What was found
PROTUBERANCE ON, BETWEEN LONGERON 24RT AND 25RT BS 168 AT OUTER FUSELAGE SKIN. THIS DAMAGE WAS FOUND WITH PREVIOUS REPAIR IAW SRM 53-04-2, FIG 2, SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PROTUBERANCE ON, BETWEEN LONGERON 24RT AND 25RT BS 168 AT OUTER FUSELAGE SKIN. THIS DAMAGE WAS FOUND WITH PREVIOUS REPAIR IAW SRM 53-04-2, FIG 2, SHEET 3.