As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE EXTERIOR SKIN RT SIDE. AFTER DOUBLER REMOVAL & DEEP INSPECTION FOUND ELONGATED HOLES FROM BS 560 - 580 FROM STRINGER 26 TO 28. THERE ARE FIVE ELONGATED HOLES AS MARKED. ACCOMPLISH NEW REPAIR ON FUSELAGE SKIN BS 577. REPAIR CLASSIFIED AS MAJOR.