TE CHEROKEESIX3OO INFORMATION MANUAL ,t il
-lqo3f,h#',,*(at4 CHEROKEESIX 3OO a1h" {o \/' af INFORMATION j- --/ MANUAL CherokeeSix 3OO PA-32-300 HANDBOOK PARTNO.
A complete or partial replacement of this manual, Part No. 7 61 559, may be obtained only from Piper Customer Services.
APPLICABILITY The aircraftserialnumbereligibilitybracketfor applicationof this manualis 32-7aa0001 The specificapplicationof this manualis limited to the Piper PA-32-300 rhrough32-7640130. designated by serialnumberand registrationnumberon the backof the title page modelairplane this manual. of This manualcannotbe usedfor operationalpurposesunlesskept in a currentstatus. REVISIONS The information compiledin the Pilot'sOperatingManualwill be kept currentby revisions distributedto the airplaneowners.
(lFC(II{TEI{TS TABLE GE}IERAI SPECIFICATIO}IS . AIRPLAIIE A}ID SYSTEMS DESCRIPTI(I}I T.A.A. FUGHI MAIIUAI APPR(IYED AIRPLA]IE I.A.A.
GElt ERAt SPECtHCATt0ItS Performance Weights PowerPlant . Fuel and Oil . .
CHEROKEESIX.3OO GENERAL SPECIFICATIONS PERFORMANCE Published ftgures are for standard airplanes flown at gross weight under standard :c;rditions at sea level unlessotherwisestated. Performancefor a specificairplanemay vary ;rom publishedfigures dependingupon the equipmentinstalled,the conditionsof engines, airplane and equipment, atmosphericconditions and piloting technique.
CHEROKEESIX.3OO GROSSWEIGHTS 3400 2900 WEIGHTS StandardEmpty Weieht(lbs) MaximumUsefulLoad (lbs) t824 1516 1824 to16 POWERPLANT Engine.Lycoming '' RatedHorsepower RatedSpeed(rpm) Bore(inches) Stroke(inches) (cubic inches) Displacement Ratio Compression Dry Weight(pounds) Propeller (Standard) (Serialnos. 7440O01 through 76 4Q065 and 7 64.046:7 through 76400',7r) rO-s4GKlAs (serialnos.7640066,7640072andup) IO-54SKlG5 300 2700 ) . lz) 4.3',15 541.
.ll CHEROKEESD(-3OO DIMENSIONS f ir Wing Span (ft) Wing Area (sq ft) Wing Loading (lbs per sq ft) Length (ft) Height (ft) Power Loading (lbs) per hp) 32 . 8 1 74 . 5 19.5 27.7 8.2 I 1.3 LANDING GEAR WheelBase(ft) WheelTread(ft) (lbs) Tire Pressure GENERAL SPECIFICATIONS ISSUED:JULY l2,t97g Nose Main 7.8 10.
CHEROKEESIX.3OO 32'8.t5" I t4 ,,0.,r' GENERAL SPECIFICATIONS ISSUED:JULY 12.
DESCRIPTI(III AIRPLAIIE AllDSYSTEI'IS . The Airplane Airframe Engineand Propeller In d u cti onS ystem LandingGear Flight Controls Fuel System ElectricalSystem VacuumSystem InstrumentPanel Pitot-StaticSystem Heatingand VentilatingSystem CabinFeatures Area Baggage Stall Warning Finish Air Conditioning PiperExternalPower 2-l 2-l 2- l .. .
CHEROKEESIX . 3OO DESCRIPTION AIRPLANE AND SYSTEMS THE AIRPLANE The PA-32-300is a six-place(seventhseat optional),single-engine, low-wing.all metal seatsgivetheairplanea widerangeof cargoandpassenger monoplane.Removable loadingoptions. andpowerfulfuelinjected300horsepowerengine. Its largecapacity,combinedwith an economical rnakesthis Cherokeea versatileairplanefor personalor commercialuse.
C H ER OK E S E IX .3 OO Theconstantspeedpropelleris a HartzellHC-C2YK-I ( )F/ F8475D-4with a diameterof 80 inches.Thepropelleris controlledby a governormountedat theleftforwardsideof thecrankcase . The governoris operatedby a cablefrom the powercontrol quadrant. The power control quadrantlocatedin the lower centerof the instrumentpanelincludes throttle,mixture.and propellercontrols.A friction lock on the right sideof thequadrantprevents creepingof the controls.In addition.
CHEROKEESIX.3OO oN sER. NOS.7640m1 AND UP, THE CONTROL KNOB MUST BE PRESSED TO THE LEFT TO CLEAR THE RETAINING GATE P R I O R T O S E L E C T I N G TH E D E S I R E DP O S I T I O N .
CHEROKEESIX.3OO LANDING GEAR All three landinggearuseCleveland6.00 x 6 wheels.The main gearhavebrakedrumsand Clevelanddouble disc hydrualic brakeassemblies. The nosewheel carriesa 6.00 x 6 four or six ply tire and the main gearuse6.00 x 6 six ply tires.All threetires aretube type. The nosegearis steerableusinga combinationof full rudder pedaltraveland brakes.The nose gearcan be tumed 24o eachside of center.
CHEROKEESIX - 3OO ;/ \ \-i-\ Main WheelAssemblv AIRPLAI{E AND SYSTEMS ISSUED:JULY 12,1973
CHEROKEE SIx.3OO Console FUGHT CONTROLS Dual controls,with a cablesystembetweenthe controlsand the surfaces,are installedas standardequipment. The horizontal tail is of the all-movableslab type (stabilator).The stabilatorprovidesextra stability and controllabilitywith lesssize,drag,and weightthan conventionaltail surfaces. An anti-servotab which also acts as a longitudinal trim tab, is located on the horizontal tail. This tail is actuatedby a control mountedon the control tunnelbetweenthe front seats.
CHEROKEESIX . 3OO FUEL SYSTEM The standardfuel capacityof the CherokeeSix is 84 gallons,all of which is usableexcept for approximatelyone pint in eachof the four tanks.The two main inboardtanks,which hold 25 gallons each, ate attachedto the wing structure with screwsand nut plates and can be removedeasily for serviceor inspection.The tip tanks are constructedof resin-impregnated and eachone holds l7 gallons.
:-'i,.r:.::. o ., :.:;ii trt n o xi! FLOW DISTRIBUTION tlt (n X FUELNOZZLES a t, () FUELINJECTOR .rJ I THROTTLE (! (A .a o U) c) (D et VENT o L EF T T IP T ANK H -u2F F ats e> LEFT MAIN TANK vt2 9rd k> cr.ru z 4va -||( N(a ' ;.
CHEROKEESIX - 3OO _\_ __= \_ \ \\.--\ =-=\--.-\- ,/-T- (A\---l;,{'4--l \\ \ tfry | )WAa v-\\-. \\ mN Lli@ s; s . .---..-.-.=----.....- Fuel Drain Lever l Fuelquantitygauges for eachof thefour tanksarelocatedin theenginel3ugeclusteron the left sideof the instrumentpanel.A fuelpressure indictorisalsoincorporatedin theenginegaugecluster. An electricfuel pump is providedfor usein caseof failure of the enginedriven pump. The electricpump operatesfrom a singleswitchand independent circuitprotector.
S rX -3 0 0 c H E R OttE E Standard electricalaccessories include the starter. the electricfuel pump, the stall warning indicator. the cigar lighter, the ammeter,and the annunciator panel*. The annunciator panel* includesalternator and low oil pressureindicator lights. When the optional gyro systemis installed,the annunciatorpanelalso includesa low vacuum indicator light. The annunciator panel lights are provided only as a warning to the pilot that a systemmay not be operatingproperly.
SIX.3OO CHE RO K E E STARTER swrTcH ALTERNATOR OUTPUT G /P i ir ,l ili STAFTTER SOLENOID \ IA BAT T ER Y ALIERNATOR i L_ _ _ __ souRc€-POWER R ELAY EN ER G T Z T N CG tR C utT _'_ _ ___!h I Alternator and starter schematic(ser. Nos. 7440oal through 744olg2) AIRPLAI{E AND SYSTEMS REYISED: JUNE 20.
CIIEROKEE SIX - 3OO t^:i 5A ( IN LIN E) STARTER swrTcH WARN LIGH T STARTER SOLENOID rl IFF EXTERNAT POWER RECEPTACLE I I _ _ _ _ollrgry3L_ ___ : 't,ASTER swrTcH : - - - - -.- - - y'i,_reanaron f ; ; r; o\/ \, \zrz-{.-ol i \,'\fff L_ _ _ _ i sounce-po souRcE-powER __gh R ELAY Eti ER C tZ [{GC | R C U | T I Alternator and Starter Schematic(Ser. Nos.
CIIEROKEE SIX - 3OO o n o J> ul az SO *q u u.t FJ :(o (o Yz oi t; l( O IJJ !z oo Circuit BreakerPanel AIRPLANE AND SYSTEMS REVISED: JULY 17.
CHEROKEESIX - 3OO VACI,JUMSYSTEM The vacuum systememployedto operatethe gyro instrumentsincludesan engine-driven dry vacuumpump, a vacuumregulatorvalve,and the tubingnecessary to completethe system. The use of a dry type vacuumpump eliminatesthe needfor an oil-air separatorand the hardwarenecessaryfor its installation. The vacuum gaugeis mounted on the right side of the instrumentpanel.The gaugeis calibrated in inches of mercury and indicates the amount of suction created by the engine-driven vacuumpump.
b.) o I iE rd F + o xFtl FI v2 X (.l) o o a g (D 5 FU 5 (D EE f>ry rF ts1 o> p3 q> ez FU 4vD {ut -.{ :.rl :FI i3 v. A I. 2. 3. 4. 5, 6. 7. 8. 9. IO. M AST ER SWIT CH ACCESSORY SWITCHES ST AL L WARNING L IGHT RADIO COM PASS CL OCK T URN INDICAT OR AIRSPEED INDT CAT OR OIRECT IONAL GYRO ART IF ICT AL HORIZ ON VERT ICAL SPEED INDICAT OR II. AL T IM ET ER 1 2 , vo R/tts r NDtcAT o R t3 . vo R/il._ s tNDT CAT OR I4 . T RANSPONOER I5 . M ARKER BEACON L IGHT S I6 . M AGNET IC COM PASS 17. ll.
CHEROKEESIX - 3OO PITOT-STATIC SYSTEM The systemsuppliesboth pitot and static pressurefor the airspeedindicator.altirneterand verticalspeedindicator(wlten installed). Pitot and static pressureare picked up by the pitot head on the bottom of the left wing. An optional heatedpitot head, which alleviatesproblemswith icing or heavy rain, is available. The switch for pitot heat is locatedon the lower left instrumentpanel.
CHEROKEE SIX - 3OO I [\ \.__ \ V 5 (F o 5.9 fiH; E; H g.
E = EF vz E3 UrF trl > " lll r) v, {< = sH I. 2. 3. .. 5. 6. ,. t. 9. IO. II. F RESH AIR INL ET DRAIN T UBE OVERHEAD VENT BLOWER BULKHEADASS€MSLY OVERHEAO F RESHAIR OU C T CABIN AIR EXHAUST F RESHAIROUT L ET OEFROSTER OUTLST CABIN HEAT OUT L ET OEF ROST ER AIR CONTR OL HEAT ERAIRCONT ROL I rnes"r,n ern I oernosren ) ,,, ----\. -/ ,, err xeereo -\,/ t /i / / (' t (D D a. , oe 4 B A (D I F. D !' a TA a o B o It F o xEJ rd v, X s { SEHIAL NOS.7Ai{XII THROUGH 7EOI88 sERIALNos.
CIIEROKEESIX - 3OO The inertia reel should be checkedby tuggingsharply on the strap. The reel will lock in place under this test and prevent the strap from extending.Under normal movement,the strap will extendand retractasrequired. BAGGAGE AREA The airplanehas two separatebaggage areas,eachwith a 100 pound capacity.An 8 cubic foot forward luggagecompartment,locatedjust aft of the fire wall, is accessiblethrough a l6 x 22 inch door on the right side of the fuselage.
CHEROKEESIX.3OO An optioncl electric blower is mounted on the aft side of the rear cabin panel.Air from the baggagearea is drawn through the evaporator by the blower and distributed through an overheadduct to individualoutletslocatedadjacentto eachoccupant. The switchesand temperaturecontrol are locatedon the lower right sideof the instrument panelin the climatecontrol centerpanel.The temperaturecontrol regulatesthe temperatureof cooling. decreases cooling;counterclockwise the cabin.
F.A.A.
FLIGHT AIRPLANE MANUAL FO R CHEROKEE SIX3OO THROUGH 32.
AIRPLAI{E FTIGHT MA}IUAL Log of Revisions 3-iii Limitations 3-t Procedures 3-7 Performance 3-9 Supplements 3-l l
CIIEROKEE SX.3OO (lFC(I}ITE]ITS TABLE Log of Revisions 3-iii SECTIONI Limitations A . E ngine:::::. : . : : . . B. Fuel C. Propeller D. PowerInstruments E. AirspeedLimitationsandAirspeedInstnrmentMarkings (CalibratedAirspeed) F. MaximumWeight G. C. G. Range H. Maneuvers I. Placards J. RearCabinDoor or RearCabinDoor and CargoDoor Removed. K. Seven-Pasenger Operation L.
CHEROKEESD(.300 SECTIONI LIMITATIONS in the operationof this airplane: ThefollowingIimitationsmustbeobserved A. ENGINE Lycomins IO'540-KIA5 (Serial nos. 7440001 through 7640A65 and 7640067 through 764007t) 2 andup) LycomingIO'54GKlG5 (Serialnos.7640066,7640A7 ENGINE LMITS For all operations2700 RPM,300HP B. FUEL 100/130minimum aviationgradefuel c. PROPELLER HartzellHC{2YK-l 18475D4or HC{2YK-I( )184754or HC{2YK-I( Low pitch stop 13.5' t .
CHEROKEESIX.3OO E. AIRSPEED LIMITATIONS AND AIRSPEED INSTRUMENT MARKINGS (Calibrated Airspeed) NEVER EXCEED MAXIMUM STRUCTURALCRUISE MANEUVERTNG FLAPS EXTENDED MAXIMUM POSITIVELOAD FACTOR MAXIMI.JMNEGATIVE LOAD FACTOR AIRSPEEDINSTRUMENTMARKINGS Red RadialLine (Never-Exceed) Yellow Arc (CautionRange) (SmoothAir Only) GreenArc (NormalOperatingRange) WhiteArc (Flap Down) 2I2MPH I68 MPH I49 MPH 125MPH 3.
CHEROKEESIX.3OO r. PLACARDS In full view of the pilot: .THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS AND MANUALS. NO ACROBATIC MANEIIVERS,INCLUDING SPINS,APPROVED.'' ..THIS AIRCRAFT APPROVEDFOR NIGHT IFR NON.ICING FLrclrT WHEN EQUTPPEDIN ACCORDANCEWITH FAR 9l oR FA R 135.
CHEROKEESIX.3OO In full view of the pilot: (For operationwith the reardoor removed) ..FOR FLIGHT WITH THE DOOR REMOVED, SEE THE LIMITATIONS AND PROCEDURES SECTIONS OF THE AIRPLANE FLIG}IT MANUAL.' On the instrumentpanelin full view of the pilot when the AutoFlite is installed: "FOR HEADING CHANGES: PRESSDISENGAGE SWITCH ON CONTROL WHEEL. CHANGE HEADING. RELEASE DISENGAGESW[TCH.'' On the fuel selectorvalve cover: *ALL WEIGHT IN EXCESS OF 3II2 POUNDS MUST BE FUEL WEIGHT ONLY. FILL TIP TANKS FIRST.
CHEROKEESD(.300 J. REAR CABIN DOOROR REAR CABIN DOORAND CARCODOORREMOVED The following limitations must be observedin the operationof this airplanewith the rear cabindoor or rear cabindoor and cargodoor removed: l. 2. 3. 4. 5. 6. The airplanemay be flown with the rear cabindoor or rear cabindoor and cargo door removed.Flight with the front door removedis not approved. Maximumspeed- 165 mph. No smoking. All loosearticlesmust be tied down and stowed.
CIIEROKEE SD(.300 SECTIONII PROCEDURES l. The stall warningsystemis inoperativewith the masterswitch off. 2. Electricfuel pump must be on for both landingand takeoff. 3. Except asnoted above,all operatingprocedures for this airplanearenormal. 4. When operating with the rear cabin door removed,it is recommendedthat all occupantswearparachutes. 5. Air conditionedModels only: Warning- the air conditionermust be off to insure n ormal takeoff performance. 6.
SIX.3OO CTTEROKEE d. Exryninethe contentsof the containerplacedunder the fuel sump drain outlet for waterand sedimentand disposeof the contents. CAUTION Whendrainingany amountof fuel, careshouldbe taken to insure that no fire hazardexistsbeforestartingengine. After using the under-seatquick drain, it should be checkedfrom outsideto makesureit hasclosedcompletelyand is not leaking.
CREROKEESIX.3OO SECTION Itr PERFORMAI{CE AII performanceis givenfor a weight of 3400 pounds. Loss of altitude during stallscan be as great as 350 feet, dependingon configurationand power.
CHEROKEESD(.300 SECTIONry OPTIONAL EQUIPMENT NOTE THE INFORMATION CONTAINED IN THIS SECTION APPLIESWHEN THE RELATED EQUIPMENTIS INSTALLED IN THE AIRCRAFT. A. Electric Pitch Trim Installation B. AutoFlite II Installation C. Air ConditionerInstallation D. Piper AutoControl III and/or AutoContol IIIB Installation E.
CIIEROKEE SD(-3OO A. ELECTRrc PITCH TRIM INSTALLATION The following emergency information applies in case of electric pitch trim malfunction. l. electricpitch trim by operatingpush button In caseof malfunction,disengage panel. trim switch on instrument 2. In emergenry,electric pitch trim may be overpoweredusingmanualpitch trim. 3. In cruise configuration,malfunction results in 10" pitch changeand 50 ft altitudevariation.
CHEROKEESIX.3OO D. PIPER AUTOCONTROL Itr AI{D/OR AUTOCONTROL IIIB INSTALLATION l. LIMITATIONS a. Autopilot OFF duringtakeoff and landing. b. Autopilot useprohibitedabove180 MPH CAS. 1 PROCEDURES a. PREFLIGHT ( l) Roll Section (a) Place Radio Coupler in "Heading" mode and place A/P ON/OFF switch in the "ON" positionto engageroll section. Rotate roll command knob Left and Right and observe conbol wheel describesa correspondingLeft and Right turn, then centerknob. (b) Set proper'D.G.Headingon D.G.
CHEROKEESIX.3OO (4) voR (a) To Intercept: l. Using OMNI Bearing Selector,dial desiredcourse, inboundor outbound. 2. Setidenticalheadingon CourseSelectorD.G. 3. After aircraft has stabilized,position coupler mode selector knob to OMNI mode. As aircraft nears selectedradial, interception and crosswindcorrection will be automatically accomplishedwithout further switching. NOTE If aircraft position is lessthan 45o from selectedradial, aircraft will intercept before station.
CHEROKEESIX. 3OO NOTE For precise tracking over OMNI station, without "S" tum, position coupler mode selector to HDG mode just prior to station passage.If holding pattern is desired,position coupler mode selector to HDG mode at station passageinbound and selectoutbound headingin directionof turn. After elapsedtime, dial inbound course on Course Selector D.G. When aircraft headingis 45o to radial,positioncouplermodeselectorto OMNI mode.
CIIEROKEESIX.3OO C. 3. EMERGENCYOPERATION ( I ) In an emergencythe AutoControl can be disconnected by placingthe A/P ON/OFF switchto the "OFF" position. (2) The AutoControl can be overpoweredat either control wheel. (3) An Autopilot runaway, with a 3 seconddelay in the initiation of recovery,wfule operatingin a climb, cruiseor descending flight could resultin a 38" bank and 40 foot altitudeloss.
PR0CEIIURES EtrlERGEllCY Introduction EnginePower LossDuring Takeoff EnginePowerLossIn Flight PowerOff Landing . . . PropellerOverspeed Spins .
SD(.300 CAEROKEE EMER,GENCYPROCEDURES INTRODUCTION This sectioncontainsproceduresthat are recomrnended if an emergencyconditionshould occur during ground operation, takeoff, or in flight. Theseproceduresare zuggested as the best courseof action for coping with the particular condition described,but are not a substitutefor soundjudgmentand commonsense.Sinceemergencies rarely happenin modernaircraft,their occuren@ is usuallyunexpected,and the best correctiveaction may not'alwaysbe obvious.
CHEROKEESIX . 3OO ENGINE POWERI,oSS IN FIIGHT Completeenginepower los is usually causedby fuel flow intemrption, and power will be restoredshortly after fuel flow is restored.If power loss occursat low altitude, the first step is to preparefor an emergencylanding(SeePOWEROFF LANDING). Maintainan airspeedof at least100 MPH IAS, and if altitudepermits,proceedasfollows: l. Fuel Selector- Switchto anothertank containingfuel. 2. Electric Fuel hrmp - On 3. Mixture - Rich 4. AlternateAir - On 5.
CHEROKEESIX - 3OO POWEROFF LANDING If lossof power occursat altitude, trim the aircraft for bestgliding angle(100 MPH IAS, Air Cond. - OFF), and look for a suitablefield. If measurestaken to restorepower are not effective,and if time permits,checkyour chartsfor airportsin the immediatevicinity;it may be possibleto land at one if you have sufficient altitude.
CHEROKEE SIX.3OO SPINS Intentional spins are prohibited in this aircraft. If a spin is inadvertently entered, immediatelyusethe following recoveryprocedures: I. THROTTLE. IDLE 2. RUDDER . FULL OPPOSITETO DIRECTIONOF ROTATION 3. CONTROLWHEEL. FULL FORWARD 4. RUDDER. NEUTRAL (WHEN ROTATION STOPS) 5. CONTROL WHEEL - AS REQUTREDTO SMOOTHLYREGATNLEVEL FLrcH'r ATTITUDE OPENDOOR The cabin door on the Cherokeeis double latched,so the chancesof its springingopenin flight at both the top and bottom are remote.
CHEROKEESIX.3OO FIRE The presenceof fire is noted through smoke,smell,and heat in the cabin.It is essential that the sourceof the fire be promptly identified through instrument readings,characterof the smoke,or other indications,sincethe action to be takendifferssomewhatin eachcase. SOURCEOF FIRE . CHECK t. ElectricalFire (Smokein Cabin): a. MasterSwitch- Off b. Vents - Open c. CabinHeat- Off d. Land assoonaspossible. ) EngineFhe (In Flight): a. Fuel Selector- Off b. Throttle - Closed c.
CHEROKEESIX - 3OO LOSSOF OIL PRESSURE Loss of oil pressuremay be eitherpartial or complete.A partiallossof oil pressureusually indicatesa malfunction in the oil pressureregulatingsystem,and a landing should be made as soon aspossibleto investigatethe causeand preventenginedamage. A complete loss of oil pressureindication may signify oil exhaustionor may be the result of a faulty gauge.In either case,proceed toward the nearestairport, and be preparedfor a forced landing.
CHEROKEESIX - 3OO ALTERNATOR FAILURE Loss of alternator output is detected through zero reading on the ammeter. Before executing the fotlowing procedure, insure that the reading is zero and not merely low by actuating an electrically powered device, such as the landing light. If no increasein the ammeter reading is noted, alternator failure can be assumed. ReduceElectrical Load. ,, l. 2. Alternator Circuit Breakers- Check "Alt" Switch - Off (for I second), then On 3.
AND BALANCE WEIGHT FO R stx300 CHEROKEE APPLICABLE TO SERIAL NUMBERS 32-744OOOI THROUGH 32-7640130 ISSUED:MAY 14, 1973 REYISED:'MARCH 23.
WEIGHT AIIDBAIA}ICE Log of Revisions 5-iii Weight and Balance 5-l Weight and BalanceData - Weighing Procedure 5-3 Weight and BalanceData 5-7 C. G.
CHEROKEESIX.3OO WEIGHT AND BALANCE In order to achievethe performance,safety and good flying characteristicswhich are designedinto the airplane,it must be flown with the weiglrt and center of gravity (C.G.) position wthin the approvedenvelope.The aircraft offers a tremendousflexibility of loading. full fuel However,you cannot fill the airplane,with the maximum numberof adult passengers, With the flexibility comesresponsibility.The pilot must ensure tanks and maximum baggage.
CHEROKEESIX.3OO WEIGIIT AND BALANCE DATA WEIGIIING PROCEDURE At the time of delivery,PiperAircraft Corporationprovideseachairplanewith the licensed empty weight and center of gravity location. This datais on Page5-7. The removal or addition of an excessiveamount of equipment or excessiveairplane modificationscan affect the licensedempty weight and empty weight centerof gravity.The following is a weighingprocedurcto determinethis licensedempty weightand centerof gravity location: I. PREPARATION a.
CHEROKEESD(.300 3. WEIGHING. AIRPLANE EMPry WETGHT a' lVith the ailplane level and brakes released,record the weight shown on each scale.Deduct the tare, if any, from each reading. ScalePositionand Symbol Nose\Yheel (N) Right'Main.Wheel (R)" Left Main Wheel (L) Airplane Empty Weight,asWeighed(T) 4. EMPTYWEIGHTCENTEROF GRAVITY a. The following geometry appliesto the PA-32-300airplanewhen airplaneis level(SeeItem 2). 24il i illl {t #' -,-q6r.
CHEROKEESD(.300 b. Obtain measurement"A" by measuringfrom a plumb bob droppedfrom the wing leading edge, at the intersectionof the straieht and tapered section, horizontally and parallel to the airplane centerline, to the main wheelcenterline. Obtain measurement'oB" by measuringthe distancefrom the main wheel centerline,horizontallyand parallelto the airplanecenterline,to eachside the measurements. of the nosewheelaxle.Then average d.
CHEROKEESIX.3OO WEIGIIT AND BALANCE DATA MODEL PA-32.300CHEROKEE AirplaneSerialNumber RegistrationNumber Date AIRPLANE BASTCWEIGHT Weight (Lbs) Item C. G. Arm (InchesAft of Datum) X Moment (In-Lbs) Actual Computed *Empty Weight UnusableFuel (3.2 pints) 2.3 103.0 237 22.5 r6.6 374 StandardEmpty Weight OptionalEquipment LicensedEmpty Weight Oil ( 12 quarts) BasicWeight *Empty weight is defined as dry empty weight (including paint and hydraulic fluid) plus 2.4lbs undrainableengineoil.
CHEROKEESIX.3OO C. G. RANGE AND WEIGHT INSTRUCTIONS l. Add the weightof all itemsto be loadedto the basicweight. 2. Use the loadinggraphto determinethe moment of all items to be carriedin the airplane. 3. Add the momentof all itemsto be loadedto the basicweightmoment. 4. Divide the total moment.bythe total weightto determinethe C.G,-location-; 5. By using the figuresof ltem I and Item 4, locate a point on the C.G. rangeand weight graph.tf the point falls within the C.G.
EHEROKEESD(.300 LOADINGGRAPH ..c\) D( ."l o+ -19\ \e,2 t f) ,.4i ad 450 -t ^1Q
CHEROIGE SIX.3OO C. G . RA NG EA ND WE I G HT 3400 \ 3(x)0 / / ::. 8'u '2 ffi Z rl I oi c = :': / F T (9 E zzoo = 1800 1400 r8 0 828/.
(lPE RATI}IG I}ISTRU CTI(I}I S Preflight Starting Engine Starting EngineWhenCold Starting EngineWhenHot . StartingEngineWhenFlooded StartingWith ExtemalPowerSource Warm-Up GroundCheck Takeoff Climb Stalls . Cruising Turbulent Air Operation Maneuvers Approachand Landing . . StoppingEngine Air sp eedData.
CHEROKEESIX - 3OO OPERATING IN STRUCTIONS PREFLIGHT The airplane should be given a thorough preflight and walk-aroundinspection.The preflight shouldinclude a checkof the airplane'soperationalstatus,computationof weightand C.G. limits, takeoff distance,and in flight performance.A weatherbriefingshouldbe obtained for the intended fliglrt path, and any other factors relatingto a safeflight should be checked beforetakeoff. Walk-AroundInspection I. a. Releaseseatbeltssecuringthe control wheel. b.
CHEROKEESIX - 3OO 4. 5. 6. 7. c. a. Checknavigationlights. Visuallycheckmain fuel tank fuel supply;securecaps. Drain main fuel tank sumps(SeeDescription- Airplaneand SystemsSectionfor "b. procedure). c. Checkthat fuel systemventsareopen. d. Checkmain gearshockstrutsfor properinflation (4-l12 inches). e. Checktires for cuts,wear,and properinflation. f. Checkbrakeblocksfor wearand damage. g. On left wing checkpitot head:Removecoverif used;checkthat holesareclear. a. Checkwindshieldfor cleanliness. b.
CHEROKEESIX - 3OO STARTINGENGINEWHEN HOT l. 2. 3. 4. 5. Openthe throttle approximatelyl/2 inch. Turn the masterswitchON. Turn the auxiliaryelectricfuel pump ON. Mixture control in IDLE CUTOFF. Engagethe starter by rotating the magnetoswitch clockwise and pressing in. When the enginefires, releasethe magnetoswitch;advance the mixture: move the throttle to the desiredsetting. STARTINGENGINEWHENFLOODED I. 2. 3. 4. 5. Openthe throttle full. Turn the masterswitchON. Turn the auxiliaryelectricfuel pump OFF.
CHEROKEESD(.300 WARM-UP Warm-upthe engineat 1000 to 1200 RPM. Avoid prolongedidling at low RPM, as this practicemay resultin fouled sparkplugs. Takeoff may be madeassoonasthe groundcheckis completed,providedthat the throttle may be openedfully without backfiring or skipping,and without a reduction in engineoil pressure. Do not operatethe engineat high RPMwhenrunningup or taxiing overgroundcontaining loosestones,gravelor any loosematerialthat may causedamageto the propellerblades.
CHEROKEESIX - 3OO TAKEOFF Just beforetakeoff the following itemsshouldbe checked: l. Fuelon propertank 2. Electricfuel pump on 3. Enginegaugeschecked 4. Alternate air closed 5. Mixture set 6. Propellerset 7. Seatbackserect 8. Fastenbelts/harness 9. Empty seats- seatbeltssnuglyfastened I 0. Flapsl0' ( I st notch) I l. Trim tab set 12. Controlsfree 13. DoorslatchOd L4. Air conditioneroff The takeoff techniqueis conventionalfor the CherokeeSix.
CHEROKEESIX - 3OO CLIMB The best rate of climb at grossweight will be obtainedat 105 miles per hour. The best angleof climb may be obtainedat 95 milesper hour. At lighterthangrossweightthesespeeds are reducedsomewhat.*For climbingen route,a speedof I l5 milesper hour is recommended. This will producebetter forward speedand increasedvisibility over the noseduring the climb. Whenreachingthe desiredaltitude,the electricfuel pump may be turned off.
CHEROKEESIX - 3OO Use of the mixture control in cruising flight reducesfuel consumptionsignificantly, especiallyat higher altitudes.The mixture should be leanedduring cruisingoperationabove 5000 feet altitude and at pilot's discretionat lower altitudeswhen 757opower or lessis being used.If any doubt existsas to the amountof power beingused,the mixture shouldbe in the FULL RICH positionfor all operationsunder 5000 feet.
l.|$|li|]li|ll||]L||]l|l1!11jlll|{ll|llilJl|Nl$llflffiIflffiI CHEROKEESIX.3OO TURBULENT AIR OPERATION In keepingwith good operatingpracticeusedin all aircraft, it is recommendedthat when turbulent air is encounteredor expected,the airspeedbe reducedto maneuveringspeedto reducethe structuralloadscausedby gustsand to allow for inadvertentspeedbuild-upswhich may occurasa resultof the turbulenceor of distractionscausedby the conditions. MANEUVERS Intentional spins are prohibited in this airplane.
CHEROKEESIX - 3OO STOPPING ENGINE At the pilot's discretion, the flaps should be raised and the electric fuel pump turned off. After parking, the air conditioner and radios should be turned off, the propeller set in the full increaseposition, and the engine stopped by disengagingthe mixture control lock* and pulling the mixture control out to idle cutoff. The throttle should be left full aft to avoid engine vibration while stopping.
CHEROI(EEsrx- 300 Air ConditionerControls AIR CONDITIONING'T To operatethe air conditioning systemeither on the ground or in flight: I. Start the engine. 2. Turn the air conditioningMasterSwitchto "ON." 3. Turn "TEMP" control to desiredtemperature.Clockwiserotation increasescooling. 4. Selectdesired"FAN" position,"LOW," "MED' or "HIGH." AIR CONDITIONER OPERATIONAL CIIESK PROCEDURE Prior to takeoff the air conditionershouldbe checkedfor properoperationas follows: l. CheckaircraftMasterSwitchON. 2.
CHEROKEESIX - 3OO tf the "Air Cond. Door Open" light does not respondas specifiedabove,an air conditioner system or indicator bulb malfunction is indicated, and further investigationshouldbe conductedprior to flight. The above operationalcheck may be performed during fliglrt if an in flight failure is suspected. 5. AIR CONDITIONER EFFECTSON AIRPLAT.IEPERFORMANCE Operationof the air conditionerwill causeslightdecreases in cruisespeedand range.
CHEROKEESIX.3OO The unit is equipped with a portable antenna to allow the locator to be removed from the airplane in caseof an emerpncy and used as a portable signal transmitter. A pilot's remote switch, located on the left side panel, is provided to allow thc transmittcr to be controlled from inside the cabin. l. On somemodelsthe pilot'sremoteswitchhasflrreepositionsand is placarded"ON," "AUTO/ARM," and "OFFIRESET." The switch is normally left in the "AUTO/ARM" position.
(IPERATII{G TIPS OperatingTips g_I
CHEROKEESIX.3OO OPERATING TIPS The following OperatingTips are of particular value in the operation of the Cherokee PA-32-300. l. Learn to trim for takeoff so that only a very light back pressureon the wheel is requiredto lift the airplaneoff the ground. 2 . The best speedfor takeoff is about 70 MPH undernormal conditions.Trying to pull the controllabilityof the the airplaneoff the ground at too low an airspeeddecreases airplanein event of enginefailure. up to 125MPH. To reduceflap operatingloads,it 3 .
CHEROKEESIX - 3OO 8. The shape of the wing fuel tanks is such that in certain maneuversthe fuel may move away from the tank outlet. If the ouflet is uncovered, the fuel flow will be itrterrupted and a temporary loss of power may result. Pilots can prevent inadvertent uncovering of the outlet by avoiding maneuvers which could result in uncovering the outlet. Extreme running turning takeoffs should be avoided as fuel flow interruption may occur.
PERF(|R}IA}ICE CHARTS Altitude ConversionChart Takeoff Performance(Flaps l0' ) Takeoff Performane (Flaps25" ) Climb Performance CruisePerformance CruisePerformance - Range(3400 Lbs GrossWt) CruisePerformance - Range(2900 Lbs GrossWt) >- L Glide Performan@ Stalling Speedvs Weight Stalling Speedvs Angle of Bank 9-8 9-9 9- l0 LandingPerformane PowerSettingTable 9-t2 9-2 9-3 9-4 9-5 9-6 9-7 9-lI
CIIEROKEE SIX - 3OO PA-32-300 CHEROKEE SIX llllllllll l GHART CONVERSUON ALTUTUDE Ttl BEUSED THIS CHART SHtlUTIl DETER}IIIIE DI}ISIW ALTITUDE TEHPERATURE M(lil EXISTIIIG ATTITUI|T AIII!PRESSURE C(III|IITI(I]IS PTRf(IRIIAIICE I(lRUSE ITITII CHARTS. 2t000 20000 STD. .$sil TEii'\ F \ l.| 16000 EI E F \@ > 12000 \iF9- v, Ll EI - \ 8000 <_ ,7 ; t000 = T \rup + I I st .{0 -20 0 s.$l 20 \@ \ ..db\ v f0 E0 80 100 TETPERATURE.
CHEROKEESIX.3OO PA-32-300 CHEROKEE SIX TAKE@FF PERFORMANGE ' 1.2Ys TAKE0FF SPEED FLIPS t0' _ RU]IIIAY tEVEtDRY PAVEI| zER0 wtilo -i I REI.EASE BTT(IRT FULIPIIIVER BRAKE (lFCHART T(tO(l FT.IS IIIYAIID AB(IYE TXTRAP(ITATIOII 6000 - l! r*l EI = E 5ooo 6 looo H - 3400lBS. - 2s00LBs. r000 2000 3000 {000 DISTAIICE TAfG-0FF lFT.l NOTE: SEE SECTION7 FOR EFFECTSOF AIR CONDITIONING INSTALLATIONON PERFORMANCE, 9-2 PERTORMANCE CIIARTS REIIISED: IUNE 2n.
CHEROKEESIX.3OO PA-32-300 CHEROKEE SIX TAKE@FF PERFORMANCE SPEED TATE0FF 1.2Ys FIAPS 25' TEYET RU}ITIAY PAYED DRY zER(l wlllD BRAI(E RTTEASE BET(IRE FUttPIIYIER (lT CHART T(lO(lTT.ISIIIYAI.III EXTRAP(II.ATIOII AB()YE - 0000 lr r{ EI 5000 E <' > F aat 3400 [BS. - 2900 tBs, Ei -, iooo 1000 5000 TAfG.ort DtsTAr{cE lFT.l *o"',t*?liJl'i^lJSi.t^'.'ot-T:nff..^'*coNDrrroNrNG PERFORI\.TANCE CHARTS REVISED:JUNE 20.
CITEROKEE SD( .3OO PA-32-300 CHEROKEE SIX _GLIMtsPERF@RMANCE n I 18000 r0' FIAPS I r05ilPHCAS _l GR(ISS 3400 v{EtcilT I LBS. . TUttTHROIII.E I POWER l.Y0(lil]rctlrslRUCTr(l l{s il IXTURE - ttAlrPER \ r6 0 0 0 \ rf0 0 0 \ ll \ - t2000 uIEIGHI@2rt00t BS \ lr RAII:0tcutBI351 I TPil |iT UTE B2r,500 r8s0r. GEILIII, ,-,tt = \ tn n n n \ ll d \ H sooo - \ \ 6000 \ \ 1 00 0 \ 20[l \ \ 200 100 600 800 t000 1200 tlil.l RATE 0t CutEltl.
CHEROKEESIX - 3OO PA-32-300 SIX CHEROKEE PERF@RMANGE GRUISE - TRUEAORSPEED iltSTALtED w}|tEttAtRH0S BTST P()I{ER lilxTuRE - tEAllPER tyc0il|rotilsTRucTt0l{s ll0 T t :S UB T RA3CT t P t l lF t rHrrt F A I RHG AS Rt IIl)I IItSTAtLED. rBs. 3100 2900LBS. t{ + Ll 8000 a t1 ; 6000 U7 t^l EI - 130 r10 !50 160 t70 t80 TRUE ATRSPETOIIPH NOTE: SEE SECTION7 FOR EFFECTSOF AIR CONDITIONING INSTALLATTONON PERFORMANCE.
CHEROKEESIX.3OO PA-32-300 CHEROKEE SIX eRt0sI PEtsF@tsMANGE -,R4N( E fiHcllr 3400 Poulros GR(lss I rurr i81cAL. T0TAr fAtRmGS HSTALLED : ITHEEL l-- BEST ECoil0rY I I ltlXTUR E- ttAlrPtRtyc0iilltctilsTRucTt(ll s I r lt lll !- PERCElII APPRllx. RATTIl OPH P(lY{ER 75 7A 65 60 55 FlF | 8.0 14.8 I 3.8 12.7 il.9 RESEIYE 'Ill $il. RESE 15 RYEA I 557oP0|Ytl rl_ lt I 6000 l l l i l *r 12000 r_ r.l Q. l*l GI a I .
CHEROKEESIX - 3OO PA-32-300 SIX CHEROKEE PERFORMANGE GRU0sE - RANGE 2900P0ult0sGR0ss TYHG]|T 84 GAt.T(ITAL FUEL FAIRITIGS YTHTET IIISTIILEO BEST EC(III(ITY rGTtul ill I rulrt - rtAil t,Ht LYuuiililEHSTBI ts ttttl PERCTIIT RATEO IPPR()X. SPlf P0rf tR 75 r6.0 t1.8 70 t 3.8 65 12.1 60 il.9 55 lIORESERYE AT55%P0V{ER 15 iltil. RISERVI r6000 3/ r lrtlI ,?l I l4l + r2ooo .oo/ r4l e a -l 'r -s c.< > u|t rR Q 13, 8000 Ll -EI 1000 e - l R/ slt e* l l I 700 I I I , o.
CHEROKEE SIX.3OO PA-32-300 CHEROKEE SIX I I PERFORMANGE GLODE r6000 / / t {000 / / r2000 g- / r0000 = e e / tr| ttrl / E 8000 / tal C3 l- 5 / 6000 / 3100 t8 . t00flPH / {0 0 0 2900 t8 . g0tPfi / PR0P Wlil|,ntuttc / 2000 0' tllPs . ztn0lllflll / st ttl{ / 5t0152 0 2 5 . STAIUTE 8U0t0tsTtnGE iltES NOTE: SEE SECTION7 FOR EFFECTSOF Al R CONDlTloNlNc INSTALLATIONON PEBFORMANCE. 9{ PERFORMANCE CEARTS REYISED: JLJNE20.
PA-32-300 SIX CHEROKEE llll SPEED STALLONG Vs WEIGHT P0rfrn 0rr vt c, ?0 4 I0 -6 a lr, Ll r -50 va {0 1800 2000 2200 2{00 2600 2800 3000 GR0SS WElElrT - P(|UilIlS NOTE: SEE SEcTlOfi 7 FOR EFFECTS OF AIR CONDITIONING I NSTALLATION ON PERFORMANCE.
CHEROKEESIX.3OO PA-32-300 CHEROKEE SIX SPEED STALLING Vs ANGLE@FBANK tvflGllT - 3400P0ullDs v, cr 90 r -I F80 EI L U' j 'o 70 l0 20 30 f0 50 O]BT}II( AIIBIE - DEBREES NOTE: SEE SECTION 7 FOR EFFECTSOF AIF CONOITIONING INSTALLATIONON PERFORMANCE.
CITEROKEE SIX.3OO PA-32-300 CHEROKEE SIX ttr r r r t t l _ LANDONG _ PERF@RMANCE P0ffiR ffir tuPsl0' PtYt0ttvEt|lRyRuilwty illl wtl{|l ttxttut Bnilflltc I I I E oooo I Lt a = = I 5000 v? tooo E - ,L I > E - 3100 rBs. cw rBs.Gt -- isoo r ai -Fr--€ a: l l-3,r' I I -s= € l t, €l s nI e C! -**I €1 I 2000 I | t/ I I | 000 I I r000 r200 .DtsTrlrcE ulrDilrc lrT.l NorE'iftE'lEf i,B^li""ir;?'"tr"J:"o;:'tcoNorrroNrNc PERFORMANCECHARTS REYISED: JUNE 20.
o E \o I rrl F h) o xti IT' (A S et t ing P ower T a b l e [ycoming Model l0-540-K,-[,-i l i e s3,0 0H PEn g i n e Ser Alr StdAlr Temp Feat of Press. E 6f (,l rn l eo FE ez -l t8 pO sr !E "cE {F! l.)Ut SL 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 9,000 10,000 11,000 12,000 13,000 14,000 15,000 59 55 52 48 45 4L 38 u 31 27 23 19 16 L2 9 5 Roted f65 HP - 55Vo RPMANDMAN.PRESS. 2100 2200 2300 2400 22.5 22.3 22.1 21.9 21.7 21.5 2r.3 2r.0 20.8 20.6 20.4 20.2 20.0 : 2t.8 2t-6 2L.4 21.
HA}IDLI}IG A]IDSERYICIIIG lGl tG l lGl Ground Hand!:.g To*'tng Taxiing Parkine Moonng Cleaning EngineCompartment Cleanrng CleaningLandingGear . ra-2 lO-2 lG3 l0-3 lG3 ,,,,,::::....::::,,,,,,, lfi Ei;ilili*llt*'t:gx'.:s;x.
CHEROKEESIX. 3OO HANDLING AND SERVICING This sectioncontainsinformation on preventivemaintenance.Refer to the PA-32Service Manual for furrher maintenanceprocedures.Any complex repair or modification should be b1'a PiperCertifiedSewiceCenter.
CHEROKEESIX - 3OO PARKING When parking the airplane, be sure that it is sufficiently protected from adverse weather conditions and that it presentsno dangerto other aircraft. When parking the airplanefor any lengthof time or overnight,it is suggested that it be mooredsecurely. a. To park the airplane,headit into the wind if possible. b. Set the parkingbrakeby pulling back on the brakeleverand depressing the knob on the handle.
CHEROKEESIX - 3OO CLEANING CLEANING E\Gt\E COIIPARTI1ENT Before ,--:::.-:g :l-.: :r.gine compartment,place a strip of tape on the magnetovents prevent ar.;.s:."::.i :rcr.r enteringtheseunits. to a. Pl:ce ; .ar;:: pan under the engineto catchwaste. \\'irh ;Ii: ergine cowling removed, spray or brush the engine with solvent or a b. r.liLxturecf solvent and degreaser.In order to remove especiallyheavy dirt and greas deposits,it may be necessaryto brush areas.thatwere sprayed.
CHEROKEESIX,3OO CLEANING EXTERIOR SURFACES The airplaneshouldbe washedwith a mild soapand water.Harshabrasives or alkaline soapsor detergentscould make scratcheson painted or plastic surfacesor could cause corrosionof metal. Cover areaswhere cleaningsolution could causedamage.To washthe airplane,usethe following procedure: a. Flush awayloosedirt with water. b. Apply cleaningsolution with a soft cloth, a spongeor a soft bristle brush. c.
CHEROKEESIX - 3OO CLEANING CARPETS To clean carpets,first remove loose dirt with a whisk broom or yacuum. For soiled spots and stubborn stains use a noninflammable dry cleaningfluid. Floor carpetsmay be removed and cleanedlike any householdcarpet. ENGINE AIR FILTER RemovingEngineAir Filter (SerialNos. 7440001through7540188) a. b. Removethe top cowling. The air filter is locatedon the lower left side of flre engine.Removethe thumb screwssecuringthe cover.Removethe cover,then the filter.
o o\ .'I I \ '?:'i i 'r '' \ \\ rn i 'r - \\ 7l \\ \ >./' t17 frl -/ rrt V) --"' a /4 I u) o I --''' ,7/-,. \ --'t ( ll' ) l't' t_J X 7f o )t 't-a' ,/ ,/ --'< \ -, \\... v) al /-- o )' / \--- )r / / \ z AF 22 Eo tr> ZZ k t'rl ''{r,) "t-.lS r-O Y,Z u rO -l \, I ''-t-------- \ ) \ -- tl/. //l I _-)' ---'--'' I. 2. 3. 4. 5. 6. 7. 8. 9. IO. II. I2. I3. I4.
LANDING GE.{R SER\ICE .\:-:-...:: *:.:----,. : -r. : : ri:s-x;:t -..The landrnggearsus€ C,:":--: x 6 tube b'pe.The marn gear i::: ai: t ;.'. ::--.-; a-: ---: -:s: :ar ::: i TIRE INFLATION. this Sectio:.' :=:= -*Y il[-: off rhe i;: :a:. .r.€ t-: i:,: '-:: :rit: :: : :: u-.:i Main wheelsareremovedb1'tai
CHEROKEESIX - 3OO PROPELLERSERVICE The spinner and backing plate should be cleanedand inspected for cracks frequently. Before each flight the propeller should be inspected for nicks, scratches,and corrosion. If found, they should be repairedas soon as possibleby a rated mechanic,sincea nick or scratch causesan area of increasedstresswhich can lead to seriouscracksor the lossof a propeller tip. The back face of the bladesshould be painted when necessarywith flat black paint to retard glare.
CHEROKEESIX - 3OO Fuel Drain DRAINING FIJEL VALVES AND LINES The fuel systemstrouldbe drainedbefore the first flight of the day and after refueling to avoid the accumulationof water and sediment.Each fuel tank has an individualquick drain at the lower inboard corner. A fuel strainerwith a fuel systemquick drain is located at the lowest point in the system.Each tank strouldbe drainedthrough its individual quick drain until sufficient fuel has flowed to ensurethe removalof any contaminants.
CHEROKEESIX.3OO DRAIMNG FI'EL SYSTEM The bulk of the fuel may be drainedby openingthe individualdrain on eachtank. The remaining fuel may be drained tfuough the fuel strainer. Any individual tank may be drainedby closingthe fuel selectorvalveand then drainingthe desiredtank. TIRE INFLATTON For maximum servicefrom the tires, keep them inflated to the proper pressures- 28-30 psi for the nose gearand 3540 psi for the main gear.All wheelsand tires are balancedbefore original installation,.
CHEROKEESIX.3OO Senice I.ettersdealwith product improvementsand servicehints pertainingto the aircraft. They are sent to dealersand distributorsso they canproperlyservicethe aircraftand keepit up to date with the latestchanges. Ownersshouldgive carefulattentionto the ServiceLetter information, ServiceSparesLettersoffer improvedparts,kits and optional equipmentwhich were not availableoriginallyand which may be of interestto the owner.
CHEROKEESTX- 3OO PREVENTIVE MA IN TENAI{CE The holder of a Pilot CertificateissuedunderFAR Part 6l may perform certainpreventive maintenancedescribedin FAR Part43. This maintenance may be performedonly on an aircraft which the pilot owns or operatesand which is not usedin air carriersewice.The following is a list of the maintenancewhich the pilot may perform: l. Repairor changetires and tubes. 2. Servicelandinggearwheelbearings,suchascleaning,greasingor replacing. 3.
CHEROKEESIX.3OO REQUIREDSERVICEAND INSPECTIONPERIODS Piper Aircraft Corporation providesfor the initial and first 50-hour inspection,at no chargeto the owner.The Owner ServiceAgreementwhich the ownerreceivesupon deliveryof the aircraft should be kept in the aircraft at all times.This identifieshim to authorizedPiper agreement with the regularsengice dealersand entrtlesthe ownerto receiveservicein accordance terms.This agreementalsoentitlesthe transientowner full warrantyby any Piperdealeriu the world.
r - .1 ? L ,. .r i \. SPECIALINSTRUCTIONS TYPEOF LUBRICANTS $ IDENTIFICATIOII LETTER A B F G H I sPEClFlCATlOtrl LUDRICANT LUBRICATINGOIL, GENERAL PURPOSE.LOW TEMP, IUARICATING OIL, AIRCFAFT RECI'ROCATING ET'IOII{E IPISIO'{} GFAOE AS SPECIFIED SAE SOABOVE6OCTAIB TEMP. sAE ao 30c TO 906F Atn IEMP. TOOFAlR TEMP. SAE il OE 'O TOOFAIR TEMP. SAE 20 EELOIV HYDFAULIC FLUID, PEIROLEUM EASE GREASC,AIRCRAFT ATIO INSIFUME'{I, GEAR AT{O ActuAtoR scRE|l, GREASE.AIFCRAFT. HIGH TCMP.
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al _ BERLIN AVIONICS 3]-55 DONALD DOUGLAS LOOP S SANTA MONTCA, CA. 90405 FAA REPAIR STATION Ebur109k WEIGHT AND BALANCE REPORT *** REVISED EQUIPME}TT LISTq ----o G-^ --5: .:- -: : : a : : Ubbel (r --tr /rT Re g istr ation - : --: : : a ' i l'1':':::..:n Gross Weiqht ?. = ' . - : s e i we ig h t and balance :: -- a : a :e o 0 2 /L9 /04- P IP E R P A 32-30 0 32-7 4400 14 N7801_A 3400 LBS q computat io n s a re b a s e d o n p re v io u s WEIGHT (LBS ) ARM ( IN) MOMENT ( IN/LBS ) s.0 69 .
