What was found
FUSELAGE SKIN DENTED AT BS 102.2, STRINGER 24P. REFORMED AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-044, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DENTED AT BS 102.2, STRINGER 24P. REFORMED AND CONSIDERED STRUCTURALLY ACCEPTABLE IAW EA 42-2018-044, REV A.