reducing the torque slows the propagation rate.
Does the reduction in MCP "reduce" or "stop" the propagation of the cracking?
In about a half dozen posts....we have directly contradictory comments.
Am I the only one here that sees this 225 MGB problem being far more dangerous than EC is letting on?
Are we seeing Operators and EC conspiring to put the 225's back into Service without
FIRST determining
exactly what is causing the Failures....and
THEN re-designing the MGB to
ELIMINATE the problem and doing the necessary
TESTING to
CONFIRM/CERTIFY the
CURE.....
BEFORE putting the aircraft back into service?