AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT

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AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT,CESSNA 182Q 182R. IO 550 3500 LBS,THIS PAGE BLANK,Page 2 of 81 IR APR 14 2014. AIRPLANE FLIGHT MANUAL SUPPLEMENT AMPHIBIAN,CESSNA 182Q 182R. IO 550 3500 LBS, This Airplane Flight Manual Supplement contains information applicable to the Cessna. Model 182Q serial numbers 18266591 through 18267715 except 18267302 and 182R. serial numbers 18267302 and 18267716 through 18268586 when equipped with Wipline. 3000 amphibious floats a 3500 lb gross weight increase kit and 300 BHP IO 550 D. engine installed under STC SA00152WI,ORIGINAL ISSUE AND REVISIONS.
This Airplane Flight Manual Supplement was originally issued on To. ensure that information in this manual is current revisions must be incorporated as they. are issued Revision status is noted on the Log of Revisions page and in the List of. Effective Pages Revision status of individual pages is noted on the bottom of each page. It is the responsibility of the airplane owner to maintain this supplement in a current status. when it is being used for operational purposes, The List of Effective Pages contains page numbers and revision levels for all pages. contained in this supplement The Log of Revisions contains a history of the revisions and. dates of approval When a revision occurs the old pages should be replaced with new. pages containing the latest revision according to the List of Effective Pages. APR 14 2014 IR Page 3 of 81,AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT. CESSNA 182Q 182R,IO 550 3500 LBS,THIS PAGE BLANK,Page 4 of 81 IR APR 14 2014. AIRPLANE FLIGHT MANUAL SUPPLEMENT AMPHIBIAN,CESSNA 182Q 182R. IO 550 3500 LBS,LOG OF REVISIONS,NO DESCRIPTION DATE FAA APPROVED.
IR Initial Release,APR 14 2014 IR Page 5 of 81,AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT. CESSNA 182Q 182R,IO 550 3500 LBS,LIST OF EFFECTIVE PAGES. Page Revision Level Page Revision Level Page Revision Level. 1 IR 28 IR 55 IR,2 IR 29 IR 56 IR,3 IR 30 IR 57 IR. 4 IR 31 IR 58 IR,5 IR 32 IR 59 IR,6 IR 33 IR 60 IR. 7 IR 34 IR 61 IR,8 IR 35 IR 62 IR,9 IR 36 IR 63 IR.
10 IR 37 IR 64 IR,11 IR 38 IR 65 IR,12 IR 39 IR 66 IR. 13 IR 40 IR 67 IR,14 IR 41 IR 68 IR,15 IR 42 IR 69 IR. 16 IR 43 IR 70 IR,17 IR 44 IR 71 IR,18 IR 45 IR 72 IR. 19 IR 46 IR 73 IR,20 IR 47 IR 74 IR,21 IR 48 IR 75 IR. 22 IR 49 IR 76 IR,23 IR 50 IR 77 IR,24 IR 51 IR 78 IR.
25 IR 52 IR 79 IR,26 IR 53 IR 80 IR,27 IR 54 IR 81 IR. Page 6 of 81 IR APR 14 2014,AIRPLANE FLIGHT MANUAL SUPPLEMENT AMPHIBIAN. CESSNA 182Q 182R,IO 550 3500 LBS,TABLE OF CONTENTS. TITLE PAGE 1,LOG OF REVISIONS 5,LIST OF EFFECTIVE PAGES 6. SIDE VIEW 8,GENERAL INFORMATION 9,SECTION 1 GENERAL 11.
SECTION 2 LIMITATIONS 17,SECTION 3 EMERGENCY PROCEDURES 25. SECTION 4 NORMAL PROCEDURES 39,SECTION 5 PERFORMANCE 57. SECTION 6 WEIGHT AND BALANCE 69,SECTION 7 AIRPLANE AND SYSTEMS DESCRIPTION 73. SECTION 8 AIRPLANE HANDLING SERVICE AND MAINTENANCE 79. APR 14 2014 IR Page 7 of 81,AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT. CESSNA 182Q 182R,IO 550 3500 LBS,Figure 1 1 Side View.
Page 8 of 81 IR APR 14 2014,AIRPLANE FLIGHT MANUAL SUPPLEMENT AMPHIBIAN. CESSNA 182Q 182R,IO 550 3500 LBS,GENERAL INFORMATION. MAXIMUM ENROUTE RATE OF CLIMB AT SEA LEVEL,3 500 Pounds 867 ft min. SERVICE CEILING 13 518 ft, TAKEOFF PERFORMANCE AT SEA LEVEL 3 500 Pounds Land. Ground Roll 1113 ft,Total Distance Over 50 Ft Obstacle 2224 ft.
LANDING PERFORMANCE AT SEA LEVEL 3 350 Pounds Land. Ground Roll 709 ft,Total Distance Over 50 Ft Obstacle 1526 ft. TAKEOFF PERFORMANCE AT SEA LEVEL 3 472 Pounds Water. Water Run 1313 ft,Total Distance Over 50 Ft Obstacle 2585 ft. LANDING PERFORMANCE AT SEA LEVEL 3 350 Pounds Water. Ground Roll 912 ft,Total Distance Over 50 Ft Obstacle 1820 ft. STALL SPEED,Flaps Up Power Off 3 500 Pounds 67 KCAS. Flaps Down Power Off 3 500 Pounds 60 KCAS,MAXIMUM WEIGHT.
Ramp 3 510 lb,Dock 3 482 lb,Takeoff on Wheels 3 500 lb. Takeoff on Water 3 472 lb,Landing on Wheels or Water 3 350 lb. STANDARD EMPTY WEIGHT 2 550 lb,USEFUL LOAD 960 lb,WING LOADING. 3 500 Pounds 20 1 lbs sqft,POWER LOADING,3 500 Pounds 11 7 lbs HP. FUEL CAPACITY 92 gal,OIL CAPACITY 12 qts,Teledyne Continental IO 550 D.
300 BHP at 2700 RPM,MT Propeller 3 Blade Constant Speed Composite. Diameter 82 7 in 210 cm,APR 14 2014 IR Page 9 of 81. AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT,CESSNA 182Q 182R. IO 550 3500 LBS,THIS PAGE BLANK,Page 10 of 81 IR APR 14 2014. AIRPLANE FLIGHT MANUAL SUPPLEMENT AMPHIBIAN,SECTION 1 CESSNA 182Q 182R.
IO 550 3500 LBS,INTRODUCTION, This AFM supplement written especially for operators of the Cessna 182Q and 182R. Skylane amphibian with 300 hp IO 550 D engine provides information not found in the. basic Pilot s Operating Handbook It contains procedures and data required for safe and. efficient operation of the Cessna 182Q 182R Skylane equipped with Wipline Model 3000. amphibious floats and Continental IO 550 D engine installed under Air Plains STC. SA00152WI This AFM Supplement contains eight 8 sections and includes the material. required to be furnished to the pilot by Federal Aviation Regulations FAR and additional. information provided by Wipaire Inc The information contained herein supplements or. supersedes the basic Cessna 182 Skylane POH AFM and the Air Plains AFM Supplement. only in those areas listed For limitations procedures and performance information not. contained in this supplement consult the basic POH AFM or Air Plains AFM Supplement. as applicable Generally pertinent information has been repeated here for quick. reference Information contained in the basic handbook for the Cessna 182Q 182R. Skylane which is the same as that for the floatplane is generally not repeated in this. supplement, 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,Number of Engines 1,Engine Manufacturer Teledyne Continental. Engine Model Number IO 550 D, Engine Type Normally aspirated direct drive air cooled horizontally. opposed fuel injected six cylinder engine with 550 cu In. displacement,Maximum Power 300 rated BHP at 2700 RPM.
Maximum Continuous Power 300 rated BHP at 2700 RPM. Propeller Manufacturer MT Propeller,Propeller Model Number MTV 9 D 210 58. Number of Blades 3,Propeller Diameter Maximum 82 7 in 210 cm. Minimum 78 7 in 200 cm, Propeller Type Constant speed hydraulically actuated composite bladed. propeller with a low pitch setting of 7 5 and a high pitch. setting of 38 79 cm station,APR 14 2014 IR Page 11 of 81. AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT,CESSNA 182Q 182R SECTION 1.
IO 550 3500 LBS,MAXIMUM CERTIFICATED WEIGHTS,Takeoff from Land 3 500 lbs 1587 kg. Takeoff from Water 3 472 lbs 1575 kg,Landing on Land or Water 3 350 lbs 1520 kg. STANDARD AIRPLANE WEIGHTS,Standard Empty Weight 2 550 lbs 1157 kg. Maximum Useful Load 960 lbs 435 kg,SPECIFIC LOADINGS at 3 500 lbs 1587 kg. Wing Loading 20 1 lbs sq ft,Power Loading 11 7 lbs HP.
SYMBOLS ABBREVIATIONS AND TERMINOLOGY,GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS. KCAS Knots Calibrated Airspeed is indicated airspeed corrected for position. and instrument error and is expressed in knots,Page 12 of 81 IR APR 14 2014. AIRPLANE FLIGHT MANUAL SUPPLEMENT AMPHIBIAN,SECTION 1 CESSNA 182Q 182R. IO 550 3500 LBS, KGS Knots Groundspeed is the actual speed over the ground or water and is. expressed in knots, KIAS Knots Indicated Airspeed is the speed shown on the airspeed indicator.
and is expressed in knots, KTAS Knots True Airspeed is the airspeed relative to undisturbed air which is. KCAS corrected for altitude and temperature and is expressed in knots. VA Maximum Operating Maneuvering Speed is the maximum speed at. which full or abrupt control movements may be used at a particular weight. VFE Maximum Flap Extended Speed is the highest speed permissible with. wing flaps extended, VNO Maximum Structural Cruising Speed is the speed that should not be. exceeded except in smooth air then only with caution. VNE Never Exceed Speed is the speed which should never be exceeded. during flight operations, Vs Stalling Speed or the minimum steady flight speed at which the. airplane is controllable, Vs0 Stalling Speed or the minimum steady flight speed at which the. airplane is controllable in the landing configuration at the most forward. center of gravity, 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. of altitude in a given time,METEOROLOGICAL TERMINOLOGY. OAT Outside Air Temperature is the free air static temperature and is. expressed in either degrees Celsius or degrees Fahrenheit. Standard Standard Temperature is 15 C as sea level pressure altitude and. Temperature decreases by 2 C for each 1000 feet of altitude. Pressure Pressure Altitude is the altitude read from an altimeter with its barometric. Altitude scale set to 29 92 inches of mercury 1013 2 mb. ISA International Standard Atmosphere is the atmosphere in which. 1 The air is a perfect dry gas,2 The temperature at sea level is 15 C. 3 The pressure at sea level is 29 92 inches Hg 1013 2 mb. APR 14 2014 IR Page 13 of 81,AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT. CESSNA 182Q 182R SECTION 1,IO 550 3500 LBS, 4 The temperature gradient from sea level is 1 98 C per 1000 feet of.
ENGINE POWER TERMINOLOGY, BHP Brake Horsepower is the power developed by the engine. RPM Revolutions Per Minute is engine speed, 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. AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY. Demon Demonstrated Crosswind Velocity is the velocity of the crosswind. strated component for which adequate control of the airplane during takeoff. Crosswind landing taxi was demonstrated during certification tests The value. Velocity shown is not considered to be limiting,g g is the acceleration due to gravity. NMPG Nautical Miles Per Gallon is the distance which can be expected per. gallon of fuel consumed at a specific engine power setting and or flight. configuration, GPH Gallons Per Hour is the amount of fuel consumed per hour.
Unusable Unusable Fuel is the quantity of fuel that cannot be safely used in flight. Usable Fuel Usable Fuel is the fuel available for flight planning. WEIGHT AND BALANCE TERMINOLOGY, Arm Arm is the horizontal distance from the reference datum to the center of. gravity C G of an item, Basic Empty Basic Empty Weight is the standard empty weight plus the weight of. Weight optional equipment, Center of Center of Gravity is the point at which an airplane would balance if. Gravity suspended Its distance from the reference datum is found by dividing the. C G total moment by the total weight, C G Arm C G Arm is the arm obtained by adding the airplane s individual moments. and dividing the sum by the total weight,Page 14 of 81 IR APR 14 2014.
AIRPLANE FLIGHT MANUAL SUPPLEMENT AMPHIBIAN,SECTION 1 CESSNA 182Q 182R. IO 550 3500 LBS, C G Limits C G Limits are the extreme center of gravity locations within which the. airplane must be operated at any given weight, MAC MAC Mean Aerodynamic Chord of a wing is the chord of an imaginary. rectangular airfoil having the same pitching moments throughout the flight. range as that of the actual wing, Maximum Maximum Landing Weight is the maximum weight approved for the. Landing landing touchdown, Maximum Maximum Takeoff Weight is the maximum weight approved for the start.
Takeoff of the takeoff roll, Moment Moment is the product of the weight of an item multiplied by its arm. Moment divided by 1000 is used in this supplement to simplify balance. calculations by reducing the number of digits, Reference Reference Datum is an imaginary vertical plane at the front face of the. Datum firewall from which all horizontal distances are measured for balance. Standard Standard Empty Weight is the weight of a standard airplane including. Empty unusable fuel full operating fluids and full engine oil. Station Station is a location along the fuselage given in terms of distance from the. reference datum Also referred to as Fuselage Station FS. Tare Tare is the weight of chocks blocks stands balance weights 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. Useful Useful Load is the difference between ramp weight and the basic empty. Load weight,WARNINGS CAUTIONS AND NOTES, WARNING An operating procedure technique or maintenance practice which. may result in personal injury or loss of life if not carefully followed. CAUTION An operating procedure technique or maintenance practice which. may result in damage to equipment if not carefully followed. NOTE An operating procedure technique or maintenance condition which is. AMPHIBIAN AIRPLANE FLIGHT MANUAL SUPPLEMENT CESSNA 182Q 182R SECTION 1 IO 550 3500 LBS Page 14 of 81 IR APR 14 2014 4 The temperature gradient from sea level is 1 98 C per 1000 feet of altitude ENGINE POWER TERMINOLOGY BHP Brake Horsepower is the power developed by the engine RPM Revolutions Per Minute is engine speed

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