What was found
FWD CARGO LH TRANSITION PANEL HAS A PUNCTURE BETWEEN STA. 500-500A. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040. MAT LOSS 100% AT PUNCTURE FABBED AND INSTALLED REPAIR PER B737-900 SRM 53-00-53-2R-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FWD CARGO LH TRANSITION PANEL HAS A PUNCTURE BETWEEN STA. 500-500A. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040. MAT LOSS 100% AT PUNCTURE FABBED AND INSTALLED REPAIR PER B737-900 SRM 53-00-53-2R-5.