Cessna. 1979 - TOPS Flying Club – Troy Oakland Pilots

1 October 1978 Page Date Title. 1 October 1978 Assignment Record thru h 1 October 1978 1 October 1978 Page 6-2 Bank 6-thru 6-13. G-14 Blank Date 1 October 1978 1 October 1978 1 October 1978 1-1 thru 1-9 1-10 Blank 1 October 1978 1 October 1978 6-15 thru 6-25......... 6-26 Blank 1 October 1978 1 October 1978 2-1... 2-2 Blank 2-3 thru 2-11...c 2-12 Blank 3-1 thru 3-19... 3-20 Blank 1 October 1978 1 October 1978 1 October 1978 1 October 1978 1 October 1978 1 October 1978 4:1 thru 4-24…….. 1 October 1978 5.1...... 5-2 Blank 5-3 thru 5-29 1 October 1978 1 October 1978 1 October 1978 5 JO Blank 61 1 October 1978 1 October 1978 7-1 thru 7-49. 7-50 Blank 6-1 5-2 Blank. 8-3 thru 8-15. 8-16 Blank 9-1 thru 9-24ancem NOTE Refer to Section 9 Table of Contents for supplements applicable to optional systems 1 October 1978 1 October 1978 1 October 1976 1 October 1978 1 October 1978 1 October 1978 1 October 1978 1 October 1978 TABLE OF CONTENTS CESSNA MODEL TR182 TABLE OF CONTENTS SECTION GENERAL.... LIMITATIONS... EMERGENCY PROCEDURES. 1 2 3 NORMAL PROCEDURES....... .. 4 PERFORMANCE.. 5 WEIGHT & BALANCE/ EQUIPMENT LIST AIRPLANE & SYSTEMS DESCRIPTIONS...... 6 .....7 AIRPLANE HANDLING, SERVICE & MAINTENANCE SUPPLEMENTS 8 (Optional Systems Description 9 & Operating Procedures) 1 October 1978 CESSNA MODEL TR182 SECTION 1 GENERAL SECTION 1 GENERAL TABLE OF CONTENTS Page Three View Introduction Descriptive Data Engine Propeller 1-2 1-3 1-3 1-3 " 1-3 Fuel Oil 1-3 1-4 Maximum Certificated Weights Standard Airplane Weights Cabin And Entry Dimensions Baggage Space And Entry Dimensions 1-5 1-5 1-5 1-5 Specific Loadings 15. Symbols, Abbreviations And Terminology 1-6 General Airspeed Terminology And Symbols 1-6 Meteorological Terminology 1-7 Engine Power Terminology 1-7 Airplane Performance And Flight Planning Terminology 1-7 Weight And Balance Terminology 1-8 1 October 1978 1-1 SECTION 1 GENERAL CESSNA MODEL TR182 1-2 HVOT POINT MAX 82 8DD- 36.0 NOTES depresand as far as possible and flashing 7. Minimum turning radius in pevart point PIVOT POINT Figure 1-1. Three View 1 October 1978 CESSNA MODEL TR182 SECTION 1 GENERAL INTRODUCTION This handbook contains 9 sections, and includes the material required to be furnished to the pilot by CAR Part 3. It also contains supplemental data supplied by Cessna Aircraft Company. Section 1 provides basic data and information of general interest. It also contains definitions or explanations of symbols, abbreviations, and terminology commonly used. DESCRIPTIVE DATA ENGINE Number of Engines: 1. Engine Manufacturer: Avco Lycoming. Engine Model Number: 0-540-L3C5D. Engine Type: Turbocharged, direct-drive. air-cooled, horizontally- opposed, carburetor equipped, six-cylinder engine with 541.5 cu. in displacement. Horsepower Rating and Engine Speed: 235 rated BHP at 31 inches Hg and 2400 RPM. PROPELLER Propeller Manufacturer. McCauley Accessory Division. Propeller Model Number: B2D34C217/90DHB-8. Number of Blades: 2. Propeller Diameter. Maximum: 82 inches. Minimum: 80.5 inches. Propeller Type: Constant speed and hydraulically actuated, with a low pitch setting of 15.8" and a high pitch setting of 31.9" (30 inch station). FUEL Approved Fuel Grades (and Colors): 100LL Grade Aviation Fuel (Blue). 100 (Formerly 100/130) Grade Aviation Fuel (Green). 1 October 1978 1-3 SECTION 1 GENERAL Total Capacity: 92 gallons. Total Capacity Each Tank: 46 gallons. Total Usable: 88 gallons. CESSNA MODEL TR182 NOTE To ensure maximum fuel capacity when refueling and minimize cross-feeding when parked on a sloping surface. place the fuel selector valve in either LEFT or RIGHT position. OIL Oil Grade (Specification): MIL-L-6082 Aviation Grade Straight Mineral Oil: Use to replenish supply during first 25 hours and at the first 25-hour oil change. Continue to use until a total of 50 hours has accumulated or oil consumption has stabilized. NOTE The airplane was delivered from the factory with a corro- sion preventive aircraft engine oil. This oil should be drained after the first 25 hours of operation. MIL-L-22851 Ashless Dispersant Oil: This oil must be used after first 50 hours or oil consumption has stabilized. Recommended Viscosity For Temperature Range: MIL-L-6082 Aviation Grade Straight Mineral Oil: SAE 50 above 16°C (60°F). SAE 40 between -1°C (30°F) and 32°C (90°F). SAE 30 between -18°C (0°F) and 21°C (70°F). SAE 20 below -12°C (10°F). MIL-L-22851 Ashless Dispersant Oil: SAE 40 or SAE 50 above 16°C (60°F). SAE 40 between -1°C (30°F) and 32°C (90°F). SAE 30 or SAE 40 between -18°C (0°F) and 21°C (70°F). SAE 30 below -12°C (10°F). Oil Capacity: Sump: 8 Quarts. 1-4 Total: 9 Quarts. 1 October 1978 CESSNA MODEL TR182 SECTION 1 GENERAL MAXIMUM CERTIFICATED WEIGHTS Ramp: 3112 lbs. Takeoff: 3100 lbs. Landing: 3100 lbs. Weight in Baggage Compartment: Baggage Area "A" (or passenger on child's seat) - Station 82 to 110: 120 lbs. See note below. Baggage Area "B" - Station 110 to 134: 80 lbs. See note below. NOTE The maximum combined weight capacity for baggage areas A and B is 200 lbs.. STANDARD AIRPLANE WEIGHTS Standard Empty Weight, Turbo Skylane RG: 1764 lbs. Turbo Skylane RG II: 1815 lbs. Maximum Useful Load, Turbo Skylane RG: 1348 lbs. Turbo Skylane RG II: 1297 lbs. 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 lbs./sq. ft. Power Loading: 13.2 lbs./hp. 1 October 1978 1-5 SECTION 1 GENERAL SYMBOLS, ABBREVIATIONS AND TERMINOLOGY CESSNA MODEL TR182 GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS KIAS KTAS VFE VLE VLO VNO VNE 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. 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. Manuevering Speed is the maximum speed at which you may use abrupt control travel. Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. Maximum Landing Gear Extended Speed is the maximum speed at which an airplane can be safely flown with the landing gear extended. Maximum Landing Gear Operating Speed is the maximum speed at which the landing gear can be safely extended or retracted. 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 at which the airplane is controllable. Stalling Speed or the minimum steady flight speed at which the airplane is controllable in the landing configu ration at the most forward center of gravity. 1-6 1 October 1978 CESSNA MODEL TR182 SECTION 1 GENERAL Vy Best Angle-of-Climb Speed is the speed which results in the greatest gain of altitude in a given horizontal distance. Best Rate-of-Climb Speed is the speed which results in the greatest gain in altitude in a given time. METEOROLOGICAL TERMINOLOGY OAT Standard Tempera- ture Pressure Altitude Outside Air Temperature is the free air static temperature. It is expressed in either degrees Celsius or degrees Fah- renheit. Standard Temperature is 15°C at sea level pressure alti- tude and decreases by 2°C for each 1000 feet of 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 RPM MP Brake Horsepower is the power developed by the engine. Revolutions Per Minute is engine speed. Manifold Pressure is a pressure measured in the engine" induction system and is expressed in inches of mercury (Hg). AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Demon- strated Crosswind Velocity Usable Fuel Unusable Fuel GPH Demonstrated Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplane during takeoff and landing was actually demon- strated during certification tests. The value shown is not considered to be limiting. Usable Fuel is the fuel available for flight planning. Unusable Fuel is the quantity of fuel that can not be safely used in flight. Gallons Per Hour is the amount of fuel (in gallons) consumed per hour. 1 October 1978 1-7 SECTION 1 GENERAL CESSNA MODEL TR182 NMPG Nautical Miles Per Gallon is the distance (in nautical miles) which can be expected per gallon of fuel consumed at a specific engine power setting and/or flight configura- tion. g is acceleration due to gravity. WEIGHT AND BALANCE TERMINOLOGY Reference Datum Station Arm Moment Center of Gravity (C.G.) C.G. Arm C.G. Limits Standard Empty Weight Basic Empty Weight Useful Load Reference Datum is an imaginary vertical plane from which all horizontal distances are measured for balance purposes. Station is a location along the airplane fuselage given in terms of the distance from the reference datum. Arm is the horizontal distance from the reference datum to the center of gravity (C.G.) of an item. 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 reduc- ing the number of digits.) 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. Center of Gravity Arm is the arm obtained by adding the airplane's individual moments and dividing the sum by the total weight. 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 is the weight of a standard air- plane, including unusable fuel, full operating fluids and full engine oil. Basic Empty Weight is the standard empty weight plus the weight of optional equipment. Useful Load is the difference between ramp weight and the basic empty weight. 1-8 1 October 1978