Instructions

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15. Declaration of Conformity (DOC)
Conrad Electronic SE, Klaus-Conrad-Straße 1, D-92240 Hirschau, hereby declares that this product complies with
directive 2014/53/EU.
 ThecompletetextoftheEUdeclarationofconformityisavailableunderthefollowingwebaddress:
www.conrad.com/downloads
 Choosealanguagebyclickingaagsymbolandentertheitemnumberoftheproductintothesearcheld;
thenyoumaydownloadtheEUdeclarationofconformityinthePDFformat.
16. Technical data
a) Model airplane
Wing span .........................................................1200 mm
Length...............................................................700 mm
Weight .............................................................Asofapprox.490g
Wing area .........................................................15.2 dm²
Control ..............................................................4 channels (aileron, elevator, rudder, motor)
Propeller ...........................................................22.8x17.8cm(9x7")
b) Electric Motor
Electrical motor power consumption .................approx.100W
Operating voltage .............................................2 cell LiPo (rated voltage 7,4 V)
Revolutions per Volt (KV) .................................1050
c) Flight Controller
Input voltage .....................................................2 - 3 cells LiPo (7.4 to 11.1 V)
 Theightcontrollercanbeoperatedwith2-3cellsLiPo,butthemotororightmodelusedisdesignedfor
2 cells. Therefore only operate the model plane with a 2-cell LiPo battery to avoid damage.
Current capacity ...............................................Permanentcurrent12A,shortterm(30s)max.20A
Undervoltage recognition ..................................3,0 V/cell
BEC-output (linear) ...........................................5 V/DC, 1 A