What was found
STRINGER 44 BETWEEN FRAME 64 - 65 HAS CORROSION. REMOVED CORROSION & INSTALLED REPAIR ANGLE IAW SRM 53-00-13 FIGURE 202 SHEET 2. NO SRI REQUIRED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER 44 BETWEEN FRAME 64 - 65 HAS CORROSION. REMOVED CORROSION & INSTALLED REPAIR ANGLE IAW SRM 53-00-13 FIGURE 202 SHEET 2. NO SRI REQUIRED.