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15. Declaration of Conformity (DOC)
The manufacturer hereby declares that this product complies with the essential requirements and regulations and all
other relevant provisions of the 1999/5/EC directive.
The compliance statement for this product is available at www.conrad.com.
16. Technical Data
Model:
Wing span ............................................................ 1200 mm
Length .................................................................. 700 mm
Weight .................................................................. As of approx. 460 g
Wing area ............................................................ 15.2 dm²
Control ................................................................. 4 channels (aileron, elevator, rudder, motor)
Propeller .............................................................. 22.8 x 17.8 cm (9 x 7")
Electric Engine:
Electrical motor power consumption ................... approx. 100 W
Operating voltage ................................................ 2 cell LiPo (7,4 V)
Revolutions per Volt (KV) .................................... 1050
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
