SID's - Front & Rear Spar Eddy Current (bolt hole)
Hi Everyone
I need some thoughts on this matter from other members of the forum, last week all SID's were completed on my plane with the exception of the front and rear spar bolts / screws.
Aircraft is 33701575 (1974)
In my aircraft these two bolts / screws do not exist, they are rivits and are factory. The SID's which my aircraft S/N falls into still specifies the removal of the bolts /screws to complete the stated eddy current inspection of the bolt hole. They even show the photograph of the bolts / screws.
1. Does anyone have information or documentation from Cessna regarding this?
2. Has anyone completed the SID's on their aircraft which has rivits, and what did you do?
A previou post mentioned a discussion with Cessna had taken place regarding this particular issue - the response was remove the rivits and replace with bolts / screws.
I have a window of opportunity to finalise this last remaining SID tomorrow, do I remove the rivits?
Appreciate and assistance with this.
Dave
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