TL Ultralight TL-3000 Sirius Quick start guide

Aircraftserial

number:

Documenttype



Flightandoperationalmanual R

gis

ation:



TL‐3000SIRIUS

TLUltralights.r.o.

Airport,building84

50341HradecKralove

CzechRepublic

Tel:+420495211753

+420495218910

Tel/Fax:+420495213378

www.tl‐ultralight.cz

Flightandoperationalmanual

TL3000SIRIUS

 Page2

0Listofchanges



Change,

amendment

serial

number

Bulletin



number

Changed

pages



Newpage

releaseor

changedate

Executiondateand

signature

Flightandoperationalmanual

TL3000SIRIUS

 Page3

CONTENTS



Section1Generalinformation  4‐10

Section2Operationallimitations  11‐21

Section3Emergencyprocedures  22‐26

Section4Normalprocedures        28‐34

Section5Performances  36‐39

Section6Weightandgravitycentreposition  41‐43

Section7Aircraftanditssystemsdescription  45‐49

Section8Operating,servicingandmaintenance  51‐60

Section9Amendments                62‐63

Flightandoperationalmanual

TL3000SIRIUS

 Page4

Section1

Generalinformation



1.1Introduction 5

1.2Certificationattest 6

1.3Abbreviationsanddefinitions7

1.4Warnings,notificationsandnotes8

1.5Technicaldata8

1.6Three‐viewdrawing10

Flightandoperationalmanual

TL3000SIRIUS

 Page5

1.1Introduction



ThisflightandoperationalmanualproducedbyTLUltralightisdesignedto

introduceTL‐3000SIRIUSaircrafttoitsoperator.Itprovidesthebasicusage

informationandoperationalproceduresensuringthemosteffectiveaircraft

utilizationbytheoperator.

Eachholderofthisflightandoperationalmanualand/oritspartsisobliged

tomaintainitinupdatedstatebyimplementationofamendments,

revisionsandchangesaspublishedinthebulletinthroughthefollowing

web‐page:

http:

‐u

tral

ght.

cz/e

lle

tin



Handwrittenamendmentsandrevisionsofthismanualarenotallowed

exceptofsituationswhenthesecurityinterestrequiresanimmediate

amendmentorrevision.

Thisflightandoperationalmanualisdividedbytopicsintoseveralsections

thataresplitintoparagraphsaccordingtothesignificanceandimportanceof

theirsubjectmatter.Incaseofpagereplacement,amendmentor

handwritingrevision,suchfactmustberecordedontheChangeslogpage

byrecordingthechangeoramendmentserialnumber,bulletinnumberin

whichthechangewaspublishedorpagechangedoramended,newpageor

changepublishingdate,andimplementationdateandsignature.

Thisoperationalmanualisestablishedsuchwaythatanyrevisionor

amendmentexecutionisonlypossiblebyreplacingoraddingthe

appropriatepagesanddiscardingtheobsoletepages.Therefore,itis

necessarythatallmanualholderspayincreasedattentiontorecordingall

changesandamendmentsandtheirimplementing.

Caution



Thisaircraft,belongingtosportsaviationgadgets,isnotsubjecttoCivil

AviationAuthorityoftheCzechRepublicapprovalandisoperatedby

theuserathis/herownrisk.

Flightandoperationalmanual

TL3000SIRIUS

 Page6

1.2Certificationattest

ThisaircrafthasbeenapprovedbytheAmateurLightAircraftAssociationof

theCzechRepublicinaccordancewiththeregulation“UltralightAircraft

AirworthinessRequirements”.

ThetypecertificateNr.ULL‐01/2010wasissuedonApril1st,2010.



Flightandoperationalmanual

TL3000SIRIUS

 Page7

1.3Abbreviationsandd

itions



CASThecalibratedairspeedistheindicatedairspeedcorrectedfor

thepositionalandinstrumentalerror.Thecalibratedairspeedis

equaltotherealairspeedintheISAattheseelevel.

IASTheindicatedairspeedistheairspeedshownontheaircraft

Pitotstaticspeedindicatingsystemwiththescalethatis

adjustedtoincludetheinfluenceofthe

atic

stream

coercibilityatstandardatmospherezeroaltitudebutnot

correctedforthespeedometersystemerror.

(ςo

/ς

)1/2.

ςo=airspecificweightattheseelevel

ς =airspecificgravityatgivenaltitude

ISAInternationalstandardatmosphere

MACMeanaerodynamicchord

V

NEMaximumneverexceedspeed

Maximumstructuralcruisingspeed

VRAMaximumturbulencepenetratingspeed

V

ADesignmanoeuvringspeed

V

FEMaximumflapextendedspeed

GLETEmptyaircraftweight(kg)

GPALFuelweight(kg)

GPOSCrewweight(kg)

GZAVLuggageweight(kg)

GPAircraftweightloadonthenosegear(kg)

GHAircraftweightloadonthemainundercarriage(kg)

XTEmptyaircraftcentreofgravitydistancefromtheindexplane,i.e.

fromthewingleadingedge(mm)

X%LETEmptyaircraftcentreofgravityposition(%MAC)

X%KONFIGURACERequiredconfiguration

centring

position(%MAC)

Flightandoperationalmanual

TL3000SIRIUS

 Page8

1.4Warnings,cautionsandnotes

Thisflightandoperationalmanualprovidesthefollowingdefinitionsofwarning,

cautionandnote



WARNING:

Overlookinganappropriateprocedureleadstoinstantorsignificantflightsafety

decrease.



CAUTION:

Overlookinganappropriateprocedureleadstoshortorlonglastingminorflight

safetydecrease.



NOTE:

Itnotifiesaboutaspecialpointthatisnotdirectlyrelatedtotheflightsafetybut

isimportantorunusual



1.5Technicaldata

TL‐3000Siriusultralightaircraftisatwo‐seatclassicaldesignhigh‐wing

monoplanewiththenosetypeundercarriage.Theentireaircraftisbuiltof

thecompositematerials.



Wing



Wingspan9,4m

Length6,75m

Height2.25m

Wingarea11,15m2

Wingspan–cordratio7,92

Areaload40,3kg/m2

Rootprofiledepth1,3m

Tipprof

edepth0,9m

Ailerons



Aileronspan1.87m

Aileronarea0.51

AileronangleUpwards150

Downwards90

Flaps



Flapspan2.07m

Flaparea0.66m2

FlapangleStart10.50

Flightandoperationalmanual

TL3000SIRIUS

 Page9

Interposition280

Landing450

Horizontaltailplane



Horizontaltailplanespan3.0m

Horizontaltailplanearea1.62m2

ElevatorangleUpwards19,50

Downwards110

Verticaltailplane



Verticaltailplanearea 1.45m2

Rudderangle+/‐200

Undercarriage



Mainwheel‐spacing2.17m

Wheelbase1.53m

Undercarriagewheeldimensions400X100

Atmosphericpressureinthetyres2.0kP



NosewheelreboundCoilspring

MainundercarriagereboundTyres,undercarriagelegresilience

BrakesHydraulicdiscbrakes

Fueltankvolume



130

lit

res



Emptyaircraftweightkg

Wingmeanaerodynamicchordlength

(

MAC

)



MAC=1230mm



Engine

Rotax912ULS,aboxertypefour‐strokefour‐cylinder,theheadsofcylinders

areliquid‐cooledandthecylindersareair‐cooled.Theengineisintegratedwith

areducerandtwocarburettors.Itisequippedwithadoublecontactless

condenserignition.



Propeller

Theaircraftisequippedwithathree‐blade,DUCgroundadjustablepitch

propeller.



Rescuesys

m

GRS473

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