What was found
CRACK ON EXTERNAL FUSELAGE SKIN AT BS 1437 BETWEEN LONGERONS 3LT AND 4LT. CRACK WAS REMOVED AND REPAIRED IAW SRM 53-04, FIG 27.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON EXTERNAL FUSELAGE SKIN AT BS 1437 BETWEEN LONGERONS 3LT AND 4LT. CRACK WAS REMOVED AND REPAIRED IAW SRM 53-04, FIG 27.