Piper Cherokee SIX 300 Guida rapida alla configurazione

CHEROKEE

SIX

3OO

INFORMATION

MANUAL

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a1h"{o CHEROKEE

SIX3OO

\/'

af j- INFORMATION

--/ MANUAL

Cherokee

Six 3OO

PA-32-300

HANDBOOKPARTNO.

761

-559

A complete or partial replacement of this manual, Part No.

61 559,

may beobtained

only from Piper

Customer

Services.

Publishedby

PUBLICATIONS

DEPARTMENT

Piper

AircraftCorporation

761

5s9

Issued:

July1973

APPLICABILITY

The

aircraft

serial

numbereligibility

bracket

for application

of this

manual

32-7aa0001

rhrough

32-7640130.

Thespecific

application

of this

manual

islimited

to thePiper

PA-32-300

modelairplane

designatedby

serialnumber

andregistration

numberon

thebackofthetitle

page

of this

manual.

This

manualcannotbe

usedfor operational

purposes

unlesskeptin acurrent

status.

REVISIONS

Theinformationcompiledin the

Pilot'sOperatingManual

will bekeptcurrent

by revisions

distributed

to the

airplane

owners.

Revision

material will consist

of information necessary

to updatethe text of the present

manual

and/orto add

informationto coveraddedairplaneequipment.

I. Revisions

Revisionswill be distributedwhenevernecessary

as completepagereplacementsor

additionsand strall

beinsertedinto themanualin accordance

with theinstructions

given

below:

l. Revision

pages

will replace

onlypages

with thesamepage

number.

2. Insert

all additional

pages

in proper

numerical

orderwithin eachsection.

3. Pagenumbersfollowedby a smalllettershall

beinsertedin direct

sequence

withthe

same

common

numbered

page.

II. Identificationof Revised

Material

Revised

text and

illustrations

shall

beindicatedby ablackvertical

linealongtheleft hand

margrn

of the page,

oppositerevised,

addedor deleted

material.

A line oppositethe page

number or sectiontitle and printing date, will indicatethat.the text or illustrationwas

unchangedbut materialwasrelocatedto adifferent page

or that anentire

page

was

added.

Black

lines

will indicateonly current

revisions

with changesandadditions

to ordeletions

of existing

text and

illustrations.

Changesin capitalization,spelling,

punctuation

or thephysical

locationof material

onapage

will notbeidentified

by symbols.

III. OriginalPagesIssued

Theoriginal

pages

issuedfor thismanual

prior to revision

are

given

below:

l-l through

14,2-1 through

2-19,3-l through

3-18,

4-l through

+7,5-1 through5-30,

7-l through7-12,8-lthrough8-2,9-l through

9-12,

lGl through10-15.

ltr

TABLE

(lF

C(II{TEI{TS

GE}IERAISPECIFICATIO}IS

DESCRIPTI(I}I

.AIRPLAIIEA}ID

SYSTEMS

AIRPLA]IE

FUGHIMAIIUAI

T.A.A.

APPR(IYED

EilIERGE}ICY

PROCEDffiES

I.A.A.

APPROYEII

EMERGENCY

PROCEDURES

ITHGHT

A}ID

BAtAilCE

L(lADtitG

lilsTRucn(Iils

OPERATINO

INSTRIICTIONS

(lPilATING

TIPS

PERF(IRMAIICE

CHARTS

HAilDLI}IG

A}IDSERYICING

GEltERAt

SPECtHCATt0ItS

Performance l-l

Weights l-2

Power

Plant . 1-2

Fueland

Oil . . l-2

BaggageArea l-2

Dimensions l-3

Landing

Gear l-3

3-View l-4

CHEROKEE

SIX.3OO

GENERALSPECIFICATIONS

PERFORMANCE

Publishedftguresare for standard

airplanes

flown at gross

weight under standard

:c;rditions

at sea

levelunless

otherwisestated.Performance

for a specificairplane

mayvary

;rom published

figures

depending

upon the equipment

installed,

the conditions

of engines,

airplane

and equipment,atmosphericconditions

and piloting technique.

Each

performance

figure

below

issubject

to thesame

conditionsas

onthecorresponding

performance

chart

from

which

it istaken

in the

Performance

Charts

Section.

GROSS

I{EIGHTS 3400 2900

TakeoffGroundRun,l0 o

flaps,

sea

level

(ft) 1050 7

TakeoffDistanceOver

5Gft Obstacle,

l0 o

flaps,

sealevel

(ft) I500 I200

BestRate

ofClimbSpeed

(mpnl 105 100

Rateof Climb

(ft per

min) 1050 1350

Best

Angle

of Climb

Speed

(mph) 95

Max

Speed,sealevel

(mph) l?4* 175*

Max

Speed

Optimum

Altitude,8,300

ft,757o

power(TAS)

(mph) 168* l7l*

Service

Ceiline

(ft) 16,250 20,000

Absolute

Ceiling

(ft) 18,000 21.500

CruiseSpeed

atBestPowerMixture

(mph)

657o

Power,

I1,500ft

55%

power,

15,000

RangeatBest

Power

Mixture

(mi1**

power,

8,000

657o

power,

I 1,500

55%

power,

15,000ft

Cruise

Speed

atBest

Economy

Mixture

(mph)

757o

power,

8,000

657o

power,

I 1,400

5570

power,

15,000ft

Range

atBest

Economy

Mixture

(mi;**

power,

8,000ft

657o

power,

I 1,400

55%

power,

15,000

StallingSpeed,flaps

down,

(CAS)

(mph)

Stalling

Speed,flaps

up,

(CAS)

(mph)

LandingRoll,flaps

down,sea

level

(ft)

LandingDistance

Over5&ft Obstacle,

sea

level

(ft)

*The speedstatediswith optionalwheel

fairings

installed.

Subtract

3mph

not installed.

**No reserve.

GEMRAL SPECIFICATIONS

ISSUED:JULY 12,1973

t63

155 t67

163

780 779

845 850

905 935

t66 169

159 165

149 t57

850 865

945 980

1030 1080

63 s8

7r 66

630 540

1000 850

if wheel fairings are

1-1

CHEROKEE

SIX.3OO

GROSS

WEIGHTS

Standard

Empty

Weieht

(lbs)

Maximum

Useful

Load

(lbs)

POWER

PLANT

Engine.Lycoming

Rated

Horsepower

Rated

Speed

(rpm)

Bore

(inches)

Stroke

(inches)

Displacement

(cubic

inches)

Compression

Ratio

Dry Weight

(pounds)

'' Propeller (Standard)

(Optional)*

PropellerDiameter

(inches)

(Standard)

(Optional)

FUEL AND OIL

FuelCapacity

(inboard)(U.S.

gal)

WithStandard

Auxiliary(U.S.

gal)

Oil Capacity

(U.S.

qts)

Fuel,

AviationGrade

(minoctane)

BAGGAGE

MaximumBaggage

(lbs)

BaggageSpace

(cubicft)

Baggage

DoorSize

(in.)

*Serial

nos.

7440001

3400 2900

t824

1516

(Serial

nos.7440O0

1through7

4Q06

and 764.046:7

through

76400',7r)rO-s4GKlAs

(serial

nos.

7640066,7640072

and

up)

IO-54SKlG5

300

2700

).lz)

4.3',15

541.5

8'7:

45'l

HC-C2YK-I

( )|847

s-4

orHC{2YK-r( )

|8475D-4

orHC-C2YK-I

( )F/F847

5D-4

HC{2YK-I( )/847sR4

orHC{2YK-I( )F/F8475R-0

1824

to16

100/l

Forward

100

16x22

GENERAL SPECMCATIONS

REVISED:FEBRUARY 2, 1916

Aft

100

thru7540188only

CHEROKEE

SD(-3OO

.ll

ir DIMENSIONS

WingSpan

(ft)

Wing

Area

(sqft)

WingLoading(lbs persqft)

Length(ft)

Height (ft)

PowerLoading(lbs) per hp)

LANDING GEAR

Wheel

Base

(ft)

Wheel

Tread

(ft)

TirePressure

(lbs)

GENERAL SPECIFICATIONS

ISSUED:

JULY l2,t97g

Nose

Main

32.8

4.5

19.5

27.7

8.2

I1.3

7.8

10.6

28-30

35-40

1-3

CHEROKEE

SIX.3OO

32'8.t5"

I ,,0.,r'

GENERAL SPECIFICATIONS

ISSUED:

JULY 12.1973

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