What was found
CRACK ON RING PAN AFT LOWER CORNER BETWEEN BS 294-275 LT AT CABIN PAX. FASTENERS AND DAMAGE WERE REMOVED IAW SRM 51-30-2 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED ANS INSTALLED IAW SRM 51-30-5, 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RING PAN AFT LOWER CORNER BETWEEN BS 294-275 LT AT CABIN PAX. FASTENERS AND DAMAGE WERE REMOVED IAW SRM 51-30-2 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED ANS INSTALLED IAW SRM 51-30-5, 51-30-2.