This sounds like a binding servo problem. On the earlier launch, the power 
bus may have been pulled down by the overcurrent causing the momentary 
control lockup you described.  Releasing from the winch may have released 
the bind allowing the resumption of normal control. This reasoning continues 
that on the later launch a repeat of the bind caused an overcurrent that 
blew the circuit on the switch board which was damaged by overheating during 
the earlier overload.  Just guessing.

An onboard battery checker may have helped to disclose this condition in 
advance if you watched it while exercising the servos and possibly loading 
the surfaces by hand on the ground prior to flight.

Good luck,

Tim Bennett


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