What was found
CRACK IN FUSELAGE SKIN AT BS 540, AFT FASTENER HOLE ROW, 2ND FASTENER BELOW STRINGER 22 LT. INSTALLED EXTERNAL DOUBLER IAW EA B737-53-034624.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE SKIN AT BS 540, AFT FASTENER HOLE ROW, 2ND FASTENER BELOW STRINGER 22 LT. INSTALLED EXTERNAL DOUBLER IAW EA B737-53-034624.