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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 ........................................................... 1370 mm
Length.................................................................. 1100 mm
Weight ................................................................
Ready to fly from approx. 690 g upwards
Control ................................................................. 4 channels (aileron, elevator, rudder, motor)
Propeller .............................................................. 17.8 x 14 cm (7“ x 5.5“)
Electric Engine:
Power consumption ............................................. max. approx. 180 W
Operating voltage ................................................ 3 cell LiPo (11.1 V)
Revolutions per Volt ............................................. 1050 KV
Flight Controller:
Input voltage ........................................................ 2 - 3 cells LiPo (7.4 to 11.1 V)
Current capacity .................................................. Permanent current 15 A, short term (30 s) max. 20 A
Undervoltage recognition ..................................... LiPo 3.0 V/cell, LiFe 2.5 V/cell, NiMH 0.8 V/cell
BEC-output (linear) .............................................. 5 V/DC, 1 A
Flight Battery:
Battery technology ............................................... LiPo
Number of cells .................................................... 3 (rated voltage 11.1 V)
Capacity ............................................................... 1500 mAh
Discharge rate ..................................................... 12 C
