What was found
THE FUSELAGE SKIN AT BS 240.5 BETWEEN STRINGERS 29P & 30P WAS DENTED. REPAIRED IAW EA 42-2018-040, REV A-P2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN AT BS 240.5 BETWEEN STRINGERS 29P & 30P WAS DENTED. REPAIRED IAW EA 42-2018-040, REV A-P2.