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IFT Evolve 300 CX - Page 40

IFT Evolve 300 CX
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40
Afterincreasingthecontrolresponse/authorityandinstallingtheshortlength
stabilizerflybar(aspreviouslyoutlinedinthissection)manypilotswillbeabletofly
theEvolve300CXsuccessfullyinwindsupto5mph.However,wedonotrecommend
thatallpilotsflyinwindsupto10mph,especially
firsttimeandlowtimepilots,as
moreexperienceistypicallyrequiredtomaneuver/flythehelicoptersuccessfullyinthe
higherspeed/strongerwinds.Also,wedonotrecommendattemptingtoflytheEvolve
300CXinanywindshigherspeed/strongerthan10mph.
Whenflyingoutdoorsinthewindit’srecommended
toraisethethrottletrimtothe
middleoreventhehighestpossiblepositioninordertoincreasethemaximumamount
ofpoweravailablewhenthethrottlestickisraisedtothehighestpossibleposition.
IMPORTANTNOTE:IfyoudoraisethethrottletrimleveryouMUSTrememberto
loweritANDthethrottlesticktotheirlowestpossiblepositionsIMMEDIATELYinthe
eventofacrashorrotorbladestrike.Failuretolowerthethrottletrimandthrottle
sticktotheirlowestpossiblepositionsimmediately
intheeventofacrash/rotor
bladestrikecanresultindamagetotheESCsinthe3in1controlunit (whichmay
requirereplacementofthecontrolunit).
AlthoughtheEvolve300CXislargerandmorecapableofflyingoutdoorsinwindthan
mostotherCX
(coaxial)helicoptermodels,therearesometraitsinherentduetothe
coaxialandfixedpitchdesignthatpilotsshouldalwayskeepinmind.Also,itwilltake
somepracticeformostpilots,eventhosewithexperienceflyingFP(fixedpitch)andCP
(collectivepitch)helicopters,toidentifyandbetterunderstand
allofthesetraitsbut
herearethemostimportantonestokeepinmind:
o Duetothefixedpitchrotorbladedesignmostpilotswillfindthatittakessome
‘balancing’ofthethrottle/poweroutputandthe‘angle’thehelicopteris
pitched/bankedattomaintainspeedandaltitudeduring
forward/backward/sidewaysflight.Thisisespeciallytruewhenflyingdirectly
intothewind,andinsome
casesitwillnotbepossibletoflydirectly
into/penetratethewindatareasonablegroundspeedwithoutgainingaltitude
(thistraitisalsoinherentinmostsinglerotorFPhelicopters).

o Alsoduetothefixedpitchrotorbladedesignitwilltakesomepracticetofind
thebestbalanceofthrottle/poweroutputandothercontrolstodescend/lose
altitudewithoutdecreasingthespeed/RPMsoftherotorbladestoomuch(if
thespeed/RPMsdecreasetoomuchthehelicoptercanlosealtitudetoo
quickly
and/orbecomeunstableresultinginacrash).Thisisespeciallytruewhentrying
todescend/losealtitudeandwhenflyinginto(upwind),with(downwind)or
evensidewaysinthewind(thistraitisalsoinherentinmostsinglerotorFP
helicopters).