What was found
CRACK IN FUSELAGE SKIN AT 2ND FASTENER BELOW STRINGER 22R FWD ROW OF BS 540 CHORD. REPAIRED SKIN IAW EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE SKIN AT 2ND FASTENER BELOW STRINGER 22R FWD ROW OF BS 540 CHORD. REPAIRED SKIN IAW EA.