What was found
NR 1 ENGINE NACELLE STRUT ACCESS PANEL NR 433GR CUTOUT AREA AT STA 120, INTERNAL SURFACE CORROSION. CORRODED PANEL NR 433GR R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE NACELLE STRUT ACCESS PANEL NR 433GR CUTOUT AREA AT STA 120, INTERNAL SURFACE CORROSION. CORRODED PANEL NR 433GR R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.