Well it's been a disappointing week here. It's been too hot to work in the hangar on the Cruisair project. Last evening I went out to work on it and saw new longitudinal cracks running through both front spars that were not there before. I couldn't believe my eyes. Those spars looked almost as good as the day they came out of the factory.
The only thing I can attribute this to is the excessive heat. The airplane has been dropped on both wingtips as a result of gear failures, but I inspected the spars carefully and found no signs of compression stress or yield around the hardware mounting points. These cracks seem to have resulted just from the heat alone. Maybe there were internal stresses on those spars that manifested themselves (fortunately) before the wings were covered and flying.
My point here is, with all of this excessive heat and the age of a lot of these aircraft it might be prudent to just sneak in there and get a gander at your spars. I don't know for certain what caused my issue, but I'm really hoping no one else had this happen on a flying aircraft. Stay safe out there!!
-Olbellboy (Ron)
The only thing I can attribute this to is the excessive heat. The airplane has been dropped on both wingtips as a result of gear failures, but I inspected the spars carefully and found no signs of compression stress or yield around the hardware mounting points. These cracks seem to have resulted just from the heat alone. Maybe there were internal stresses on those spars that manifested themselves (fortunately) before the wings were covered and flying.
My point here is, with all of this excessive heat and the age of a lot of these aircraft it might be prudent to just sneak in there and get a gander at your spars. I don't know for certain what caused my issue, but I'm really hoping no one else had this happen on a flying aircraft. Stay safe out there!!
-Olbellboy (Ron)