TECHNICALDESCRIPTION,OPERATING, MAINTENANCEAND REPAIRMANUAL
1.1 Introduction
TheTechnicalDescription,Operating,Maintenance andRepairManualforaeroplane
WT-9Dynamichasbeenpreparedtoprovidetheinformationforthesafeandefficient
operationofthisultralightaeroplane.
Thismanualcontainssupplementaldatasuppliedbytheaeroplanemanufacturer.
1.2 Certificationbasis
ThistypeofaircrafthasbeenapprovedinGermanybytheDeutscherAeroClube.V.
(DaeC)inaccordance withtheGermanCertificationRegulationsandAirworthiness
RequirementsforultralightaircraftoftheDaeC(BFUdesDaeC, Ausgabe10/95)and
theTypeCertificateNo.61179 hasbeenissuedon23.10.2001.
TheCivilAviationAuthoritiesofSlovakRepublicfollowing anapplicationby
AEROSPOOL, spol. sr. o.Prievidza andafterstudying thedocumentationPredpis
MDPT SRL8/ALU . P-ULL-1SRhasissuedtheTypeCertificateofAirworthiness
No.V-80/2004datedApril25th 2005 forTypeWT-9Dynamic
CategoryofAirworthiness : NormalwithMTOMup to472,5kg
1.3Warnings, cautions and notes
Thefollowing definitionsapplytowarnings, cautionsandnotesusedinthemanual.
WARNING
Meansthatthenon-observationofthecorrespondingprocedure
leadstoanimmediateorimportantdegradationoftheflight
safety.
CAUTION
Meansthatthenon-observationofthecorrespondingprocedure
leadstoaminorortoamoreorlesslongtermdegradationofthe
flightsafety.
NOTE
Drawstheattentiontoanyspecialitem, notdirectlyrelatedto
safetybutwhichisimportantorunusual.
1.4 Basicandgeneralinformation
1.4.1Aeroplanedescription
WT-9Dynamicisasingleengine,low-wingmonoplanewithtwoside-bysideseats
anddualcontrol.Anairframeconsistsofasandwichshellsfromadvancedcomposite
material.. Theaeroplaneisequippedwithafixedoraretractabletricycleundercarriage
withanosewheel.Aspowerplantofthisultralightaircraftisused4cylinder, 4stroke
enginesROTAX912 UL(59,6kW)orROTAX912 S2(73,5kW)with3blades,in
flightelectricallyadjustableaircraftpropellerWoodcompSR2000.
1.4.2 Designation
WT-9Dynamicisintendedforsporting, recreationandtouristflying inaccordance
withVFR. Aerobaticmanoeuvresandintentionalspinsareprohibited!
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