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i I i t,.tl~:'~1! I

SPECIFICATIONS

SPEED:

MaximumatSeaLevel...............

reserveat45%power.

80%powerat6000Ft....

49GallonsUsableFuel

MaximumRangeat10,000Ft

49GallonsUsableFuel

RATEOFCLIMBATSEALEVEL

SERVICECEILING.....

TAKEOFFPERFORMANCE:IIiiI1,1

Rangl'

TimeI'

,r'I n',IIt\1111Range

Time.JIIIII>1ill

1II

LANDINGPERFORMANCE:GroundRoll...........

TotalDistanceOver50-FtObstacle

8TALLSPEED(CAS):FlapsUp,powerOff..

FlapsDown,powerOff.

MAXIMUMWEIGHT....

STANDARDEMPTYWEIGHT:

HawkXP.

HawkXPII.

MAXIMUMUSEFULLOAD:

HawkXP.

HawkXPII.

\lAGGAGEALLOWANCE.

WINGLOADING:pounds/SqFt

1'(lWERLOADING:pounds/HP

I"\IKLCAPACITY:Total.

l".III

IIttII

'11'1II ':1HIII i1•. ;II

1'1I,llI

')-4/91•I'"

PILOT'SOPERATINGHANDBOOK

Ce~a@

HAWKXP1977MODELR172K3

I/4 5'I lI )1 r»

SerialNo.lS17:.-t~33.')

RegistrationNo.;1I9{18/11\

BYCARPART3FURNISHEDTOTHEPILOT

CESSNAAiRCR'AFij~OMPANY

WICHITA,KANSAS,USA

CON(:IU\,\,UI.ATIONSCESflll/\

MODELR177,1'

CONGRATULATIONS.···

workmanship.

CessnaAircraftCompany.I

ateveryCessnaDealer. \CI':S:.,NA

TABLEOFCONTENTS

SECTION

CENERAL

LIMITATIONS

EMERCENCYPROCEDURES

NORMALPROCEDURES

PERFORMANCE

WEleHT&BALANCE/

EQUIPMENTLIST....1

2 3 4 5

AIRPLA~,IE(~SYSTEMS

DESCRIPTIONS..

HANDLINe

6(/vtAIN1!ENANCE

('1';:.:,I1\

IVI

GI';NI';IU\I,

SECTION1

GENERAL

ThreeView

Introduction

DescriptiveData

Engine

Propeller

Fuel..

Oil

MaximumCertificatedWeights

StandardAirplaneWeights..

CabinandEntryDimensions

BaggageSpaceandEntryDimensions

SpecificLoadings.

Symbols,AbbreviationsandTerminology

GeneralAirspeedTerminologyandSymbols

MeteorologicalTerminology.

EnginePowerTerminology........

WeightandBalanceTerminology.....1-2

1-3 1-3 1-3 1-3 1-3 1-4 1-4 1-5 1-5 1-5 1-5y!

1-6,;;

1-6I 1-6 1-7 1-7

1-8TABLEOFCONTENTS

Page 1-( /fi

SECTION1

GENERAL<'I'::;:;N/\

1\1<,1.1':1.ItI'/:~I~Cl';:-;:-;NJ\

MODELR172K~;l':(:'1'1()N1

C:I';NI';HJ\I,

INTRODUCTION

andterminologycommonlyused.

DESCRIPTIVEDATA,II

II

ENGINE

.I

INumberofEngines:1.

EngineManufacturer:TeledyneContinental.

EngineModelNumber:IO-360-K.

placement.

PROPELLER

PropellerModelNumber:2A34C203/90DCA-14.

NumberofBlades:2.

PropellerDiameter,Maximum:76inches.

Minimum:74.5inches.

tion). FUEL

ApprovedFuelGrades(andColors):

100LLGradeAviationFuel(Blue).

TotalCapacity:52gallons.

TotalCapacityEachTank:26gallons.

TotalUsable:49gallons.III

II l'j'

NOTES:

1.Wingspanshownwithstrobe

lightsinstalled.

2.Maximumheightshownwith

nosegeardepressed,alltiresand nosestrutproperlyinflated,and flashingbeaconinstalled.

3.WheelbaselengthisG5"

4.Propellergroundclearanceis103/4".

5.Wingareais1}4squarefeet.

6.Minimumtunuuqradius(*pivotpoint

tooutboardwi!lCJtip)is27'51/2",

PIVOTPOif'~'f*PIVOTPOINT

1-3

Figure]

1

SECTION1

GENERALt'II::l:.N/\

1\1111'1':1,IU'/;~!{::1';(:'1'1(INI

(:I':NI':IU\I,

200lbs.Seenotebelow.

I.()I)I'f'\-'1'IIt.,111I,'Iq1111/'

NOTE OIL areas1and2is200lbs,

OilC;rad.·(::1"",I",,111,")

HawkXPII:1573Ibs..,

NOTE

STANDARDAIRPLANEWEIGHTS

MaximumUsefulLoad:

tionhasstabilized.

RecommendedViscosityForTemperatureRange:

SAE50above4°C(40°F).

HawkXPII:NormalCategory

1001Ibs.

9771bs.UtilityC_ategory

6511bs.

6271bs.

CABINANDENTRYDIMENSIONS

NOTE areillustratedinSection6. mendedforimprovedstartingincoldweather.

OilCapacity:

Sump:8Quarts.

illustratedindetailinSection6.

MAXIMUMCERTIFICATEDWEIGHTS

UtilityCategory:2200lbs.

Landing,NormalCategory:2550Ibs.

PowerLoading:13.1Ibs./hp.

1-4 1-5I

SECTION1

GENERAL

1'I1'1'::.::NA

1\Ii1111':I,I{.I'/;>,1\

SYMBOLS,ABBREVII\liONSI\NI>IIHMINOLOGY

KCAS KIAS KTAS VA VFEI \VNO V NE Vs Vs 0 Vx al.lllI'::ldll-14'.i.l,:;4~alovol, ",11,11.11<1<-;llIdI,(!lnperature. iun.v1I::t!:IJJI:lliii;controltravel. withcaution. exceededatanytime. whichtheairplaneiscontrollable. rationatthemostforwardcoutorofgr-avitv. greatestgaininaltitudeinagivenLimo. OAT

METEOROLOGICALTERMiNOLOGY

1-6

Standard

Tempera-

ture

Pressure

Altitude~;I':(;'I'\()N1

(:I':N1':1U\),

29.92inchesofmercury(1013mb).

BHP

ENGINEPOWERTERMINOLOGY

RPM

MPRevolutionsPerMinuteisenginespeed.

(Hg). consideredtobelimiting. usedinflight. sumedperhour. tion.

£isaccelerationduetogravity.Demon-

strated

Crosswind

Velocity

Usable

Fuel

Unusable

Fuel GPH NMPG g

SECTION1

GENERALCl';SSNA

MOlJI';LR172K

WEIGHTANDBALANCETERMINOLOGY

Reference

Datum

Station

Arm

Moment

Centerof

Gravity

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