NOTICE - Learn to Fly in Miami at Wayman Flight …

1 NOTICEAT THE TIME OF ISSUANCE, THISINFORMATION manual WAS AN EXACTDUPLICATE OF THE OFFICIAL PILOT'SOPERATING HANDBOOK AND FAAAPPROVED AIRPLANE Flight MANUALAND IS TO BE USED FOR GENERALPURPOSES WILL NOT BE KEPT CURRENT AND,THEREFORE, CANNOT BE USED AS ASUBSTITUTE FOR THE OFFICIAL PILOT'SOPERATING HANDBOOK AND FAAAPPROVED AIRPLANE Flight MANUALINTENDED FOR OPERATION OF AIRCRAFT COMPANYORIGINAL ISSUE - 2 DECEMBER 1996 Dec 2/96iPERFORMANCE-CESSNASPECIFICATIONSMOD EL 172 RPERFORMANCE - SPECIFICATIONS* SPEED:Maximum at Sea Level .. 123 KNOTSC ruise, 80% Power at 8000 FT .. 122 KNOTSCRUISE: Recommended lean mixture with fuel allowance forengine start, taxi, takeoff, climb and 45 Power at 8000 FT.

2 Range580 NM 53 Gallons Usable HRSR ange at 10,000 FT, 60% power.. Range687 NM 53 Gallons Usable HRSRATE OF CLIMB AT SEA LEVEL..720 FPMSERVICE CEILING ..13,500 FTTAKEOFF PERFORMANCE:Ground Roll .. 945 FTTotal Distance Over 50 FT Obstacle .. 1685 FTLANDING PERFORMANCE:Ground Roll .. 550 FTTotal Distance Over 50 FT Obstacle .. 1295 FTSTALL SPEED:Flaps Up, Power Off .. 51 KCASF laps Down, Power Off .. 47 KCASMAXIMUM WEIGHT:Ramp..2457 LBST akeoff..2450 LBSL anding ..2450 LBSSTANDARD EMPTY WEIGHT ..1639 LBSMAXIMUM USEFUL LOAD..818 LBSBAGGAGE ALLOWANCE ..120 LBSiiFeb 28/00 CESSNASECTION 1 MODEL 172 RGENERALPERFORMANCE-SPECIFICATIONS(Conti nued)WING LOADING: Lbs/Sq Ft.

3 LOADING: Lbs/HP .. CAPACITY..56 GALOIL CAPACITY ..8 QTSENGINE: Textron Lycoming ..IO-360-L2A160 BHP at 2400 RPMPROPELLER: Fixed Pitch, Diameter..75 IN.* NOTES peed performance is shown for an airplane equipped withoptional speed fairings which increase the speeds byapproximately 2 knots. There is a corresponding differencein range, while all other performance figures are unchangedwhen speed fairings are above performance figures are based on the indicatedweights, standard atmospheric conditions, level hard-surfacedry runways and no wind. They are calculated values derivedfrom Flight tests conducted by the Cessna Aircraft Companyunder carefully documented conditions and will vary withindividual airplanes and numerous other factors affecting flightperformanceFeb 28/00iii/(iv blank)Information ManualThe Cessna AircraftCompany Model 172 RCOPYRIGHT 1996 The Cessna Aircraft CompanyWichita, Kansas USAM ember of GAMAP/N: 172 RIM Nov 3/97v/(vi blank)CESSNAMODEL 172 RTABLE OF CONTENTSTABLE OF CONTENTSSECTIONGENERAL.

4 1 LIMITATIONS .. 2 EMERGENCY PROCEDURES .. 3 NORMAL PROCEDURES .. 4 PERFORMANCE .. 5 WEIGHT & BALANCE/EQUIPMENT LIST .. 6 AIRPLANE & SYSTEMS DESCRIPTION .. 7 HANDLING, SERVICE & MAINTENANCE .. 8 SUPPLEMENTS .. 9 Dec 2/96vii/(viii blank)CESSNASECTION 1 MODEL 172 RGENERALSECTION 1 GENERALTABLE OF CONTENTSPageThree View - Normal Ground Attitude ..1-2 Introduction ..1-4 Descriptive Data ..1-4 Engine ..1-4 Propeller ..1-4 Fuel ..1-4 Oil ..1-5 Maximum Certificated Weights..1-6 Standard Airplane Weights..1-7 Cabin And Entry Dimensions ..1-7 Baggage Space and Entry Dimensions..1-7 Specific Loadings ..1-7 Symbols, Abbreviations and Terminology.

5 1-8 General Airspeed Terminology And Symbols..1-8 Meteorological Terminology ..1-9 Engine Power Terminology ..1-9 Airplane Performance And Flight Planning Terminology.. 1-10 Weight And Balance Terminology.. 1-11 Metric / Imperial / Conversion Charts.. 1-13 Weight Conversions.. 1-14 Length Conversions.. 1-16 Distance Conversions .. 1-20 Volume Conversions .. 1-21 Temperature Conversions .. 1-24 Hectopascals to Inches Mercury Conversions.. 1-25 Volume to Weight Conversions.. 1-26 Quick Conversions.. 1-27/1-28 Revision 71-1 SECTION 1 CESSNAGENERALMODEL 172 RFigure 1-1. Three View - Normal GroundAttitude (Sheet 1 of 2) 75 MAX 0510T10050510T100536 -1 11 -4 1-2 Revision 7 CESSNASECTION 1 MODEL 172 RGENERALF igure 1-1.

6 Three View - Normal Ground Attitude (Sheet 2) 0510T100527 -2 8 -11 MAX. NOTE 1:WING SPAN SHOWN WITH STROBE 2:WHEEL BASE LENGTH IS 65 .NOTE 3:PROPELLER GROUND CLEARANCE IS 11 1/4 .NOTE 4:WING AREA IS 174 SQUARE 5:MINIMUM TURNING RADIUS (* PIVOT POINT TOOUTBOARD WING TIP) IS 27 -5 1/2 .NOTE 6:NORMAL GROUND ATTITUDE IS SHOWN WITH NOSE STRUT SHOWING APPROXIMATELY 2 OFSTRUT, AND WINGS 71-3 SECTION 1 CESSNAGENERALMODEL 172 RINTRODUCTIONThis handbook contains 9 sections, and includes the materialrequired to be furnished to the pilot by FAR Part 23. It also containssupplemental data supplied by Cessna Aircraft 1 provides basic data and information of general also contains definitions or explanations of symbols,abbreviations, and terminology commonly DATAENGINEN umber of Engines: Manufacturer: Textron Model Number: Type:Normally aspirated, direct drive, air-cooled, horizontally opposed, fuel injected, four cylinderengine with 360 cu.

7 In. Rating and Engine Speed: 160 rated BHP at 2400 Manufacturer: McCauley Propeller Model Number: 1C235 of Blades: Diameter: 75 Type: Fixed OF UNAPPROVED FUELS MAY RESULT INDAMAGE TO THE ENGINE AND FUEL SYSTEMCOMPONENTS, RESULTING IN POSSIBLEENGINE Fuel Grades (and Colors):100LL Grade Aviation Fuel (Blue).100 Grade Aviation Fuel (Green).1-4 Revision 7 CESSNASECTION 1 MODEL 172 RGENERALNOTEI sopropyl alcohol or diethylene glycol monomethyl ether(DiEGME) may be added to the fuel supply. Additiveconcentrations shall not exceed 1% for isopropyl alcohol to for DiEGME. Refer to Section 8 foradditional Capacity:Total Capacity Each Tank: Usable Each 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 inthe Left or Right position.

8 Refer to Figure 1-1 for normalground attitude Specification:MIL-L-6082 or SAE J1966 Aviation Grade Straight Mineral Oil:Used when the airplane was delivered from the factory and shouldbe used to replenish the supply during the first 25 hours. This oilshould be drained and the filter changed after the first 25 hours ofoperation. Refill the engine with MIL-L-6082 or SAE J1966 AviationGrade Straight Mineral Oil and continue to use until a total of 50hours has accumulated or oil consumption has or SAE J1899 Aviation Grade Ashless DispersantOil: Oil conforming to the latest revision and/or supplements toTextron Lycoming Service Instruction No.

9 1014, must be used afterfirst 50 hours or once oil consumption has 71-5 SECTION 1 CESSNAGENERALMODEL 172 RRecommended Viscosity for Temperature Range: TemperatureMIL-L-6082orSAE J1966 StraightMineral OilSAE GradeMIL-L-22851 orSAE J1899 Ashless DispersantSAE GradeAbove 27 C (80 F)60 60 Above 16 C (60 F)5040 or 50-1 C (30 F) to 32 C (90 F)4040-18 C (0 F) to 21 C (70 F)3030, 40 or 20W-40 Below -12 C (10 F) 2030 or 20W-30-18 C (0 F) to 32 C (90 F)20W-5020W-50 or 15W-50 All Temperatures >>>15W-50 or 20W-50 NOTEWhen operating temperatures overlap, use the lighter gradeof Capacity:Sump: 8 QuartsTotal:9 QuartsMAXIMUM CERTIFICATED WEIGHTSRamp WeightNormal Category: 2457 Category: 2107 WeightNormal Category: 2450 Category: 2100 WeightNormal Category: 2450 Category: 2100 7 CESSNASECTION 1 MODEL 172 RGENERALW eight in Baggage Compartment, Normal Category:Baggage Area 1 (Station 82 to 108):120 lbs.

10 See note Area 2 (Station 108 to 142): 50 lbs. See note maximum combined weight capacity for Baggage Area 1and Baggage Area 2 is 120 in Baggage Compartment, Utility Category:In this category, the rear seat must not be occupied and thebaggage compartment must be AIRPLANE WEIGHTSS tandard Empty Weight: 1639 Useful Load, Normal Category: 818 Useful Load, Utility Category : 468 AND ENTRY DIMENSIONSD etailed dimensions of the cabin interior and entry door openingsare illustrated in Section SPACE AND ENTRY DIMENSIONSD imensions of the baggage area and baggage door opening areillustrated in detail in Section LOADINGSWing 71-7 SECTION 1 CESSNAGENERALMODEL 172 RSYMBOLS, ABBREVIATIONS AND TERMINOLOGYGENERAL AIRSPEED TERMINOLOGY AND SYMBOLSKCASK nots Calibrated Airspeed is indicated airspeedcorrected for position and instrument error andexpressed in knots.