PERFORM WHERE OTHERS CAN’T - placo.co.zafinal).pdf · ranging from 400-800m level to 380-600m...

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PERFORM WHERE OTHERS CAN’T

Transcript of PERFORM WHERE OTHERS CAN’T - placo.co.zafinal).pdf · ranging from 400-800m level to 380-600m...

Page 1: PERFORM WHERE OTHERS CAN’T - placo.co.zafinal).pdf · ranging from 400-800m level to 380-600m with 5 ... The different configurations include passenger ... > Sets the benchmark

PERFORM WHERE OTHERS CAN’T

Page 2: PERFORM WHERE OTHERS CAN’T - placo.co.zafinal).pdf · ranging from 400-800m level to 380-600m with 5 ... The different configurations include passenger ... > Sets the benchmark

XSTOL EXTREMELY SHORT TAKE-OFF & LANDINGXSTOL™ = The ability of an aircraft to take-off and land in less than 800 ft (244m) while carrying a load greater than its own empty weight.

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800 ft /244m

1,800kg

3,968lb

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THIS AIRCRAFT HAS SUCH UNIQUE EXTREMELY SHORT TAKE-OFF AND LANDING (XSTOL™) CAPABILITIES THAT IT DEMANDED A CLASS OF ITS OWN. THE RESULT OF MORE THAN SIXTY YEARS OF EVOLUTION, THE P-750 XSTOL IS THE WORLD’S FIRST XSTOL™ AIRCRAFT UNMATCHED BY ANY OTHER PRODUCTION AIRCRAFT.

> Take-offandlandinginlessthan800ft(244m)atMTOW,evenwhenit’shotandhigh.

> Operateoffsemi-preparedstripsinalltypesofterrain.

> Carryaloadofalmost4,000lb(1,814kg)eveninhotandhighconditions.

> Rugged,dependableconstructionwithextendedairframe/engineinspectionintervalsof150hrs.

The XSTOL™ delivers unsurpassed capability to provide:

> Proven,globally-supportedcomponentsfromleadingaerospacecompanies,includingPratt&WhitneyCanada,Garmin,HartzellandHoneywell.

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THE ULTIMATEUTILITYAIRCRAFT“We operate into approximately 300 remote bush strips throughout Papua New Guinea ranging from 400-800m level to 380-600m with 5-18% slopes. There is no airstrip in the country (currently open and maintained) that we cannot operate the XSTOL™ into.”ROGER S MILLIST, PILOT / CEO, ADVENTIST AVIATION, PAPUA NEW GUINEA

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SincePALstartedmanufacturingaircraftin1954,itsmanufacturingfacilityinHamilton,NewZealandhasproducedmorethan600extraordinarilycapableaircraft.PacificAerospacehasbuiltanexcellentnameforruggedaircraftthatareeasytoflyandmaintainandareoptimisedforeveryjobtheyundertake.

PERFORM WHERE OTHERS CAN’T

THE P-750 XSTOL IS THE LATEST AIRCRAFT FROM PACIFIC AEROSPACE AND HAS CONSISTENTLY PROVEN ITSELF WHILE OPERATING IN SOME OF THE TOUGHEST ENVIRONMENTS AN AIRCRAFT CAN FACE.

“The P-750 XSTOL performs where others can’t. Our customers’ success is our success.” DAMIAN CAMP, CHIEF EXECUTIVE OFFICER, PACIFIC AEROSPACE LTD.

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*BasedonanaircraftwithanEmptyWeightof3600lbs,equippedforBasicVFRflight.

PERFORM WHERE OTHERS CAN’TMAIMAFU, EASTERN HIGHLANDS, PAPUA NEW GUINEA

>CO-ORDINATES

06 30.10’S 145 02.02’E >ALTITUDE

5,200ft / 1,585m>TEMPERATURE

Average 30°C+ / 86°F+

>LENGTH

1,450ft / 442m >SLOPE OVERALL

15% / max >18%>TAKE-OFF PAYLOAD

3,900 lb/ 1,769 kg*

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PERFORMANCE ENHANCED PROFIT

ACCESS MORE STRIPS, MORE OFTEN, WITH MORE PAYLOAD. THE XSTOL™ CAN ACCESS TWICE AS MANY OF THE WORLD’S LANDING STRIPS COMPARED TO OTHER UTILITY AIRCRAFT, AND IT DOES SO WHILE CARRYING 3,900 LB / 1,769 KG, * GREATER THAN ITS EMPTY WEIGHT.

Whilesomeofthesestripscanbereachedbysmallsix-seateraircraftcarryingsmallloads,theXSTOL™hasprovenitsability,inthetoughestenvironments,tocarryuptothreetimestheloadofotheraircraftoffthesameairstrips,achievingintwohourswhatpreviouslytookawholeday’sflyingtocomplete.

Itsunmatchedreliabilityandlowmaintenancecostsprovidesyouwithanaircraftthatmaximisesprofitabilityandcangetthejobdone,allowingyoutomakeaprofitonroutesthatwerepreviouslymarginal.

XSTOL™ Performance Demonstration

AFRICA AEROSPACE & DEFENCE EXPO, AIR FORCE BASE YSTERPLAAT, CAPE TOWN, SOUTH AFRICA,

DATE: 19TH SEPTEMBER 2008 ELEVATION: 200FT (61M), WIND: 10KTS, TEMP: 12ºC (53.6ºF)

AtAAD2008,renownedSouthAfricanpilotChrisBriersflyingastandardproductionP-750XSTOLweighing4,200lb(1,909kg)andcompletewithcargopod,puttheaircraftthroughitspaces.ThedemonstrationclimaxedinChrisachievingatake-offdistanceoflessthan140ft(32m)andalandingdistanceof164ft(50m).Thiscrowd-pleasingdemonstrationleftnouncertaintytotheextremeSTOLperformanceandmanoeuvrabilityoftheP-750XSTOL.

TO VIEW THE DEMONSTRATION PLEASE VISIT WWW.AEROSPACE.CO.NZ

LANDING164ft /50m

TAKE-OFF104ft /32m

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HIGH ALTITUDE, HOT CONDITIONS, HEAVY LOADS.In the world’s hottest environments, the XSTOL’S high lift wing comes into its own carrying full loads out of short strips. This gives the operator the ability to operate out of the same airstrips, all day, every day, regardless of temperature and without compromising load.

PROVENIN THE HOTTEST, HIGHEST MOST RUGGED ENVIRONMENTS

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MAXIMUM UTILITY THROUGH QUICK TURN-AROUNDA MULTI-TASKER THAT MAKES THE MOST OF EVERY MINUTE.

TheP-750XSTOLisdesignedtogetthejobdoneandeveryattentionhasbeengiventoensurethatitisareliableaviationworkhorse–theretogetthejobdoneandgeneratethemaximumprofitforitsoperators.

Quickturnarounds,essentialforproductivity,arefacilitatedbydoublerearcabindoorsandalargesinglecompartmentcargopodwitharear

rampenablingtheXSTOL™tobequicklyloadedandunloaded.Theconfigurationoftheaircraftcanbequicklychangedbetweenpassengerandcargoroleswithin30minutes.Allthestandardpassengerseatscanberemovedandstowedineitherthestoragecompartmentattherearofthecabin,orinthecargopodforquickconversionbetweenrolesonreturnlegs.

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TOUGH RELIABLE, EASY TO MAINTAIN & OPERATE

Low Maintenance

Withits150-hourairframe/engineinspectioninterval,theXSTOL™haslowermaintenancerequirementsthananycomparableaircraft.TheaircrafthasbeendesignedtobeeasilymaintainedandembodiesoversixtyyearsofknowledgeandexperiencegainedfrompreviousmodelsofPacificAerospaceagriculturalaircraft.Theseaircraftaveragefiveminuteflightcycleswithmaximumloadsandoperatefromremotesemi-preparedstripsinNewZealandhillcountry,alldayeveryday.Atoughprovingground.

Easy To Refuel And Check

WithitslowwingtheXSTOL™iseasytorefuel,whereveritispositioned.Pre-flightchecksandrefuellingcanbecarriedoutwithoutaladder,unlikehighwingaircraft.

Notonlyisturnaroundfaster,it’ssafer–especiallyinbadweather.

Byutilisingwellproven,reliableandglobally-supportedsystems–suchasPratt&WhitneyCanadaPT6A-34turbopropengines,HartzellpropsandGarminavionics–wecanensurethathigh-quality,reliablesupportisalwayswithinreachanywhereintheworld.

Quality Components

Byutilisingwellproven,reliableandglobally-supportedsystems–suchasPratt&WhitneyCanadaPT6A-34turbopropengines,HartzellpropsandGarminavionics–wecanensurethathigh-quality,reliablesupportisalwayswithinreachanywhereintheworld.

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READY TO DEPART

AIRCRAFT ONLY MAKE MONEY WHEN THEY ARE FLYING: THE XSTOL™ IS READY TO FLY MORE THAN ANY OTHER AIRCRAFT.

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VERSATILE ONE PLANE, SO MANY APPLICATIONSThe P-750 XSTOL is the world’s most versatile utility aircraft. This PT6 turbine powered aircraft has a unique quick-change modular floor system and easily removable role equipment, which allows the aircraft to be transformed rapidly between no less than ten distinct mission configurations.

The quick change, multirole floor allows P-750 operators to move easily between different role configurations to maximise aircraft utilisation. The different configurations include passenger/freight; agriculture solid and liquid; firebombing; survey geophysical and photographic; medical evacuation; skydiving; and surveillance, search & rescue.

Passenger / Utility

> Setsthebenchmarkfor10-seaterSTOLutilityaircraft.

> Amplepassengerlegroomandluggagestorage.

> Abletoundertakemixedpassenger/freightroles.

> Cancarryaloadofpassengersononeleg,thenrapidlyconverttoanall-freightconfigurationforthenextlegbystowingthepassengerseatsinarearcabincompartment.

> Noneedforatailstandwhenloadingtheaircraft.

> Sub-dividablesinglecompartmentCargoPodwith1,000lb(454kg)capacity.

> Optionofmouldedormetalliningsinthecabinforincreaseddurability.

Skydive

> Globallyrecognisedastheultimateskydivingplatform.

> Achieveprofitwithsmallloadsi.emakeaprofitwithsevenjumpers.

> Abletocarryseventeenskydiversorseventandemteams.

> Unmatchedabilitytoclimbrapidlytojumpheighte.g.sealevelto12,000ftintenminutes.

> Factory-installedskydivingdoorthatcanbeoperatedbythepilotensuringnoopen-doorspeedrestrictionsondescent.

> Climbanddescentprofileisabouthalfthehorizontalairspaceofmostotherjumpplanes,assistingoperationinnoise-sensitiveareas.

> Widecentreofgravityrangemakingitaverystablejumpplatform.

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Agriculture – Solid / Liquid and Firebombing

> Abletocarrya4,888lb(2,217kg)hopper.

> Effectivelyoperatesoffshort,narrowhillcountryairstripsthatareoftensituatedonridgelines.

> Operatorscommonlycompleteupto17cycles(load,take-off,dispense,land)perhour.

> Hoppercanberemovedwithoutaffectingtheairframe,allowingversatilityintherolesoftheaircraft.

> Aircraftcanbeconvertedtoanotherfactory-approvedconfiguration,maximisingitsusefullifeandresalevalue.

Aerial Survey

> Superiorstabilityevenatlowspeedallowstheaircrafttoundertakesurveyrolesusuallyreservedforhelicopters.

> Factory-approvedmodificationssupporteasyinstallationofcameraholesintheflooroftheaircraft.

> Norequirementforcontrolcablereroutingoranyothercustomisationoftheaircraftsystems.

> Canbereadilycustomer-modifiedforgeophysicalsurveywork.

> Electrically‘quiet’aircraftwithminimalelectro-magneticinterferenceandallmajorcontrolsystemsmechanicalratherthanelectric.

> Theaircraftstructureservesasaneffectivefaradaycageblockingoutexternalstaticelectricfields.

Freight/Cargo

> Optionalwall-mountedtrackforusewithcargonets.

> Large50”wide,46.5”high(127cmx118cm)cargodoor.

> Single-compartment(sub-dividable)CargoPodwith1,000lb(454kg)capacityandaccessviathreesidecargodoorsandonelargerearramp.

> Cargocompartmentpartitionlocatedbehindthepilotprovidingloadsecurity.

> Widecentreofgravityrangeallowingforloadingflexibility.

> Noneedforatailstandwhenloadingtheaircraft.

VERSATILE ONE PLANE, SO MANY APPLICATIONS

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P-750 XSTOL KEY FEATURES

Constantspeed,fullfeatheringandreversiblepropellerforshort-fieldperformance.

3-BladeStandard4-BladeOptional

Thickchordwingforhighlift.

Outerwingdihedralforlateralstability.

Easyaccess‘gullwing’crewdoors. Large240ft3cabinwiththeabilityforittoberapidlyreconfiguredbetweenroles.

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Largeairintakeisoptimisedforrapidclimb,andprovidesRAMairandthrustrecoveryevenatlowforwardspeeds.AneffectiveinertiaseparationsystemforFODprotectionisincorporatedintheinlet.

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Highvisibilitycockpitforsuperiorsituationawarenessforthepilot.

Easilyremovedenginecowlingallowingforcompleteaccesstotheengineandsystems.

WellprovenandgloballysupportedPratt&WhitneyCanadaPT6A-34TurbineEngineproducing750shp.

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Highstrengthfixedlandinggearwitholeopneumaticshockstrutallowingforcustomisationofthecylinderpressuretotheconditions.

HighFlotationWheel(optional).Itwillsignificantlyimprovesoftgroundperformanceandgivesatleasta46%increaseinthefootprinttyre.

Aquickchangemulti-rolefloorallowsoperatorstomoveeasilybetweendifferentroleconfigurationstomaximiseaircraftutilisation.

Allmetalconstructionfordurability,ruggednessandeaseofrepairinthefield.

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Highvolume(70ft3,1,000lb)singlecompartment(removabledividernets)cargopodwithahingedrearloadingrampabletotakefulllengthsofplywood,roofingironandotheroversizeditems.

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Largedoubledoorsforrapidloadingandunloadingofpassengersandfreight.

Largepowerfulsingleslottedflapsspanningthecentrewingprovidinga58ktsstallspeed.

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Largepassengerwindowsforexcellentvisibility.

Lowwingforsuperiorlowspeedstability,finalapproachvisibilityandeaseofaccessforpre-flightchecks,refuellingandmaintenance.

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EXTERNAL DIMENSIONS

AREAS >WING GROSS

305.00 FT2 28.34 M2

>NETT

267.80 FT2 24.88 M2

>FLAPS

31.74 FT2 2.95 M2

>AILERONS

21.94 FT2 2.04 M2

>TAILPLANE

33.64 FT2 3.13 M2

>ELEVATOR

27.92 FT2 2.59 M2

>FIN

19.40 FT2 1.80 M2

>RUDDER

11.70 FT2 1.09 M2

12.08 FT3.68 M

Ø 8.83 FTØ 2.69 M

5.0 FT1.5 M

10.42 FT3.18 M

38.83 FT11.84 M

13.25 FT4.04 M

42 FT12.8 M

16.25 FT4.95 M

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INTERNAL DIMENSIONS

* Dimensions measured on top surface spar cover** Dimensions at cabin floor

40 IN102 CM

32 IN81 CM

102 IN259 CM

47 IN119 CM

*52 IN132 CM

**47 IN119 CM

**33 IN83 CM

56 IN142 CM

45 IN114 CM

56 IN142 CM

52 IN132 CM

43 IN109 CM

197 IN500 CM

40 IN102 CM

158 IN401 CM

30 IN76 CM

39.75 IN101 CM

48.75 IN123 CM

27 IN68 CM

42 IN107 CM

26 IN66 CM

34 IN86 CM

32 IN81 CM

32 IN81 CM 15 IN

38 CM

17 IN43 CM

30 IN76 CM

45.25 IN115 CM

30 IN76 CM

20 IN51 CM

20 IN51 CM

30 IN76 CM

32.5 IN82 CM

26 IN66 CM

36 IN91 CM

35 IN89 CM

32 IN81 CM

32 IN81 CM

6 IN15 CM

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>WEIGHT AND BALANCE

BASIC EMPTY WEIGHT(StandardIFR) 3,600lbs* 1,633kgs*

*BasicEmptyWeightiscompleteaircraft,emptyofusablefuelandwithoutoptionalequipment,butincludingengineoil,unusablefuel.BEWwillvarybetweenaircraftserialnumbersdependinguponfinalconfigurationandequipmentspecificationselected.

MAXIMUM OPERATING WEIGHTS

MaximumRampWeight 7,540lb 3,420kg

MaximumTake-OffWeight 7,500lb 3,402kg

MaximumLandingWeight 7,125lb 3,232kg

MaximumUsefulLoad 3,900lb 1,769kg

CentreofGravityRange 102.8to124.60inchesaftofdatum

2.3%to28.5%MAC(MeanAerodynamicChord)

>SPEEDS

TAS(TrueAirSpeed)10,000FT 167kts 309km/h

NeverExceedSpeed(VNE) 170kts 315km/h

DesignCruisingSpeed(Vc) 140kts 259km/h

MaximumManoeuvringSpeed(VA) 131kts 243km/h

MaximumFlapExtendedSpeed(VFE) 120kts 222km/h

StallSpeed(IdlePower)WithFlapsUp(VS) 58kts 107km/h

> RANGE

Max.RangeatOptimumSpeed(nilwind,noreserves),15,000ft. 1,172nm 2,183km

EnduranceatOptimumSpeed(noreserves) 8hrsStandard 10hrsw/Aux.Fuel.

AverageFuelConsumption(optimumcruisesettings) 49USGal/hr 184Litres/hr

FuelCapacity(useable) 330USGal 1,256Litres

Max.RangewithAux.FuelTankfitted(102US.Gal/387Lusable)** 1,400nm 2,593km

**Estimatebasedonoptimumcruisesettings,nilwindandnilreserves.

TECHNICAL SPECIFICATIONS

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>TAKE-OFF & LANDING PERFORMANCE Nil wind, 7,500 MTOW, Aircraft optimised for STOL performance (flight test data not yet published in POH)

Take-OffGroundRollatSeaLevel,ISA 721ft 220m

Take-OffDistanceTo15m(50ft),ISA 1,503ft 458m

LandingGroundRollatSeaLevel** 543ft 166m

LandingDistanceFrom15m(50ft)** 950ft 289m

**Reversethrustselectedontouchdown

CLIMB (AT MTOW)

MaximumRateofClimbatSeaLevel 1,067ft/min 325m/min

MaximumRateofClimbat8,000FT 951ft/min 290m/min

Climbto12,000FTFromBrakesRelease 14min

ALTITUDE LIMITS

MaximumOperatingAltitude 20,000ft*** 6,096m

ServiceCeiling(atMax.Weight) 25,000ft**** 7,620m

***Demonstratedto32,000ft.Approvalpendingforcertificationto25,000ft.****Estimatebasedonpreviousflighttesting.

CLIMB (AT MTOW)

MaximumPositiveG +3.5G

MaximumNegativeG -1.4G

WingLoading 120.07KG/M2 24.59LB/FT2

PowerLoading 10.0LB/SHP 4.5KG/SHP

Distancetoclear15m(50ft)is289m(950ft)

Groundroll:166m(543ft)

Distancetoclear15m(50ft)is458m(1,503ft)

Groundroll:220m(721ft)

15m(50ft)

XSTOL™extremedemonstration(refertopage7)

15m(50ft)

32m(104ft)

50m(164ft)

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PERFORMANCE

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THE ULTIMATE MULTI-ROLE AIRCRAFTQUICK CHANGE BETWEEN ALL MISSIONS

PASSENGER + FREIGHT

AGRICULTURE SOLID

AGRICULTURE LIQUID

FREIGHT

SURVEY PHOTOGRAPHIC

SURVEY GEOPHYSICAL

SURVEILLANCE, SEARCH & RESCUE

MEDEVAC

SKYDIVING

FIREBOMBING

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PACIFIC AEROSPACE LTD Private Bag 3027, Hamilton 3240, New Zealand 333 Airport Road, Hamilton 3282, New Zealand

TEL +64 7 843 6144 FAX +64 7 843 6134 EMAIL [email protected] WEB www.aerospace.co.nz