru 7-317-4 7 - 5 thru 7 - 11 * 7 - 12 7 - 13 thru 7 - 14 7- 15 thru 7 - 18 7 - 19 thru 7 - 26 7 - 27 7 - 28 thru 7 - 35 * 7 - 36 7 - 37 thru 7 - 47 * 7 - 48 thru 7 - 51 7 - 52 thru 7 - 53 7 - 54 thru 7 - 55 Revised Original Revised Original Revised Original Revised Original Revised Original Revised Revised Revised (Continued Next Page) I x U.S. CESSNA MODEL 182T NAV Ill INTRODUCTION LOG OF EFFECTIVE PAGES (Continued) Page Number 7 - 56 thru 7 - 57 * 7-58 thru 7- 59 7-60 - * 7-61 thru 7- 62 7-63 thru 7 - 66 * 7-67 thru 7-7517-76 '8 - 1 thru 8 - 2 8-3 thru 8-5 8 - 6 8-7 thru 8-8 * 8-9 thru 8-12 8 - 13 * 8 - 14 8-15 thru 8- 22 * 8-23 thru 8- 24 Page Status Original Revised Criginal Revised Original Revised Revised Original Revised Original Revised Original Revised Original Revised Original Revision Number DATE OF APPROVAL a3, OhCEUBEp U.S. xilxii CESSNA INTRODUCTION MODEL 182T NAV Ill TABLE OF CONTENTS SECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GENERAL 1 LIMITATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . 2 EMERGENCY PROCEDURES . . . . . . . . . . . . . . 3 NORMAL PROCEDURES . . . . . . . . . . . . . . . . . 4 PERFORMANCE . . . . . . . . . . . . . . . . . . . . . . . . 5 WEIGHT AND BALAIVCEIEQUIPMENT LIST . . . . 6 AIRPLANE AND SYSTEMS DESCRIPTION . . . . 7 HANDLING. SERVICE AND MAINTENANCE . . . 8 . . . . . . . . . . . . . . . . . . . . . . . . SUPPLEMENTS 9 CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL GENERAL TABLE OF CONTENTS Page . . . . . . . . . . . . . . . . . . . Three View . Normal Ground Attitude 1 - 3 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Descriptive Data 1 -5 Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-5 Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 5 Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 6 Oil . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 7 . . . . . . . . . . . . . . . . . . . . . Maximum Certificated Weights 1 - 8 . . . . . . . . . . . . . . . . . . . . . . . . Standard Airplane Weights 1-8 . . . . . . . . . . . . . . . . . . . . . . . Cabin And Entry Dimensions 1 - 8 . . . . . . . . . . . . . . . Baggage Space And Entry Dimensions 1-8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Specific Loadings 1 -8 . . . . . . . . . . . . . . . . Symbols, Abbreviations And Terminology 1 - 9 . . . . . . . . . . . General Airspeed Terminoiogy And Symbois 1-5 . . . . . . . . . . . . . . . . . . . . . . . Meteorological Terminology 1 - 10 . . . . . . . . . . . . . . . . . . . . . . . Engine Power Terminology 1 - 10 Airplane Performance And Flight Planning Terminology . . 1-11 . . . . . . . . . . . . . . . . . . Weight And Balance Terminology 1 - 12 . . . . . . . . . . . . . . . . Metricllmperial1U.S. Conversion Charts 1 -14 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Weight Conversions 1-15 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Length Conversions 1 - 17 . . . . . . . . . . . . . . . . . . . . . . . . . . . Distance Conversions 1 - 21 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Volume Conversions 1- 22 . . . . . . . . . . . . . . . . . . . . . . . . Temperature Conversions 1 -25 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pressure Conversion 1 - 26 . . . . . . . . . . . . . . . . . . . . . Volume to Weight Conversion 1- 27 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Quick Conversions 1 - 28 U.S. 1-111-2 CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL THREE VIEW - NORMAL GROUND ATTITUDE b-11'- 8" - 4 Figure 1 - 1 (Sheet 1 of 2) (Continued Next Page) U.S. 1 - 3 SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill THREE VIEW - NORMAL GROUND AlTITUDE (Continued) k-29'- 0" -I NOTE a Wing span shown with standard strobe lights installed. a Wheel base length is 66 1/2". a Propeller ground clearance is 10 7/8". a Wing area is 174 square feet. a Minimum turning radius ('pivot point to outboard wing tip) is 27' - 0 . a Normal ground attitude is shown with nose strut showing approximately 2" of strut, and wings level. Figure 1 - 1 (Sheet 2) 1 - 4 U.S. CESSNA MODEL 182T NAV Ill SECTlOlV 1 GENERAL INTRODUCTION This handbook contains 9 sections and includes the material - required to be furnished to the pilot by FAR Part 23. It also contains supplemental data supplied by Cessna Aircraft Company. Section 1 provides basic data and information of general interest. It also contains definitions and explanations of symbols, abbreviations, and terminology commonly used. DESCRIPTIVE DATA ENGINE Number of Engines: 1. Engine Manufacturer: Textron Lycoming. Engine Model Number: 10-540-AB1A5. Engine Type: Normally aspirated, direct drive, air - cooled, horizontally opposed, fuel injected, six cylinder enaine with 541 cu. in. dis~lacement. Horsepower ~ating"andEngine Speed: 230 rated BHP at 2400 RPM. PROPELLER Propeller Manufacturer: McCauley Propeller Systems. Propeller Model Number: B3D36C43118OVSA-1. Number of Blades: 3. Propeller Diameter: 79.0 inches. Propeller Type: Constant speed and hydraulically actuated, with a low pitch setting of 14.9 " and a high pitch setting of 31.7" (30 inch station). (Continued Next Page) U.S. 1 - 5 SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill DESCRIPTIVE DATA (Continued) FUEL WARNING USE OF UNAPPROVED FUELS MAY RESULT IN DAMAGE TO THE ENGINE AND FUEL SYSTEM COMPONENTS, RESULTING IN POSSIBLE ENGINE FAILURE. Approved Fuel Grades (and Colors): 100LL Grade Aviation Fuel (Blue). 100 Grade Aviation Fuel (Green). NOTE lsopropyl alcohol or diethylene glycol monomethyl ether (DiEGME) may be added to the fuel supply. Additive 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. gallons Total Capacity Each Tank: . . . . . . . . . . . . . . . 46.0 U.S. gallons Total Usable Each Tank: . . . . . . . . . . . . . . . . 43.5 U.S. gallons NOTE To ensure maximum fuel capacity and minimize crossfeeding when refueling, always park the airplane in a wings level, normal ground attitude and place the fuel selector in the LEFTorRlGHT p o s ~ t ~ o "Refer to Figure 1-1 for normal ground attitude dimensions. (Continued Next Page) CESSNA MODEL 182T NAV III SECTION 1 GENERAL DESCRIPTIVE DATA (Continued) OIL Oil Specification: MIL -L- 6082 or SAE J1966 Aviation Grade Straight Mineral Oil: used when the airplane was delivered from the factory and should be used to replenish the supply during the first 25 hours. This oil should be drained and the filter changed after the first 25 hours of operation. Refill the engine with MIL -L- 6082 or- SAE ~196% Aviation Grade Straight Mineral Oil and continue to use until a total of 50 hours has accumulated or oil consumption has stabilized. MIL -L- 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 once oil consumption has stabilized. Recommended viscosity for temperature range: or SAE J1899 NOTE When operating temperatures overlap, use the lighter grade of oil. Oil Capacity: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Sump: 8 U.S. quarts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Total: 9 U.S. quarts (Continued Next Page) SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill DESCRIPTIVE DATA (Continued) MAXIMUM CERTIFICATED WEIGHTS Ramp Weight: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3110 Ibs Takeoff Weight: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3100 Ibs Landing Weight: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2950 Ibs Weight in Baggage Compartment, Normal Category: Baggage Area A (Station 82 to 109): . . . . . . . . . . . . . . . . 120 Ibs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refer to note below. Baggage Area B (Station 109 to 124): . . . . . . . . . . . . . . . . 80 Ibs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refer to note below. Baggage Area C (Station 124 to 134): . . . . . . . . . . . . . . . . 80 Ibs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refer to note below. NOTE The maximum allowable combined 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: . . . . . . . . . . . . . . . . . . . . . . . . 1924 Ibs Maximum Useful Load, Normal Category: . . . . . . . . . . . 1186 Ibs CABIN AND ENTRY DIMENSIONS Detailed dimensions of the cabin interior and entry door openings are illustrated in Section 6. BAGGAGE SPACE AND ENTRY DIMENSIONS Dimensions of the baggage area and baggage door opening are illustrated in detail in Section 6. SPECIFIC LOADINGS Wing Loading: . . . . . . . . . . . . . . . . . . . . . . . . . . . 17.8 Ibslsq. ft. Power Loading: . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13.5 Ibslhp. 1 - 8 U.S. - - -- - 4 nn-r I O L I PHAUS-00 CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL SYMBOLS, ABBREVIATIONS AND TERMINOLOGY GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS Knots Calibrated Airspeed is indicated airspeed corrected for position and instrument error and expressed in knots. Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea level. KlAS KTAS Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots. Knots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitude and temperature. Maneuvering Speed is the maximum speed at which full or abrupt control movements may be used. Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air, then only with caution. Never Exceed Speed is the speed limit that may not be exceeded at any time. Stalling Speed or the minimum steady flight speed is the minimum speed at which the airplane is controllable. Stalling Speed or the minimum steady flight speed is the minimum speed at which the airplane is controllable in the landing configuration at the most forward center of gravity. (Continued Next Page) U.S. 1 - 9 SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) VX Best Angle-of-Climb Speed is the speed which results in the greatest gain of altitude in a given horizontal distance. VY Best Rate-of-Climb Speed is the speed which results in the greatest gain in altitude in a given time. METEOROLOGICAL TERMINOLOGY OAT Outside Air Temperature is the free air siaiic temperature. It may be expressed in either degrees Celsius or degrees Fahrenheit. Standard Temperature Standard Temperature is 15°C at sea level pressure altitude and decreases by 2°C for each 1000 feet of altitude. Pressure Altitude Pressure Altitude is the altitude read from an altimeter when the altimeter's barometric scale has been set to 29.92 inches of mercury (1013 mb). ENGINE POWER TERMINOLOGY BHP Brake Horsepower is the power developed by the engine. Static RPM Static RPM is engine speed attained during a full throttle engine runup when the airplane is on the ground and stationary. MP Manifold Pressure is a pressure measured in the engine's induction system and is expressed in inches of mercury (in Hg). MCP Maximum Continuous Power (Continued Next Page) 1 - 10 U.S. CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Demonstrated Crosswind Velocity Demonstrated Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplane during takeoff and landing was actually demonstrated during certification tests. The value shown is not considered to be limiting. Usable Fuel Usable Fuel is the fuel available for flight planning. Unusable Fuel Unusable Fuel is the quantity of fuel that can not be safely used in flight. GPH Gallons Per Hour is the amount of fuel consumed per hour. N NlPG Nautical Miles Per Gallon is the distance which can be expected per gallon of fuel consumed at a specific engine power setting andlor flight configuration. 9 g is acceleration due to gravity. Course Datum Course Datum is the compass reference used by the autopilot, along with course deviation, to provide lateral control when tracking a navigation signal. (Continued Next Page) U.S. 1 - 11 SECTION 1 GENERAL CESSNA MODEL 182T NAV III SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) WEIGHT AND BALANCE TERMINOLOGY Reference Datum Reference Datum is an imaginary vertical plane from which all horizontal distances are measured for balance purposes. Station Station is a location along the airplane fuselage given in terms of the distance from the reference datum. Arm Arm is the horizontal distance from the reference datum to the center of gravity (C.G.) of an item. Moment Moment 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 reducing the number of digits.) Center of Gravity (C.G.) Center of Gravity is the point at which an airplane, or equipment, would balance if suspended. Its distance from the reference datum is found by dividing the total moment by the total weight of the airplane. C.G. Arm Center of Gravity Arm is the arm obtained by adding the airplane's individual moments and dividing the sum by the total weight. C.G. Limits Center of Gravity Limits are the extreme center of gravity locations within which the airplane must be operated at a given weight. Standard Empty Weight Standard Empty Weight is the weight of a standard airplane, including unusable fuel, full operating fluids and full engine oil. (Continued Next Page) 1- 12 U.S. CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) Basic Empty Weight Basic Empty Weight is the standard empty weight plus the weight of optional equipment. Useful Load Useful Load is the difference between ramp weight and the basic empty weight. MAC MAC (Mean Aerodynamic Chord) is a chord of an imaginary rectangular airfoil having the same pitching moments throughout the flight range as that of the actual wing. Maximum Ramp Weight Maximum Ramp Weight is the maximum weight approved for ground maneuver, and includes the weight of fuel used for start, taxi and runup. Maximum Takeoff Weight Maximum Takeoff Weight is the maximum weight approved for the start of the takeoff roll. Maximum Landing Weight Maximum Landing Weight is the maximum weight approved for the landing touchdown. Tare Tare is the weight of chocks, blocks, stands, etc. used when weighing an airplane, and is included in the scale readings. Tare is deducted from the scale reading to obtain the actual (net) airplane weight. U.S. 1 -13 SECTION 1 GENERAL CESSNA MODEL 182T NAV III METRIC1IMPERIAUU.S. CONVERSION CHARTS The following charts have been provided to help international operators convert U.S. measurement supplied with the Pilot's Operating Handbook into metric and imperiai measurements. The standard followed for measurement units shown is the National Institute of Standards Technology (NIST), Publication 811, " Guide for the Use of the International System of Units (SI)." Please refer to the following pages for these charts. 1 -14 U.S. CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL WEIGHT CONVERSIONS (Kilograms x 2.205 = Pounds) (Pounds x .454 = Kilograms) KILOGRAMS INTO POUNDS KILOGRAMMES EN LIVRES POUNDS INTO KILOGRAMS LIVRES EN KILOGRAMMES k9 0 Figure 1 - 2 (Sheet 1 of 2) 1 Ib. 2.205 24.251 46.297 68.343 90.390 112.44 134.48 156.53 178.57 200.62 222.67 0 10 20 30 40 50 60 70 80 90 100 U.S. 1 - 15 Ib. 22.046 44.093 66139 88.185 110.23 132.28 154.32 176.37 198.42 220.46 2 Ib. 4.409 26.456 48.502 70.548 92.594 114.64 136.69 158.73 180.78 202.83 224.87 6 kg 2.722 7.257 11.793 16.329 20.865 25.401 29.937 34.473 39.009 43.545 48.081 Ib. 0 1 kg 0.454 4.990 9.525 14.061 18.597 23.133 27.669 32.205 36.741 41.277 45.813 0 10 20 30 40 50 60 70 80 90 100 3 Ib. 6.614 28.660 50.706 72.753 94.799 7 kg 3.175 7.711 12.247 16.783 21.319 25.855 30.391 34.927 39.463 43.999 48.534 kg 4.536 9.072 13.608 18.144 22.680 27.216 31.752 36.287 40.823 45.359 2 kg 0.907 5.443 9.979 14.515 19.051 23.587 28.123 32.659 37.195 41.731 46.266 4 Ib. 8.819 30.865 52.91 1 74.957 97.003 8 kg 3.629 8.165 12.701 17.237 21.772 1 ~ 1 ~ 1 ~ 1 I 26.303 30.844 35.380 39.916 44.452 48.988 116.85 119.05 121.25 123.46 125.66 127.87 130.07 138.89 I I I I I 141.10 143.30 145.51 147.71 149.91 I 152.12 I 3 kg 1.361 5.897 10.433 14.969 19.504 24.040 28.576 33.112 37.648 42.184 46.720 9 kg 4.082 8.618 13.154 17.690 22.226 26.762 31.298 35.834 40.370 44.906 49.442 5 Ib. 11.023 33.069 55.116 77.162 99.208 160.94 182.98 205.03 227.08 4 kg 1.814 6.350 10.886 15.422 19.958 24.494 29.030 33.566 38.102 42.638 47.174 6 Ib. 13.228 35.274 57.320 79.366 101.41 171.96 194.01 216.05 238.10 5 kg 2.268 6.804 11.340 15.876 20.412 24.948 29.484 34.019 38.555 43.091 47.627 174.17 196.21 218.26 240.30 163.14 185.19 207.24 229.28 7 Ib. 15.432 37.479 59.525 81.571 103.62 165.35 187.39 209.44 231.49 8 Ib. 17.637 39.683 61.729 83.776 105.82 9 Ib. 19.842 41.888 63.934 85.980 108.03 167.55 189.60 211.64 233.69 169.76 191.80 213.85 235.90 SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill WEIGHT CONVERSIONS (Kilograms x 2.205 = Pounds) (Pounds x .454 = Kilograms) POUNDS KILOGRAMS 1 - 16 U.S. 150- 140- 1 120--55 110 100 90 - 8 0 - 70 - 60 - 50 - 40 - 30 - 2 0 - - 10 0 - 70 -65 3 0 p 6 0 50 45 40 35 ---- 30 -25 -20 -15 10 5 0 Figure 1 - 2 (Sheet 2) CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL LENGTH CONVERSIONS (Meters x 3.281 = Feet) (Feet x .305 = Meters) METERS INTO FEET METRES EN PlEDS FEET INTO METERS PlEDS EN METRES Figure 1 - 3 (Sheet 1 of 4) m 0 U.S. 1-17 0 10 20 30 40 50 60 70 80 90 100 1 feet 3.281 36.089 68.897 101.71 134.51 167.32 200.13 232.94 265.75 298.56 331.36 feet - - - 32.808 65.617 98.425 131.23 164.04 195.85 229.66 262.47 295.27 328.08 3 feet 9.842 42.651 75.459 108.27 141.08 173.86 206.69 239.50 272.31 305.12 337.93 2 feet 6.562 39.370 72.178 104.99 137.79 170.60 203.41 236.22 269.03 301.84 334.64 4 feet 13.123 45.932 78.740 111.55 144.36 177.16 209.97 242.78 275.59 308.40 341.21 5 feet 16.404 49.212 82.021 114.83 147.64 180.45 213.25 246.06 278.87 311.68 344.49 6 feet 19.685 52.493 85.302 118.11 150.92 183.73 216.53 249.34 282.15 314.96 347.77 7 feet 22.956 55.774 88.582 121.39 154.20 187.01 219.82 252.62 285.43 318.24 351.05 8 feet 26.247 59.055 91.863 124.67 157.48 I l l 190.29 223.10 255.90 288.71 321.52 354.33 9 feet 29.528 62.336 95.144 127.95 160.76 193.57 226.38 259.19 291.58 324.80 357.61 SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill LENGTH CONVERSIONS (Meters x 3.281 = Feet) (Feet x .305 = Meters) FEET METERS 15 10 20 5 0 Units x 10, 100, etc. Figure 1 - 3 (Sheet 2) 1-18 U.S. CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL LENGTH CONVERSIONS (Centimeters x ,394 = Inches) (Inches x 2.54 = Centimeters) CENTIMETERS INTO INCHES CENTIMETRES EN POUCES INCHES INTO CENTIMETERS POUCES EN CENTIMETRES crn 0 Figure 1 - 3 (Sheet 3) 1 in. 0.394 4.331 8.268 12.205 16.142 20.079 24.016 27.953 31.890 35.827 39.764 0 10 20 30 40 50 60 70 80 90 100 U.S. 1 - 19 in. ... 3.937 7.874 11.811 15.748 19.685 23.622 27.559 31.496 35.433 39.370 in. 0 2 in. 0.787 4.724 8.661 12.598 16.535 20.472 24.409 28.346 32.283 36.220 40.157 1 crn 2.54 27.94 53.34 78.74 104.14 129.54 154.94 180.34 205.74 231 .I4 256.54 0 10 20 30 40 50 60 70 80 90 100 crn ... 25.40 50.80 76.20 101.60 127.00 152.40 177.80 203.20 228.60 254.00 3 in. 1.181 5.118 9.055 12.992 16.929 20.866 24.803 28.740 32.677 36.614 40.551 2 crn 5.08 30.48 55.88 81.28 106.68 132.08 157.48 182.88 208.28 233.68 259.08 4 in. 1.575 5.512 9.449 13.386 17.323 21.260 25.197 29.134 33.071 37.008 40.945 3 cm 7.62 33.02 58.42 83.82 109.22 134.62 160.02 185.42 210.82 236.22 261.62 5 in. 1.969 5.906 9.843 13.780 17.717 21.654 25.591 29.528 33.465 37.402 41.339 4 crn 10.16 35.56 60.96 86.36 111.76 137.16 162.56 187.96 213.36 238.76 264.16 6 i n . 2.362 6.299 10.236 14,173 18.110 22.047 25.984 29.921 33.858 37.795 41.732 5 crn 12.70 38.10 63.50 88.90 114.30 139.70 165.10 190.50 7 i n . 2.756 6.693 10.630 14.567 18.504 22.441 26.378 30.315 34.252 38.189 42.126 266.70 269.24 271.78 274.32 276.86 6 cm 15.24 40.64 66.04 91.44 116.84 142.24 167.64 193.04 8 i n . 3.150 7.087 11.024 14.961 18.898 22.835 26.772 30.709 34.646 38.583 42.520 7 crn 17.78 43.18 68.58 93.98 119.38 144.78 170.18 195.58 9 in. 1 3.543 7.480 11.417 15.354 19.291 23.228 27.164 31.102 35.039 38.976 42.913 8 crn 20.32 45.72 71.12 96.52 121.92 147.32 172.72 198.12 9 cm 22.96 48.26 73.66 99.06 124.46 149.86 175.26 200.66 SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill LENGTH CONVERSIONS (Centimeters x .394 = Inches) (Inches x 2.54 = Centimeters) INCHES CENTINIETERS 2 Units x TO, 5 00, eic. 0 0585T1028 Figure 1 - 3 (Sheet 4) 1 - 20 U.S. CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL DISTANCE CONVERSIONS (Statute Miles xl.609=Kilometers) (Kilometers x.622Statute Miles) (Statute Miles x.E69=Nautical Miles) (Nautical Miles x l .15=Statute Miles) (Nautical Miles xl.E52=Kilorneters) (Kilometers x.54=Nautical Miles) STATUTE NAUTICAL MILES MILES KILOMETERS 105 160 U.S. 1 - 21 65 -- 60 - 55 - 50 - 45 -- 40 35 30 25 20 - 15 - 1 0 - 5 Figure 1 - 4 55 55 -- - 50 50 -- - 45 40 45 -- 40 - -- 35 35 - -- 30 30 - -- 25 25 - -- 20 20 - - 15 - l o ' -- 5 0 - 0 100 90 80 - 70 - 60 - 50 40 - I ~ - - ~ O -- 20 Units x 10, 100, etc. --lo 0 - 0 0585T1029 SECTION 1 GENERAL CESSNA MODEL 182T NAV III VOLUME CONVERSIONS (Imperial Gallons x 4.546 = Liters) (Liters x .22 = Imperial Gallons) LITERS INTO IMPERIAL GALLONS LITRES EN GALLONS IMPERIAL IMPERIAL GALLONS INTO LITERS GALLONS IMPERIAL EN LITRES Figure 1-5 (Sheet 1 of 3) 1- 22 U.S. CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL VOLUME CONVERSIONS (Imperial Gallons X 4.4546 = Liters) (Liters x .22 = Imperial Gallons) IMPERIAL 440 LITERS '$: Units x 10, 100, etc. Figure 1 - 5 (Sheet 2) U.S. 1-23 SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill VOLUME CONVERSIONS (Imperial Gallons x 1.2 = U.S. Gallons) (U.S. Gallons x .833 = Imperial Gallons) (U.S. Gallons x 3.785 = Liters) (Liters x .264 = U.S. Gallons) IMPERIAL U. S. LITERS 100 120 Units x 10, 100, etc. Figure 1 - 5 (Sheet 3) 0585~1033 1 - 24 U.S. CESSNA MODEL 182T NAV III TEMPERATURE CONVERSIONS Figure SECTION 1 GENERAL U.S. 1 - 25 SECTION 1 GENERAL CESSNA MODEL 182T NAV Ill PRESSURE CONVERSION Hectopascals (Millibars) to inches Mercury (inHG) Figure 1 - 7 1 - 26 U.S. CESSNA MODEL 182T NAV Ill SECTION 1 GENERAL VOLUME TO WEIGHT CONVERSION 8 W 8 AVGAS Specific Gravity = .72 (Liters x .72 = Kilograms) (Kilograms x 1.389 = Liters) (Liters x 1.58 = Pounds) (Pounds x .633 = Liters) LITERS POUNDS LITERS KILOGRAMS 1-140 125 - - 90 ,130 AVGAS FUEL 1120 15 IB5110 80 Units x 10, 100, etc. ICFigure 1 - 8 U.S. 1 - 27 SECTION 1 GENERAL CESSNA MODEL 182T NAV III QUICK CONVERSIONS R 31x0 0585T1031 R Figure 1 - 9 1 - 28 U.S. CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS OPERATING LIMITATIONS TABLE OF CONTENTS Page Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Airspeed Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Airspeed Indicator Markings . . . . . . . . . . . . . . . . . . . . . . . . . . Powerplant Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Powerplant Instrument Markings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Weight Limits Center- Of-Gravity Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . ManeuverLimits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flight Load Factor Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . Kinds Of Operations Limits . . . . . . . . . . . . . . . . . . . . . . . . . . Kinds Of Operations Equipment List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flap Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . System Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Aux Audio System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12V Power System G I 000 Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BendixIKing KAP 140 2 Axis Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . L3 Communications WX - 500 Stormscope Traffic Advisory System (TAS) . . . . . . . . . . . . . . . . . . . . . Terrain Awareness and Warning System (TAWS - B) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Placards IFAA APPROVED 182TPHAUS-04 U.S. 2-112-2 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS INTRODUCTION Section 2 includes operating limitations, instrument markings, and basic placards necessary for the safe operation of the airplane, its erlgine, standard systems and standard equipment. The limitations included in this section and in Section 9 have been approved by the Federal Aviation Administration. Observance of these operating limitations is required by Federal Aviation Regulations. NOTE Refer to Supplements, Section 9 of this Pilot's Operating Handbook for amended operating limitations, operating procedures, performance data and other necessary information for airplanes I equipped with specific options. The airspeeds listed in Figure 2 - 1, Airspeed Limitations, and Figure 2- 2, Airspeed Indicator Markings, are based on Airspeed Calibration data shown in Section 5 with the normal static source. If the alternate static source is being used, ample margins should be observed to allow for the airspeed calibration variations between the normal and alternate static sources as shown in Section 5. The Cessna Model No. 182T is certificated under FAA Type Certificate No. 3A13. FAA APPROVED 182TPHAUS- 04 U.S. 2 - 3 SECTION 2 OPERATING LIMITATIONS CESSNA MODEL 182T NAV Ill AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown in Figure 2 - 1. 2 - 4 U.S. AIRSPEED LIMITATIONS Figure 2 - 1 I FAA APPROVED 182TPHAUS-04 SYMBOL VNE VNo VA VFE ---- - SPEED Never Exceed Speed Maximum Structural Cruising Speed Maneuvering Speed: 3100 Pounds 2600 Pounds 2100 Pounds Maximum Flap Extended Speed: Flaps LIP to 10 " Flaps 10" to 20" Flaps 20" to FULL Maximum Window Open Speed KCAS 171 136 108 100 91 136 117 99 171 KlAS 175 140 110 101 91 140 120 100 175 REMARKS Do not exceed this speed in any operation. Do not exceed this speed except in smooth air, and then only with caution. Do not make full or abrupt control movements above this speed. Do not exceed this speed with flaps down. Do not exceed this speed with windows open. CESSNA MODEL 182T NAV Ill SEC-rIOI'42 OPERATING I-IMITATIONS AIRSPEED INDICATOR MARKINGS Airspeed indicator markings and their color code significance are shown in Figure 2- 2. Red Arc* AIRSPEED INDICATOR MARKINGS White Arc Green Arc SIGNIFICANCE MARKING Yellow Arc KlAS VALUE OR RANGE 20 - 41 ILOW airspeed warning. 1 140 - 175 Operations must be conducted with lcaution and onlv in smooth air. 41 - 100 51 - 140 Full Flap Operating Range. Lower limit is maximum weight VSO in landing configuration. Upper limit is maximum speed permissible with flaps extended. Normal Operating Range. Lower limit is maximum weight VS at most forward C.G. with flaps retracted. Upper limit is maximum structural cruising speed. Figure 2 -2 Red Line FAA APPROVED 182TPHAUS-00 175 1 ~ a x i m u mspeed for all operations. U.S. 2-5 * G I 000 airspeed indicator only. SECTION 2 OPERATING LIMITATIONS CESSNA MODEL 182T NAV Ill POWERPLANT LIMITATIONS Engine Manufacturer: Textron Lycoming. Engine Model Number: 10-540-AB1A5. Maximum Power: 230 BHP rating. Engine Operating Limits for Takeoff and Continuous Operations: . . . . . . . . . . . . . . . . . . . Maximum Engine Speed 2400 RPM Maximum Cylinder Head Temperature . . . . . . 500°F (260°C) . . . . . . . . . . . . . . . Maximum Oil Temperature 245°F (118°C) . . . . . . . . . . . . . . . . . . . . . . . Oil Pressure, Minimum 20 PSI . . . . . . . . . . . . . . . . . . . . . . Oil Pressure, Maximum 115 PSI Fuel Grade: Refer to Fuel Limitations. Oil Grade (Specification): MIL-L- 6082 or SAE J1966 Aviation Grade Straight Mineral Oil or I MIL -L- 22851 or SAE J1899 Ashless Dispersant Oil. Oil must comply with the latest revision and/or supplement for Textron Lycoming Service Instruction No. 1014. Propeller Manufacturer: McCauley Propeller Systems Propeller Model Number: B3D36C431180VSA-1. l ~ r o p e l l e rDiameter: 79 INCHES Propeller Blade Angle at 30 Inch Station: Low: 14.9" High: 31.7" 2 - 6 U.S. FAA APPROVED 182TPHAUS - 04 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LllVllTATlONS POWERPLANT INSTRUMENT MARKINGS Powerplant instrument markings and their color code significance are shown in Figure 2- 3. Operation with indications in the red range is prohibited. Avoid operating with indicators in the yellow range. POWERPLANT INSTRUMENT MARKINGS Figure 2 - 3 IFAA APPROVED 182TPHAUS- 04 RED (MAX) ---- INSTRUMENT Tachometer U.S. 2 - 7 Manifold Pressure Cylinder Head Temperature Oil Temperature Oil Pressure Fuel Quantity Fuel Flow Vacuum Gage RED LINE (MIN) ---- "Maximum operating limit is lower end of red arc. ---- ---- ---- ---- 0 (2.5 Gallons Unusable Each Tank) ---- ---- RED ARC (LWR) ---- ---- ---- ---- o to 20 PSI ---- ---- ---- YELLOW ARC ---- ---- ---- ---- ---- 0 i o 8 Gallons ---- ---- GREEN ARC (NORMAL OPERATING RANGE) 2000 to 2400 RPM 15 to 23 1ii.iig I -- - - I - --- 200 to 500°F - - - - 500°F 100 to 245°F 245' to ---- 250°F 50 to 90 PS I 115' to - - -- 120 PSI - 8 to 35 ---- ---- Gaiions 0 to 15 GPH - - - - ---- ---- ---- 4.5 to 5.5 in.hg. RED ARC (UPR) 2400* to2700 RPM SECTION 2 OPERATING LIMITATIONS CESSNA MODEL 182T NAV Ill WEIGHT LIMITS I Maximum Ramp Weight: . . . . . . . . . . . . . . . . . . . 3110 POUNDS Maximum Takeoff Weight: . . . . . . . . . . . . . . . . . . 3100 POUNDS Maximum Landing Weight: . . . . . . . . . . . . . . . . . 2950 POUNDS Maximum Weight in Baggage Compartment: 1 Baggage Area A - Station 82 to 109: . . . . . . . . 120 POUNDS Refer to note below. ) Baggage Area B - Station 109 to 124: . . . . . . . . 80 POUIVDS Refer to note below. ) Baggage Area C - Station 124 to 134: . . . . . . . . 80 POUNDS Refer to note below. 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-GRAVITY LIMITS Center -of -Gravity Range: Forward: 33.0 inches aft of datum at 2250 pounds or less, with straight line variation to 35.5 inches aft of datum at 2700 pounds or less, with straight line variation to 40.9 inches aft of datum at 3100 pounds, continuing to aft limit at 3100 pounds. Aft: 46.0 inches aft of datum at all weights. Reference Datum: Front face of firewall. 2 - 8 U.S. FAA APPROVED 182TPHAUS-04 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS MANEUVER LIMITS This airplane is certificated in the normal category. The normal category is applicable to aircraft intended for non aerobatic operations. These include any maneuvers incidental to normal flying, stalls (except whip stalls), lazy eights, chandelles, and turns in which the angle-of-bank is not more than 60". Aerobatic maneuvers, including spins, are not approved. FLIGHT LOAD FACTOR LIMITS Flight Load Factors (Maximum Takeoff Weight - 3100 POUNDS): ) *Flaps Up: . . . . . . . . . . . . . . . . . . . . . . . . . . . +3.8g, -1.529 *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 OPERA'TIONS LIMITS The Cessna 182T Nav Ill airplane is approved for day and night, VFR and IFR operations. Fl~ght~ntoknown-~angconditions is prohibited. The minimum equipment for approved operations required under the Operating Rules are defined by 14 CFR Part 91 and 14 CFR Part 135, as applicable. The following Kinds of Operations Equipment List (KOEL) identifies the equipment required to be operational for airplane airworthiness in the listed kind of operations. (Continued Next Page) FAA APPROVED 182TPHAUS - 04 U.S. 2-9 SECTION 2 OPERATING LIMITATIONS CESSNA MODEL 182T NAV Ill KINDS OF OPERATIONS EQUIPMENT LIST COMMENTS System, Instrument, Equipment and/or Function PLACARDS AND MARKINGS 182T Nav Ill POHIAFM Garmin G 1000TM Cockpit Reference Guide AIR CONDITIONING 1. Forward Avionics Fan 2. PFD Fan 3. MFD Fan 4. Aft Avionics Fan AUTOFLIGHT 1. BendixIKing KAP 140 POH Supplement 1 1 Accessible to pilot in flight Accessible to pilot in fliaht KIND F 0 COMMUNICATIONS 1. VHF COM ELECTRICAL POWER 1. 24V M a ~ nBattery 2. 28V Alternator 3. 24V Standby Battery 4. Main Ammeter 5. Standby Ammeter Accessible to pi!din f!ight when using autopilot Refer to Note 1 Refer to Note 1 OF v F I 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 0 0 0 NOTE 0 0 1 1 1 1 1 1 1 1 1 1 * 1 1 1 1 * 1. The European Aviation Safety Agency (EASA) requires the 24V Standby Battery and Standby Ammeter to successfully complete the pre -flight check before operating the airplane in VFR night, IFR day, or IFR night conditions in Europe. Correct operation of the 24V Standby Battery and Standby Ammeter is recommended for all other operations. OPERATION V R l R F R N R N D G D G A H A H Y T Y T 0 0 0 0 0 0 0 0 N R (Continued Next Page) I F I N R 2-10 U.S. FAA APPROVED 182TPHAUS-03 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS (Continued Next Page) (INDS OF OPERATIONS EQUIPMENT LIST (Continued) FAA APPROVED 182TPHAUS-01 System, Instrument, Equipment andlor Function EQUIPMENT AND FURNISHINGS 1. Seat Belt Assembly 2. Shoulder Harness FLIGHT CONTROLS 1. Flap Position Indicator 2. Flap Motor 3. Elevator Trim System 4. Elevator Trim Indicator 5. Rudder Trim System U.S. 2 -11 COMMENTS Each Seat Occupant Front Seat Occupants KIND OF OPERATION F y 1 1 v F I T 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 V R l R F R N R N D G D G A H A H y 1 1 I F I T 1 1 SECTION 2 OPERATING LIMITATIONS CESSNA MODEL 182T NAV Ill NOTE 1 I 2. PFD backlighting is required for day VFR flight if MFD backlighting has failed. Display backup mode must be active so engine indicators are shown. I 3. MFD backlighting is required for day VFR flight if PFD backlighting has failed. Display backup mode must be active so flight instruments are shown. KINDS OF OPERATIONS System, Instrument, Equipment and/or Function I-IGHTING 1. PFD Bezel Lighting 2. PFD Backlighting 3. MFD Bezel Lighting 4. MFD Backlighting 5. Switch and Circuit Breaker Panel Lighting 6. Airspeed lndicator (Standby) lnternal Lighting 7. Altimeter (Standby) lnternal Lighting 8. Non - stabilized Magnetic Compass lnternal Lighting 9. Attitude lndicator (Vacuum) lnternal Lighting 10. Cockpit Flood Light 11. Aircraft Position (NAV) Lights 12. STROBE Light System 13. BEACON Light 14. TAXI Light 15. LAND (Landing) Light (Continued Next Page) 2 - 12 U.S. FAA APPROVED 182TPHAUS- 04 COMMENTS 'Refer to Note 2 'Refer to Note 3 I Operations for hire onlv EQUIPMENT LIST (Continued) KIND F y * * 0 0 0 0 0 OF v F I T 0 0 0 1 1 0 0 0 1 1 0 1 0 1 1 1 0 1 0 1 1 0 1 1 1 1 1 1 1 1 OPERATION V R l R F R N R N D G D G A H A H y 1 1 0 0 0 1 0 0 0 0 0 0 0 0 0 0 I F I T 1 1 1 1 1 1 1 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS IFAA APPROVED 182TPHAUS-03 KINDS OF OPERATIONS System, Instrument, Equipment andlor Function NAVIGATION AND PITOT - STATIC SYSTEM 1. G l 000 Airspeed Indicator 2. Standby Airspeed Indicator 3. G1000 Altimeter 4. Standby Altimeter 5. G l 000 Vertical Speed lndicator 6. G1000 Attitude Indicator 7. Attitude Indicator - Vacuum (Standby) 8. G1000 Directional Indicator (HSI) 9. GI000 Turn Coordinator 10. Non - stabilized Magnetic Compass 11. VHF Navigation Radio (VORILOCIGS) 12. GPS ReceiverINavigator 13. Marker Beacon Receiver 14. Blind Altitude Encoder 15. Clock VACUUM 1. Engine -driven Vacuum Pump 2. Vacuum Indicator ENGINE FUEL AND CONTROL 1. Manifold Pressure Indicator 2. Fuel Flow Indicator ENGINE INDICATING 1. Tachometer (RPM) 2. Cylinder Head Temperature (CHT) lndicator 3. Oil Pressure Indicator 4. Oil Temperature Indicator ENGINE OIL 1. Engine Crankcase Dipstick U.S. 2-13 EQUIPMENT LIST (Continued) COMMENTS KIND F y 0 0 0 0 A/R 0 1 I F I T OF v F V R l R R N R N I D G D G A H A H T 1 1 1 1 0 0 1 1 1 1 1 1 0 0 1 1 0 0 0 0 0 0 1 1 0 0 1 1 0 0 1 1 u OPERATION F y I 1 1 1 0 0 0 A/R 0 0 1 1 0 0 0 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 A/R A/R AIR 1 1 1 A/R : I As~RequiredPer A/R A/R 1 1 1 Procedure As Required Per Procedure As Required Per Procedure As Required Per Procedure Cylinder#3 SECTION 2 OPERATING LIMITATIONS CESSNA MODEL 182T NAV Ill FUEL LIMITATIONS Total Fuel: . . . . . . . . 92.0 U.S. Gallons (46.0 gallons per tank) Usable Fuel: . . . . . . . 87.0 U.S. Gallons (43.5 gallons per tank) Unusable Fuel: . . . . . 5.0 U.S. Gallons (2.5 Gallons each tank) NOTE To ensure maximum fuel capacity and minimize cross -feeding when refueling, always park the airplane in a wings - level, normal ground attitude and place the fuel selector in the Left or Right position. Refer to Figure 1 - 1 for normal ground attitude definition. Takeoff and land with the fuel selector valve handle in the BOTH Iposition. l ~ a x i m u mslip or skid duration with one tank diy: 30 seconds. (operation on either LEFT or RIGHT tank limited to level flight only. With 114 tank or less, prolonged uncoordinated flight is prohibited when operating on either the left or the right tank. IFuel remaining in the tank after the fuel quantity indicator reads 0 (red line) cannot be safely used in flight. Approved Fuel Grades (and Colors): 100LL Grade Aviation Fuel (Blue) 100 Grade Aviation Fuel (Green) FLAP LIMITATIONS IApproved Takeoff Range: . . . . . . . . . . . . . . . . . . . . . . UP to 20" Approved Landing Range: . . . . . . . . . . . . . . . . . . . . . UP to FULL 2 - 14 U.S. FAA APPROVED 182TPHAUS-04 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS SYSTEM LIMITATIONS AUX AUDIO SYSTEM Use of the AUX AUDIO IN entertainment input is prohibited during takeoff and landing. Use of the AUX AUDIO IIV entertainment audio input and portable electronic devices~~ (PEDj sucn as celiuiar teiephones, games, cassette, CD or MP3 players is prohibited under IFR unless the operator of the airplane has determined that the use of the ~ u x ( Audio System and the connected portable electronic device(s) will not cause interference with the navigation or communication system of the airplane. 12V POWER SYSTEM The 12 Volt Power System (POWER OUTLET 12V - 10A) is not certified for supplying power to flight - critical communications or navigation devices. Use of the 12 Volt Power System is prohibited during takeoff and landing. Use of the 12 Volt Power System is prohibited under IFR unless the operator of the airplane has determined that the use of the 12 VDC( power supply and connected portable electronic device(s) will not cause interference with the navigation or communication systems of the airplane. FAA APPROVED 182TPHAUS - 04 U.S. 2- 15 SECTION 2 OPERATING I-IMITATIONS CESSNA MODEL 182T NAV Ill I The current Garmin GI000 Cockpit Reference Guide (CRG) Part Number and System Software Version that must be available to the pilot durirlg flight are displayed on the MFD AUX group, SYSTEM STATUS page. Use of the NAVIGATION MAP page for pilotage navigation is prohibited. The Navigation ~ a p is intended only to ~ enhance situational awareness. Navigation is to be conducted using only current charts, data and authorized navigation facilities. Use of the TRAFFIC MAP to maneuver the airplane to avoid traffic is prohibited. The Traffic Information System (TIS) is intended for advisory use only. TIS is intended only to help the pilot to visually locate traffic. It is the responsibility of the pilot to see and maneuver to avoid traffic. Use of the TERRAIN PROXIMITY information for primary terrain avoidance is prohibited. The Terrain Proximity map is intended only to enhance situational awareness. It is the pilot's responsibility to Iprovide terrain clearance at all times. Navigation using the GI000 is not authorized north of 70 " North latitude or south of 70 " South latitude due t o uns~uitabiiityoi the magnetic fields near the Earth's poles. In addition, operations are not authorized in the following two regions: 1. North of 65 " North latitude between longitude 75 " W and 120" W (Northern Canada). 2. South of 55" South latitude between longitude 120" E and 165" E (region south of Australia aria iiew Zeaianaj. The COM 112 (split COM) function of the GMA 1347 Audio Panel is not approved for use. During COM 112 operation, transmission by one crew member inhibits reception by the other crew member. (BENDIWKING KAP 140 2 AXIS AUTOPILOT IUse of the BendixIKing KAP 140 Autopilot is prohibited when the GMA 1347 Audio Panel is inoperative (since the aural warning will not be provided when Autopilot is disengaged). 2 - 16 U.S. FAA APPROVED 182TPHAUS- 04 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS L3 COMMUNICATIONS WX 500 STORMSCOPE (if installed) Use of the WEATHER MAP (WX -500 Stormscope) for hazard01 weather (thunderstorm) penetration is prohibited. LTNG informatic on the NAVIGATION MAP or WEATHER MAP is approved only , an aid to hazardous weather avoidance, not penetration. TRAFFIC ADVISORY SYSTEM (TAS) (if installed) Use of the TRAFFIC MAP to maneuver the airplane to avoid traf is prohibited. The Traffic Advisory System (TAS) is intended 1 advisory use only. TAS is intended only to help the pilot to visua locate traffic. It is the responsibility of the pilot to see and maneuv to avoid traffic. TERRAIN AWARENESS AND WARNING SYSTEM (TAWS-B) (if installed) Use of the Terrain Awareness and Warning System (TAWS-B) navigate to avoid terrain or obstacles is prohibited. TAWS-B is or approved as an aid to help the pilot to see -and-avoid terrain obstacles. TAWS -B must be inhibited when landing at a location not includ~ in the airport database. Use of TAWS-B is prohibited when operating using the Q f altimeter setting (altimeter indicates 0 feet altitude when the airpla~ is on the runway). The pilot is authorized to deviate from the current ATC clearant only to the extent necessary to comply with TAWS - B warnings. The geographic area of the TAWS -B database must match tl geographic area in which the airplane is being operated. IFAA APPROVED 182TPHAUS -04 U.S. 2 - 17 SECTION 2 OPERATING LIMITATIONS CESSNA MODEL 182T NAV III PLACARDS The following information must be displayed in the form of composite or individual placards. 1. In full view of the pilot: (The " DAY- NIGHT -VFR-IFR " entry, shown on the example below, will vary with installed equipment). The markings and placards installed in this airplane contain operating limitations which must 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 Operating Handbook and FAA Approved Airplane Flight Manual. No acrobatic maneuvers, including spins, approved. Flight into known icing conditions prohibited. This airplane is certified for the following flight operations as of date of original airworthiness certificate: DAY-NIGHT-VFR-IFR 2. On control lock: CAUTION! CONTROL LOCK REMOVE BEFORE STARTING ENGINE (Continued Next Page) FAA APPROVED 182TPHAUS-04 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS PLACARDS (Continued) 3. On the fuel selector valve: BOTH 87.0 GAL. TAKEOFF LANDING ALL FLIGHT ATTITUDES FUEL SELECTOR PUSH DOWN ROTATE LEFT RIGHT 43.5 GAL. 43.5 GAL. LEVEL FLIGHT ONLY LEVEL FLIGHT ONLY OFF 4. Near both fuel tank filler caps: FUEL 100LU100 MIN. GRADE AVIATION GASOLINE CAP. 43.5 U.S. GAL. USABLE CAP. 32.0 U.S. GAL. USABLE TO BOTTOM OF FILLER INDICATOR TAB (Continued Next Page) IFAA APPROVED 182TPHAUS - 04 U.S. 2 -19 SECTION 2 OPERATING LIMITATIONS CESSNA MODEL 182T NAV Ill PLACARDS (Continued) 5. On flap control indicator: LIP to 10" 140 KlAS (Initial flap range with Dark Blue color code; mechanical detent at 10 " position) 10 " to 20 " 120 KlAS (Intermediate flap range with Light Blue color code; mechanical detent at 20 " position) 20" to FULL 100 KIAS (Full flap range with White color code; mechanical stop at FULL position) 6. In baggage compartment: 120 POUNDS MAXIMUM BAGGAGE FORWARD OF BAGGAGE DOOR LATCH AND 80 POUNDS MAXIMUM BAGGAGE AFT OF BAGGAGE 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 30 " increments. 8. On the oil filler cap: OIL 9 QTS 1 9. Above the PFD: I MANEUVERING SPEED - 110 KlAS I(Continued Next Page) 12 - 20 U.S. FAA APPROVED 182TPHAUS- 04 CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS PLACARDS (Continued) 10. On the upper right instrument panel: I SMOKING PROHIBITED 11. On auxiliary power plug door and second placard on battery box: CAUTION 24 VOLTS D.C. THlS AIRCRAFT IS EQUIPPED WITH ALTERNATOR AND A NEGATIVE GROLIND SYSTEM. OBSERVE PROPER POLARITY. REVERSE POLARITY 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 91.207 13. Near the center overhead light control: Flood Light IFAA APPROVED 182TPHAUS -04 U.S. 2- 21/2- 22 CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES EMERGENCY PROCEDURES TABLE OF CONTENTS I Page Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 5 Airspeeds For Emergency Operations . . . . . . . . . . . . . . . . . . 3 - d EMERGENCY PROCEDURES . . . . . . . . . . . . . . . . . . 3-6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGINE FAILURES 3-6 . . . . . . . . . . . . . . . . . . Engine Failure During Takeoff Roll 3 - 6 . . . . . . . . . . . . . . Engine Failure Immediately After Takeoff 3 - 6 . . . . . . . Engine Failure During Flight (Restart Procedures) 3 - 6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORCED LANDINGS 3 - 7 Emergency Landing Without Engine Power . . . . . . . . . . . . 3 - 7 Precautionary Landing With Engine Power . . . . . . . . . . . . 3-8 Ditching . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-8 FIRES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 9 . . . . . . . . . . . . . . . . . . . . . . . . . . During Start On Ground 3 - 9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Fire In Flight 3-10 . . . . . . . . . . . . . . . . . . . . . . . . . . Electrical Fire In Flight 3 -10 CabinFire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 11 Wing Fire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 11 ICING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 12 . . . . . . . . . . . . . Inadvertent Icing Encounter During Flight 3-121 Static Source Blockage (Erroneous Instrument Reading Suspected) . . . . . . . . . 3-13 (Continued Next Page) I U.S. 3 - 1 SECTION 3 EMERGENCY PROCEDURES CESSIVA MODEL 182T NAV Ill TABLE OF CONTENTS (Continued) Page . . . . . . . . . . . . . . . . . . . . . . . . . IEXCESSIVE FUEL VAPOR 3 - 13 Fuel Flow Stabilization Procedures . . . . . . . . . . . . . . . . . 3 - 13 ABNORMAL LANDINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 14 . . . . . . . . . . . . . . . . . . . . . Landing With A Flat Main Tire 3 - 14 . . . . . . . . . . . . . . . . . . . . . Landing With A Flat Nose Tire 3 - 14 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS 3-15 ( High Volts Annunciator Comes On or M BAT AMPS More Than 40 . . . . . . . . . . . . . . . . . . . . 3 - 15 LOW VOLTS Annunciator Comes On Below 1000 RPM . . 3-17 LOW VOLTS Annunciator Comes On or . . . . . . . . . . . . . . . . . . Does Not Go Off at Higher RPM 3 - 17 AIR DATA SYSTEM FAILURE . . . . . . . . . . . . . . . . . . . . . . 3 - 19 . . . . . . . . . . . . . . . . . . . . Red X . PFD Airspeed Indicator 3-19 . . . . . . . . . . . . . . . . . . . . . Red X . PFD Altitude Indicator 3 -19 AlTITLIDE AND HEADING REFERENCE SYSTEM (AHRS) FAILURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-20 . . . . . . . . . . . . . . . . . . . . . Red X . PFD Attitude Indicator 3 -20 . . . . . . . . . . . Red X . Horizontal Situation Indicator (HSI) 3-20 . . . . . . . . . . . . . . . . . . . . . DISPLAY COOLING ADVISORY 3 - 20 . . . . PFD1 COOLING or MFD1 COOLING Annunciator(s) 3 - 20 VACUUM SYSTEM FAILURE . . . . . . . . LOW VACUUM Annunciator Comes On I . . . . . . . . . . . . . . HlGH CARBON MONOXIDE (CO) LEVEL ANNUNCIATOR . 3-21 CO LVL HIGH Annunciator Comes On 3 -21 . . . . . . . . . . . . . CO LVL HIGH Annunciator Remains On 3 -21 (Continued Next Page) 3 - 2 U.S. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS (Continued) Page AMPLIFIED EMERGENCY PROCEDLIRES . . . . . . . . . . . . . Engine Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Glide Forced Landings -. ;. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing Without Elevator Control . . . . . . . . . . . . . . . . . . . . . Fires . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Emergency Operation In Clouds Executing A 180" Turn In Clouds (AHRS FAILED) . . . . . . Emergency Descent Through Clouds (AHRS FAILED) . . . Recovery From Spiral Dive In The Clouds (AHRS FAILED) . . . . . . . . . . . . . . . . . Inadvertent Flight Into Icing Conditions Static Source Blocked . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Spins . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rough Engine Operation Or Loss Of Power . . . . . . . . . . . . . Spark Plug Fouling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Magneto Malfunction . . . . . . . . . . . . . . . . . . Engine -Driven Fuel Pump Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . Excessive Fuel Vapor Low Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Electrical Power Supply System Malfunctions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Excessive Rate-Of-Charge Insufficient Rate - Of- Charge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . High Carbon Monoxide (CO) Level Annunciation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Other Emergencies Windshield Damage . . . . . . . . . . . . . . . . . . . . . . . . . . . . U.S. 3-3/3-4 CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES INTRODUCTION Section 3 provides checklist and amplified procedures for coping with emergencies that may occur. Emergencies caused by airplane or engine malfunctions are extremely rare if proper preflight inspections and maintenance are practiced. Enroute weather emergencies can be minimized or eliminated by careful flight planning and 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 problem. In any situation, the most important task is continued control of the airplan and maneuver to execute a successful landing. Emergency procedures associated with optional or supplemental equipment are found in Section 9, Supplements. AIRSPEEDS FOR EMERGENCY OPERATIONS I ENGINE FAILURE AFTER TAKEOFF Wing Flaps UP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 KlAS Wing Flaps 10" - FULL . . . . . . . . . . . . . . . . . . . . . . . 70 KIAS( MANEUVERING SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3100 POUIVDS 110 KlAS 2600POLlNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101KlAS 2100 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 91 KlASIMAXIMUM GI-IDE 3100 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 76 KlAS 2600 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KlAS 2100 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58 KlASIPRECAUTIONARY LANDING WITH ENGINE POWER . 70 KlAS LANDING WITHOUT ENGINE POWER Wing Flaps UP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 KlAS . . . . . . . . . . . . . . . . . . . . . . . Wing Flaps 10" - FULL 70 K I A S ~ U.S. 3 - 5 SECTION 3 EMERGENCY PROCEDURES CESSIVA MODEL 182T NAV Ill EMERGENCY PROCEDURES Procedures in the Emergency Procedures Checklist portion of this section shown in bold faced type are immediate action items which should be committed to memory. ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF ROLL 1. Throttle Control - IDLE (pull full out) 2. Brakes - APPLY 3. Wing Flaps - RETRACT 4. Mixture Control - IDLE CUTOFF (pull full out) 5. MAGNETOS Switch - OFF 6. STBY BATT Switch - OFF 7. MASTER Switch (ALT and BAT) - OFF ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF 1. Airspeed - 75 KlAS - Flaps UP 70 KlAS - Flaps 10" - FULL 2. Mixture Control - IDLE CUTOFF (pull full out) 3. FUEL SELECTOR Valve - PUSH DOWN and ROTATE to OFF 4. MAGNETOS Switch - OFF 5. Wing Flaps - AS REQUIRED (FULL recommended) 6. STBY BATT Switch - OFF 7. MASTER Switch (ALT and BAT) - OFF 8. Cabin Door - UNLATCH 9. Land - STRAIGHT AHEAD ENGINE FAILURE DURING FLIGHT (Restart Procedures) 1. Airspeed - 76 KlAS (best glide speed) 2. FUEL SELECTOR Valve - BOTH 3. FUEL PUMP Switch - ON 4. Mixture Control - RICH (if restart has not occurred) (Continued Next Page) 13 - 6 U.S. CESSNA MODEL 182T NAV Ill SECTION 3 ENIERGENCY PROCEDURES ENGINE FAILURES (Continued) ENGINE FAILURE DURING FLIGHT (Restart Procedures) (Continued) 5. MAGNETOS Switch - BOTH (or START if propeller is stopped) NOTE If propeller is windmilling, engine will restart automatically within a few seconds. If propeller has stopped (possible at low speeds), turn MAGNETOS switch to START, advance throttle slowly from idle and lean the mixture from full rich as required to obtain smooth operation. 6. FUEL PUMP Switch - OFF NOTE If the indicated fuel flow (FFLOW GPH) immediately drops to zero, a sign of failure of the engine - driven fuel pump, return the FUEL PUMP Switch to the ON position. FORCED LANDINGS EMERGENCY LANDING WITHOUT ENGINE POWER 1. Pilot and Passenger Seat Backs - MOST UPRIGHT[ PoSI1-IOIV 2. Seats and Seat Belts - SECURE 3. Airspeed - 75 KlAS - Flaps UP 70 KlAS - Flaps 10" - FULL 4. Mixture Control - IDLE CUTOFF (pull full out) 5. FUEL SELECTOR Valve - PUSH DOWN and ROTATE toI OFF 6. MAGNETOS Switch - OFF 7. Wing Flaps - AS REQUIRED (FULL recommended) 8. STBY BATT Switch - OFF 9. MASTER Switch (ALT and BAT) - OFF (when landing is assured) 10. Doors - UNLATCH PRIOR TO TOUCHDOWN 11. Touchdown - SLIGHTLY TAIL LOW 12. Brakes - APPLY HEAVILY (Continued Next Page) U.S. 3-7 SECTION 3 EMERGENCY PROCEDLIRES CESSNA MODEL 182T NAV Ill FORCED LANDINGS (Continued) PRECAUTIONARY LANDING WITH ENGINE POWER I 1. Pilot and Passenger Seat Backs - MOST UPRIGHT POSITION 2. Seats and Seat Belts - SECURE 3. Airspeed - 75 KlAS 4. Wing Flaps - 20 " 5. Selected Field - FLY OVER, noting terrain and obstructions. 6. Wing Flaps - FULL (on final approach) 7. Airspeed - 70 KlAS 8. STBY BATT Switch - OFF 9. MASTER Switch (ALT and BAT) - OFF (when landing I assured) 10. Doors - LINLATCH PRIOR TO TOUCHDOWN 11. Touchdown - SLIGHTLY TAIL LOW 1 12. Mixture Control - IDLE CUTOFF (pull full out) 13. MAGNETOS Switch - OFF 14. Brakes - APPLY HEAVILY DITCHING 1. Radio - TRANSMIT MAYDAY on 121.5 MHz, (Give location, I intentions and SQUAWK 7700) 2. Heavy Objects (in baggage area) - SECURE OR JETI-ISON (if possible) ) 3. Pilot and Passenger Seat Backs - MOST UPRIGHT POSI-TION 4. Seats and Seat Belts - SECLIRE 5. Wing Flaps - 20" - FULL 6. Power - ESTABLISH 300 FTIMIW DESCENT AT 65 KlAS NOTE If no power is available, approach at 70 KlAS with Flaps UP or at 65 KlAS with Flaps 10" . 7. Approach - High Winds, Heavy Seas - INTO THE WIND Light Winds, Heavy Swells - PARALLEL TO SWELLS 8. Cabin Doors - UNLATCH 9. Touchdown - LEVEL ATTITUDE AT ESTABLISi4ED RATE- OF-DESCENT. (Continued Next Page) 3 - 8 U.S. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES FORCED LANDINGS (Continued) DITCHING (Continued) 10. Face - CUSHION at touchdown with folded coat 11. ELT - ACTIVATE 12. Airplane - EVACUATE THROUGH CABIN DOORS. 111 necessary, open window and flood cabin to equalize pressure so doors can be opened. 13. Life Vests and Raft - INFLATE WHEN CLEAR OF AIRPLANE FIRES DURING START ON GROUND 1. MAGNETOS Switch - START (continue cranking to start the engine) IF ENGINE STARTS 2. Power - 1800 RPM for a few minutes 3. Engine - SHUTDOWN and inspect for damage I IF ENGINE FAILS TO START 2. Throttle Control - FULL (push full in) 3. Mixture Control - IDLE CUTOFF (pull full out) 4. MAGNETOS Switch - START (continue cranking) 5. FUEL SELECTOR Valve - PUSH DOWN and ROTATE to I OFF 6. FUEL PUMP Switch - OFF 7. MAGNETOS Switch - OFF 8. STBY BATT Switch - OFF 9. MASTER Switch (ALT and BAT) - OFF 10. Engine - SECURE 11. Parking Brake - RELEASE 12. Fire Extinguisher - OBTAIN (have ground attendants obtain if not installed) 13. Airplane - EVACUATE 14. Fire - EXTINGUISH using fire extinguisher, wool blanket, or dirt. 15. Fire Damage - INSPECT (Repair or replace damaged components and/or wiring before conducting another flight) I (Continued Next Page) 182TPHAUS- 04 U.S. 3 - 9 SECTION 3 EMERGENCY PROCEDLIRES CESSIVA MODEL 182T NAV Ill FIRES (Continued) ENGINE FlRE IN FLIGHT 1 1. Mixture Control - IDLE CUTOFF (pull full out) 2. FLlEL SELECTOR Valve - PUSH DOWN and ROTATE t o OFF 3. FUEL PUMP Switch - OFF I 4. MASTER Switch (ALT and BAT) - OFF 5. Cabin Heat and Air - OFF (except overhead vents) 6. Airspeed - 100 KIAS. (If fire is not extinguished, increase glide speed to find an airspeed, within airspeed limitations, which will provide an incombustible mixture) 1 7. Forced Landing - EXECUTE, Refer to EFAERGEr\!CY LANDING WITHOUT ENGINE POWER ELECTRICAL FlRE IN FLIGHT 1. STBY BATT Switch - OFF 2. MASTER Switch (ALT and BAT) - OFF 3. VentsICabin AirIHeat - CLOSED 4. Fire Extinguisher - ACTIVATE (if available) 5. AVIONICS Switch (BUS 1 and BUS 2) - OFF 6. All Other Switches (except MAGNETOS switch) - OFF WARNING AFTER THE FlRE EXTINGUISHER HAS BEEN USED, MAKE SURE THAT THE FlRE IS EXTlNGLllSHED BEFORE EXTERIOR AIR IS USED TO REMOVE SMOKE FROM THE CABIN. 7. VentsICabin AirIHeat - OPEN (When sure that fire is completely extinguished) (Continued Next Page) 3 - 10 U.S. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES FIRES (Continued) ELECTRICAL FlRE IN FLIGHT (Continued) IF FlRE HAS BEEN EXTINGUISHED AND ELECTRICAL POWER IS NECESSARY FOR CONTINUED FLIGHT TO NEAREST SUITABLE AIRPORT OR LANDING AREA 8. Circuit Breakers - CHECK for OPEN circuit(s), do not reset. 9. MASTER Switch (ALT and BAT) - ON 10. STBY BATT Switch - ON 11. AVlOhllCS Switch (BUS 1) - ON 12. AVIONICS Switch (BUS 2) - ON ICABIN FlRE 1. STBY BATT Switch - OFF 2. MASTER Switch (ALT and BAT) - OFF 3. Ventstcabin AirIHeat - CLOSED (to avoid drafts) 4. Fire Extinguisher - ACTIVATE (if available) WARNING AFTER THE FlRE EXTINGUISHER HAS BEEN USED, MAKE SURE THAT THE FlRE IS EXTlNGLllSHED BEFORE EXTERIOR AIR IS USED TO REMOVE SMOKE FROM THE CABIN. 5. VentsICabin AirIHeat - OPEN (When sure that fire is completely extinguished) 6. Land the airplane as soon as possible to inspect for damage. I WING FlRE 1. LAND and TAXI Light Switches - OFF 2. NAV Light Switch - OFF 3. STROBE Light Switch - OFF 4. PlTOT HEAT Switch - OFF NOTE Perform a sideslip to keep the flames away from the fuel tank and cabin. Land as soon as possible using flaps only as required for final approach and touchdown. 182TPHAUS-04 U.S. 3 - 11 SECTION 3 EMERGENCY PROCEDURES CESSIVA MODEL 182T NAV Ill INADVERTENT ICING ENCOUNTER DURING FLIGHT 1. PlTOT HEAT Switch - ON 2. Turn back or change altitude to obtain an outside air temperature that is less conducive to icing. 3. Pull cabin heat control full out and rotate defroster control clockwise to obtain maximum defroster airflow. 4. Increase engine speed to minimize ice build - up on propeller blades. If excessive vibration is noted, momentarily reduce engine speed to 2200 RPM with the propeller control, and then rapidly move the control forward. NOTE Cycling the RPM flexes the propeller blades and high RPM increases centrifugal force, causing ice to shed more rapidly. Watch for signs of induction air filter icing. A loss of manifold pressure could be caused by ice blocking the air intake filter. Adjust the throttle as necessary to hold manifold pressure. Adjust mixture, as necessary, for any change in power settings. Plan a landing at the nearest airport. With an extremely rapid ice build -up, select a suitable " off airport " landing site. With an ice accumulation of 0.25 inch or more on the wing leading edges, be prepared for significantly higher power requirements, higher approach and stall speeds, and a longer landing roll. Leave wing flaps retracted. With a severe ice build-up on the horizontal tail, the change in wing wake airflow direction caused by wing flap extension could result in a loss of elevator effectiveness. Open left window and, if practical, scrape ice from a portion of the windshield for visibility in the landing approach. Perform a landing approach using a forward slip, if necessary, for improved visibility. Approach at 80 to 90 KlAS depending upon the amount of the ice accumulation. Perform a landing in level attitude. Missed approaches should be avoided whenever possible because of severely reduced climb capability. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES ICING (Continued) STATIC SOURCE BLOCKAGE (ERRONEOUS INSTRUMENT READING SUSPECTED) 1. ALT STATIC AIR Valve - PULL ON 2. CABIN HT and CABIN AIR Knobs - PULL ON 3. Vents - CLOSED 4. Airspeed - Refer to Section 5, Figure 5 - 1 (Sheet 2) Airspeed Calibration, Alternate Static Source correction chart. 5. Altitude - Refer to Section 5, Figure 5 -2, Altimeter Correction, Alternate Static Source correction chart. IEXCESSIVE FUEL VAPOR FUEL FLOW STABILIZATION PROCEDURES (If flow fluctuations of 1 GPH or more, or power surges occur.) 1. FUEL PUMP Switch - ON 2. Mixture Control - ADJUST (As necessary for smooth enginel operation) 3. Fuel Selector Valve - SELECT OPPOSITE TANK (if vapor symptoms continue) 4. FUEL PUMP Switch - OFF (after fuel flow has stabilized) U.S. 3- 13 SECTION 3 EMERGENCY PROCEDURES CESSNA MODEL 182T NAV Ill ABNORMAL LANDINGS LANDING WlTH A FLAT MAlN TIRE 1. Approach - NORMAL 2. Wing Flaps - FULL 3. Touchdown - GOOD MAlN TIRE FIRST (Hold airplane off flat tire as long as possible with aileron control) 4. Directional Control - MAINTAIN (Using brake on good wheel as required) LANDING WlTH A FLAT NOSE 'TIRE 1. Approach - NORMAL 2. Wing Flaps - AS REQUIRED 120 to 140 KlAS - Flaps Up - 10" 100 to 120 KlAS - Flaps 10" - 20" Below 100 KlAS - Flaps FULL 3. Touchdown - ON MAINS (Hold nosewheel off the ground as long as possible) 4. When nosewheel touches down, maintain full up elevator as airplane slows to stop. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS HIGH VOLTS ANNUNCIATOR COMES ON OR M BAT AMPS MORE THAN 40 I 1. MASTER Switch (ALT Only) - OFF 2. Electrical Load - REDUCE IMMEDIATELY as follows: a. AVIONICS Switch (BUS 1) - OFF b. PlTOT HEAT - OFF I c. BEACON Light - OFF d. LAND Light - OFF (Use as required for landing) e. TAXI Light - OFF f. NAV Lights - OFF g. STROBE Lights - OFF h. CABllV PWR 12V - OFF NOTE The Main Battery supplies electrical power to the Main and Essential Buses until M BUS VOLTS decreases below 20 volts. When M BUS VOLTS falls below 20 volts, the Standby Battery System will automatically supply electrical power to the Essential Bus for at least 30 minutes. Select COMl MIC and NAVl on the audio panel and tune to the active frequency before setting AVIONICS BUS 2 to OFF. If COM2 MIC and NAV2 are selected when AVIONICS BUS 2 is set to off, the COM and NAV radios cannot be tuned. (Continued Next Page) U.S. 3 - 15 SECTION 3 EMERGENCY PROCEDURES CESSNA MODEL 182T NAV Ill ELEC'TRICAC P O W E R SUPPLY SYSTEM MALFUNC'TIONS (Continued) [HIGH V OLTS ANNUNCIATOR COMES ON OR M B A T AM PS MORE THAN 40 (Continued) I i. COM1 and NAVl - TUNE TO ACTIVE FREQUENCY I j. COM1 MIC and NAV1 - SELECT (COM2 MIC and NAV2 will be inoperative once AVIONICS BUS 2 is selected to OFF). NOTE When AVIONICS BUS 2 is set to OFF, the following items will not operate: KAP 140 Autopilot GMA 1347 Audio Panel COMM 2 NAV 2 GTX 33 Transponder GDU 1040 MFD I k. AVIONICS Switch (BUS 2) - OFF (KEEP ON if in clouds) 3. Land as soon as practical. NOTE Make sure a successful landing is possible before extending flaps. The flap motor is a large electrical load during operation. (Continued Next Page) 3 - 16 U.S. CESSNA MODEL 182T NAV III SECTION 3 EMERGENCY PROCEDURES ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS (Continued) LOW VOLTS ANNUNCIATOR COMES ON BELOW 1000 RPM 1. Throttle Control - 1000 RPM 2. Low Voltage Annunciator (LOW VOLTS) - CHECK OFF LOW VOLTS ANNUNCIATOR REMAINS ON AT 1000 RPM 3. Authorized maintenance personnel must do electrical system inspection prior to next flight. LOW VOLTS ANNLINCIATOR COMES ON OR DOES NOT GO OFF AT HIGHER RPM 1. MASTER Switch (ALT Only) - OFF 2. Alternator Circuit Breaker (ALT FIELD) - CHECK IN 3. MASTER Switch (ALT and BAT) - ON 4. Low Voltage Annunciator (LOW VOLTS) - CHECK OFF 5. M BUS VOLTS - CHECK 27.5 V minimum 6. M BAT AMPS - CHECK CHARGING (+) IF LOW VOLTS ANNUNCIATOR REMAINS ON 7. MASTER Switch (ALT Only) - OFF 8. Electrical Load - REDUCE IMMEDIATELY as follows: a. AVlOlVlCS Switch (BUS 1) - OFF I b. PITOT HEAT - OFF c. BEACON Light - OFF d. LAND Light - OFF (use as required for landing) e. TAXI Light - OFF f. NAV Lights - OFF g. STROBE Lights - OFF h. CABIN PWR 12V - OFF (Continued Next Page) U.S. 3 - 17 SECTION 3 EMERGENCY PROCEDURES CESSIVA MODEL 182T NAV Ill ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS (Continued) IF LOW VOLTS ANNUNCIATOR REMAINS ON (Continued) NOTE The Main Battery supplies electrical power to the Main and Essential Buses until M BUS VOLTS decreases below 20 volts. When M BUS VOLTS falls below 20 volts, the Standby Battery System will automatically supply electrical power to the Essential Bus for at least 30 minutes. Select COM1 MIC and NAV1 on the audio panel and tune to the active frequency before setting AVIONICS BUS 2 to OFF. If COM2 MIC and NAV2 are selected when AVIONICS BUS 2 is set to OFF, the COM and NAV radios cannot be tuned. i. COMI and NAV1 - TUNE TO ACTIVE FREQUEIVCY i. COM1 MIC and NAV1 - SELECT (COM2 MIC and NAV2 will be inoperative once AVlOlVlCS BUS 2 is selected to OFF) NOTE When AVIONICS BUS 2 is set to OFF, the following items will not operate: KAP 140 Autopilot GMA 1347 Audio Panel COMM 2 NAV 2 GTX 33 Transponder GDU 1040 MFD k. AVIONICS Switch (BUS 2) - OFF (KEEP ON if in clouds) 1 (Continued Next Page) 13 - 18 U.S. CESSNA MODEL 182T NAV Ill SECTION 3 ENIERGENCY PROCEDURES ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS (Continued) IF LOW VOLTS ANNUNCIATOR REMAINS ON (Continued) 9. Land as soon as practical. NOTE Make sure a successful landing is possible before extending flaps. The flap motor is a large electrical load during operation. AIR DATA SYSTEM FAILURE RED X - PFD AIRSPEED INDICATOR 1. ADCIAHRS Circuit Breakers - CHECK IN (ESS BUS and AVN BUS 1). If open, reset (close) circuit breaker. If circuit breaker opens again, do not reset. 2. Standby Airspeed Indicator - USE FOR AIRSPEED INFORMATION RED X - PFD ALTITUDE INDICATOR 1. ADCIAHRS Circuit Breakers - CHECK IN (ESS BUS and AVN BUS 1). If open, reset (close) circuit breaker. If circuit breaker opens again, do not reset. 2. Standby Altimeter - CHECK current barometric pressure SET. USE FOR ALTITUDE INFORMATION U.S. 3 - 19 SECTION 3 EMERGENCY PROCEDLIRES CESSIVA MODEL 182T NAV Ill ATTITUDE AND HEADING REFERENCE SYSTEM (AHRS) FAILURE RED X - PFD ATTITUDE INDICATOR 1. ADCIAHRS Circuit Breakers - CHECK IN (ESS BUS and AVN BUS 1). If open, reset (close) circuit breaker. If circuit breaker opens again, do not reset. 2. Standby Attitude Indicator - USE FOR ATTI-TUDE INFORMATION RED X - HORIZONTAL SITUATION INDICATOR (HSI) 1. ADCIAHRS Circuit Breakers - CHECK IN (ESS BUS and AVhl BUS 1). If open, reset (close) circuit breaker. If circuit breaker opens again, do not reset. 2. Non - Stabilized Magnetic Compass - USE FOR HEADING INFORMATION DISPLAY COOLING ADVISORY PFD1 COOLING OR MFDl COOLING ANNUNCIATOR(S) 1. Cabin Heat (CABIN HT) - REDUCE (minimum preferred) 2. Forward Avionics Fan - CHECK (feel for airflow from screen on glareshield) IF FORWARD AVIONICS FAN HAS FAILED 3. STBY BATT Switch - OFF (unless needed for emergency power) IF PFD1 COOLING OR MFDl COOLING ANNLINCIATOR DOES NOT GO OFF WITHIN 3 MINUTES OR IF BOTH PFD1 COOLING AND MFDl COOLING ANNUNCIATORS COME ON 3. STBY BATT Switch - OFF (land as soon as practical) CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES VACUUM SYSTEM FAILURE LOW VACUUM ANNLINCIATOR COMES ON 1. Vacuum Indicator (VAC) - CHECK EIS SYSTEM page to make sure vacuum pointer is in green arc limits. CAUTION IF VACUUM POINTER IS OUT OF THE GREEN ARC DURING FLIGHT OR THE GYRO FLAG IS SHOWN ON THE STANDBY ATTITUDE INDICATOR, THE STANDBY ATTITUDE INDICATOR MUST NOT BE - -USED F O R ATTITUDE INFORMATION. HlGH CARBON MONOXIDE ANNUNCIATOR (if installed) LEVELlCO LVL HlGH ANNUNCIATOR COMES ON I1. CABIN HT Knob - OFF (push full in) 2. CABIN AIR Knob - ON (pull full out) 3. Cabin Vents - OPEN 4. Cabin Windows - OPEN (175 KlAS maximum windows open speed) ICO LVL HlGH ANNUNCIATOR REMAINS ON I5. Land as soon as practical. I U.S. 3-21 SECTION 3 EMERGENCY PROCEDURES CESSNA MODEL 182T NAV Ill AMPLIFIED EMERGENCY PROCEDURES IThe following Amplified Emergency Procedures provide additional information beyond that in the Emergency Procedures Checklists portion of this section. These procedures also include information not readily adaptable to a checklist format, and material to which a pilot could not be expected to refer in resolution of a specific emergency. This information should be reviewed in detail prior to flying the airplane, as well as reviewed on a regular basis to keep pilot's knowledge of procedures fresh. ENGINE FAILURE If an engine failure occurs during the takeoff roll, stop the airplane on the remaining runway. Those extra items on the check!ist wi!! provide added safety after a failure of this type. [If an engine failure occurs immediately after takeoff, in most cases, the landing should be planned straight ahead with only small changes in direction to avoid obstructions. Altitude and airspeed are seldom sufficient to execute the 180" gliding turn 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 most important task is to continue flying the airplane. The best glide speed, 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 engine restart should be attempted as shown in the checklist. If the engine cannot be restarted, a forced landing without power must be completed. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES MAXIMUM GLIDE Ground Distance - Nautical Miles Figure 3-1 U.S. 3-23 SECTION 3 EMERGENCY PROCEDURES CESSNA MODEL 182T NAV Ill FORCED LANDINGS If all attempts to restart the engine fail and a forced landing is imminent, select a suitable field and prepare for the landing as discussed under the Emergency Landing Without Engine Power checklist. Transmit Mayday message on 121.5 MHz giving location and intentions and squawk 7700. Before attempting an " off-airport " landing with engine power available, one should fly over the landing area at a safe, but low altitude, to inspect the terrain for obstructions and surface conditions, proceeding as discussed in the Precautionary Landing With Engine Power checklist. Prepare for ditching by securing or jettisoning heavy objects located in the baggage area and collect folded coats for protection of occupants' face at touchdown. Transmit Mayday messages on 121.5 MHz giving location and intentions and squawk 7700. Avoid a landing flare because of the difficulty in judging height over a water surface. The checklist assumes the availability of power to make a precautionary water landing. If power is not available, use of the airspeeds noted with minimum flap extension will provide a more favorable attitude for a power off ditching. In a forced landing situation, do not turn off the AVIONICS switch or MASTER switch until a landing is assured. Premature deactivation of the switches will disable all airplane electrical systems. Before completing a forced landing, especially in remote and mountainous areas, activate the ELT by setting the cockpit -mounted switch to the ON position. For complete information on ELT operation, refer to Section 9, Supplements. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES LANDING WITHOUT ELEVATOR CONTROL Trim for horizontal flight with an airspeed of approximately 80 KlAS by using throttle and elevator trim controls. Then do not change the elevator trim control setting; control the glide angle by adjusting power. During the landing flare (round -out), the nose will come down when power is reduced and the airplane may touch down on the nosewheel before the main wheels. When in the flare, the elevator trim control should be adjusted toward the full nose up position and the power adjusted at the same time so that the airplane will rotate to a horizontal attitude for touchdown. Close the throttle at touchdown. FIRES Improper starting procedures involving the excessive use of auxiliary fuel pump operation can cause engine flooding and subsequent collection of fuel on the parking ramp as the excess fuel drains overboard from the intake manifolds. This is sometimes experienced in difficult starts in cold weather where engine preheat service is not available. If this occurs, the airplane should be pushed away from the fuel puddle before another engine start is attempted. Otherwise, there is a possibility of raw fuel accumulations in the exhaust system igniting during an engine start, causing a long flame from the tailpipe, and possibly igniting the collected fuel on the pavement. If a fire occurs, proceed according to the checklist. Although engine fires are extremely rare in flight, if a fire is encountered, the steps of the appropriate checklist should be followed. After completion of the checklist procedure, execute a forced landing. Do not attempt to restart the engine. 'The first sign of an electrical fire is usually the smell of burning insulation. The checklist procedure should result in the elimination of the fire. U.S. 3- 25 SECTION 3 EMERGENCY PROCEDURES CESSNA MODEL 182T NAV Ill [EMERGENCY OPERATION IN CLOUDS If the engine -driven vacuum pump fails in flight, the standby attitude indicator will not be accurate. The pilot must then rely on the attitude and heading information (from the AHRS) shown on the PFD indicators. With valid HDG or GPSINAV and blind turn coordinator inputs, autopilot operation will not be affected. If the AHRS unit fails in flight (red X's shown through the PFD attitude and heading indicators), the pilot must rely on the standby attitude indicator and non - stabilized magnetic compass for attitude and heading information. The autopilot will not operate in HDG mode without AHRS input. With a valid GPS or NAV input and a good blind turn coordinator, the autopilot will operate in NAV, APR or REV modes. Autopilot altitude hold and vertical speed operating modes are independent of AHRS operation. Refer to Section 9, Supplements, for additional details on autopilot operations. The following instructions assume that the pilot is not very proficient at instrument flying and is flying the airplane without the autopilot engaged. (Continued Next Page) 3-26 U.S. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES EMERGENCY OPERATION IN CLOUDS (Continued) 1 EXECUTING A 180" TURN IN CLOUDS (AHRS FAILED) Upon inadvertently entering the clouds, an immediate turn to reverse course and return to VFR conditions should be made as follows: AHRS Failure 1. Note the non-stabilized magnetic compass heading. 2. Set rudder trim to the neutral position. 3. Using the standby attitude indicator, initiate a 15" bank left turn. Keep feet off rudder pedals. Maintain altitude and 15" bank angle. Continue the turn for 60 seconds, then roll back to level flight. 4. When the compass card becomes sufficiently stable, check the accuracy of the turn by verifying that the compass heading approximates the reciprocal of the originai heading. 5. If necessary, adjust the heading by keeping the wings level and using the rudder to make skidding turns (the compass will read more accurately) to complete the course reversal. 6 . Maintain altitude and airspeed by cautious application of elevator control. Keep the roll pointer and index aligned and steer only with rudder. (Continued Next Page) U.S. 3- 27 SECTION 3 EMERGENCY PROCEDURES CESSNA MODEL 182T NAV Ill (EMERGENCY OPERATION IN CLOUDS (Continued) EMERGENCY DESCENT THROUGH CLOUDS (AHRS FAILED) When returning to VFR flight after a 180" turn is not practical, a descent through the clouds to VFR conditions below may be appropriate. If possible, obtain an ATC clearance for an emergency descent through the clouds. AHRS Failure Choose an easterly or westerly heading to minimize non - stabilized magnetic compass card sensitivity. Occasionally check the compass heading and make minor corrections to hold an approximate course. The autopilot may be engaged in ROL mode to keep the wings level and VS mode to control rate- of -descent. Before descending into the clouds, prepare for a stabilized descent as follows: 1. Apply full rich mixture. 2. Set rudder trim to neutral position. 3. Turn pitot heat on. 4. Set power for a 500 to 800 feet per minute rate- of- descent. 5. Set the elevator trim for a stabilized descent at 80 KIAS. 6. Use the standby attitude indicator roll pointer and index to keep wirrgs level. 7. Check trend of compass card movement and make cautious corrections with rudder to stop the turn. 8. Upon breaking out of clouds, resume normal cruising flight. (Continued Next Page) 3 - 28 U.S. CESSNA MODEL 182T NAV I11 SECTION 3 EMERGENCY PROCEDLIRES EMERGENCY OPERATION IN CLOUDS (Continued) 1 EXECUTING A 180"TURN IN CLOUDS (AHRS FAILED) Upon inadvertently entering the clouds, an immediate turn to reverse course and return to VFR conditions should be made as follows: AHRS Failure 1. Note the non-stabilized magnetic compass heading. 2. Set rudder trim to the neutral position. 3. Using the standby attitude indicator, initiate a 15" bank left turn. Keep feet off rudder pedals. Maintain altitude and 15 " bank angle. Continue the turn for 60 seconds, then roll back to level flight. 4. When the compass card becomes sufficiently stable, check the accuracy of the turn by verifying that the compass heading approximates the reciprocal of the original heading. 5. If necessary, adjust the heading by keeping the wings level and using the rudder to make skidding turns (the compass will read more accurately) to complete the course reversal. 6. Maintain altitude and airspeed by cautious application of elevator control. Keep the roll pointer and index aligned and steer only with rudder. (Continued Next Page) U.S. 3 - 27 SECTION 3 EMERGENCY PROCEDLIRES CESSNA MODEL 182T NAV Ill IEMERGENCY OPERATION IN CLOUDS (Continued) EMERGENCY DESCENT THROUGH CLOUDS (AHRS FAILED) When returning to VFR flight after a 180" turn is not practical, a descent through the clouds to VFR conditions below may be appropriate. If possible, obtain an ATC clearance for an emergency descent through the clouds. AHRS Failure Choose an easterly or westerly heading to minimize non- stabilized magnetic compass card sensitivity. Occasionally check the compass heading and make minor corrections to hold an approximate course. The autopilot may be engaged in ROL mode to keep the wings level and VS mode to control rate - of -descent. Before descending into the clouds, prepare for a stabilized descent as follows: 1. Apply full rich mixture. 2. Set rudder trim to neutral position. 3. Turn pitot heat on. 4. Set power for a 500 to 800 feet per minute rate -of -descent. 5. Set the elevator trim for a stabilized descent at 80 KIAS. 6. Use the standby attitude indicator roll pointer and index to keep wings level. 7. Check trend of compass card movement and make cautious corrections with rudder to stop the turn. 8. Upon breaking out of clouds, resume normal cruising flight. (Continued Next Page) 3 -28 U.S. CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES EMERGENCY OPERATION IN CLOUDS) (Continued) IR E C O V E R Y FR OM S P I R A L DI VE IN THE CLOUDS (AHRS- FAILED) AHRS Failure If a spiral is entered while in the clouds, continue as follows: 1. Retard throttle to idle position. 2. Remove feet from rudder pedals. 3. Stop turn by carefully leveling the wings using aileron control to align the roll index and roll pointer of the standby attitude indicator. 4. Cautiously apply elevator back pressure to slowly reduce the airspeed to 80 KIAS. 5. Adjust the elevator trim control to maintain an 80 KIAS glide. 6 . Set rudder trim to neutral position. 7. Use aileron control to maintain wings level (keep roll pointer and index aligned) and constant heading. 8. Resume EMERGENCY DESCENT THROUGH THE CLOUDS procedure. 9. Upon breaking out of clouds, resume normal cruising flight. INADVERTENT FLIGHT INTO ICING CONDITIONS Flight into icing conditions is prohibited and extremely dangerous. An inadvertent encounter with these conditions can be resolved using the checklist procedures. The best action is to turn back or change altitude to escape icing conditions. Set the PlTOT HEAT switch to the ON position until safely out of icing conditions. During these encounters, an unexplained loss of manifold pressur could be caused by ice blocking the air intake filter or in extreme1 rare instances ice completely blocking the fuel injection ai reference tubes. In either case, the throttle should be positioned t hold manifold pressure (in some instances, the throttle may need t any change in power settings. !be retarded for maximum power). Adjust mixture+a necessary; fon I U.S. 3 - 29 SECTION 3 EMERGENCY PROCEDLIRES CESSNA MODEL 182T NAV III STATIC SOURCE BLOCKED If erroneous readings of the static source instruments (airspeed, Ialtimeter and vertical speed) are suspected, the ALT STATIC AIR valve should be pulled ON, thereby supplying static pressure to these instruments from the cabin. When the ALT STATIC AIR valve is ON, the