What was found
1 CRACK ACROSS RIVET HOLE AT VERT. STAB SKIN FWD OF R/H LWR CORNER OF SADDLE PANEL CUT OUT. FOUND ON B-2 LETTER CHECK INSTALLED DOUBLER PER M/M 54-30-0 #1
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
1 CRACK ACROSS RIVET HOLE AT VERT. STAB SKIN FWD OF R/H LWR CORNER OF SADDLE PANEL CUT OUT. FOUND ON B-2 LETTER CHECK INSTALLED DOUBLER PER M/M 54-30-0 #1