Monday, July 20, 2009

July 10, 2009: Static Air continued


P. 10-10 step 6-10. Took care to debur the F-1210C Angle so as not to cause a deformation when riveting the top skin onto the tailcone. First clecoed skin onto tailcone and then match drilled as per step 6. Dissassembled and deburred. Then re-clecoe and rivet. also followed directions to mask over holes within 7 inches of the fwd edge of the tailcone skins.