i Believe that the currant method of detecting the debonding issue with the main rotor blades is an acceptable method as long as it is followed properly , repainted, as and when neccessary to prevent the bonding from being exposed to the elements.
i do however disagree with the statement that it is not a manufacturing problem.
it is obvious that the vary design of these blades is contributing to the situation that we are finding ourselves in.
i might well ask what other blade manufactures are having this kind of problem and are they also going down this same path way ? no .
if the blades were of a composite material would we be having this problem?
is there any evidience to show that the new dash 7 replacement blades would be any better?
if so what is the difference in the manufacturing process to produce the replacement blades ?
the new blades could develop an even bigger problem than the one we have allready ,
i would like to be reasurred that in the event that the FAA belive that replacement of the blades would eleminate this problem once and all not a repeat of the last epiosode
Howard Edward Carlsen
This is comment on Rule
Airworthiness Directives: Robinson Helicopter Co. Model R22, R22 Alpha, R22 Beta, R22 Mariner, R44, and R44 II Helicopters
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