What was found
CRACK ON EXTERNAL SKIN LOCATED AT BS 420+13.5" AND STR 16R UPPER LOBE FUSELAGE. REPAIRED SKIN PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON EXTERNAL SKIN LOCATED AT BS 420+13.5" AND STR 16R UPPER LOBE FUSELAGE. REPAIRED SKIN PER SRM.