Just a simple question about the topic above: if experienced a start up wihout removing one or both of the engine air inlet covers what actions should be taken before the next flight?
I was told that it depends wether the ITT has exceeded the maximum permitted temperature or not and I was told also that there is a standard procedure on the manual dealing exactly with this case more than explaining what to do in case of a "normal" FOD during the start up or the flight.
I've looked all the documents I got in order to find this specific procedure but I found nothing ...
Does anyone of you has ever experienced this kind of issue and is aware of the correct procedure to follow and where I can find it ?
I hope not to be OT ...
... by the way it's a very important point to discuss about do you agree with me ?
Thanks a lot to you all,
Sax