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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 flag symbol and enter the item number of the product into the search field;
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 flight controller can be operated with 2 - 3 cells LiPo, but the motor or flight 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