What was found
CRACK INDICATION ON RIGHT FUSELAGE SKIN PANEL SHELL LOWER AFT FASTENER HOLE AT FRAME 35, STRINGER 30R. REPAIRED THE SKIN IAW EA 268395 AND DRAWING R53370269.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK INDICATION ON RIGHT FUSELAGE SKIN PANEL SHELL LOWER AFT FASTENER HOLE AT FRAME 35, STRINGER 30R. REPAIRED THE SKIN IAW EA 268395 AND DRAWING R53370269.