What was found
AT C CHECK, NR 1 ENGINE TOP COWL INNER STRUCTURE NR 7 RIB FROM FRONT TO BACK CHAFFED THROUGH. INSTALLED DOUBLER PER SRM 54-10-3, 8 BY 1.25 BY .75, FILLER 1 BY .75, N/R 6126.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, NR 1 ENGINE TOP COWL INNER STRUCTURE NR 7 RIB FROM FRONT TO BACK CHAFFED THROUGH. INSTALLED DOUBLER PER SRM 54-10-3, 8 BY 1.25 BY .75, FILLER 1 BY .75, N/R 6126.