What was found
AFT FUSELAGE STRINGER 43L CORRODED BETWEEN FRAMES 56-63. REMOVED CORROSION & FOUND BLENDED AREA OUT OF SRM LIMITS BETWEEN FR 57-58. FABRICATED & INSTALLED REINFORCING ANGLE REPAIR REF SRM 53-00-13 FIG 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE STRINGER 43L CORRODED BETWEEN FRAMES 56-63. REMOVED CORROSION & FOUND BLENDED AREA OUT OF SRM LIMITS BETWEEN FR 57-58. FABRICATED & INSTALLED REINFORCING ANGLE REPAIR REF SRM 53-00-13 FIG 202.