What was found
DURING A STRUCTURE INSPECTION, FOUND A CRACK IN THE UPPER FUSELAGE BS 727B+8.5, STRINGER 16R AT UPPER CHEM-MILLED AREA. REPAIRED THE DAMAGED AREA IAW SRM 53-30-3, FIGURE 48, DETAIL VII.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A STRUCTURE INSPECTION, FOUND A CRACK IN THE UPPER FUSELAGE BS 727B+8.5, STRINGER 16R AT UPPER CHEM-MILLED AREA. REPAIRED THE DAMAGED AREA IAW SRM 53-30-3, FIGURE 48, DETAIL VII.