What was found
EXTERIOR FUSELAGE SKIN DENTED AT THREE PLACES BETWEEN FRAMES 23 & 24 AND STRINGERS 23 & 24L. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG.115. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG.232 PG. 505-506.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERIOR FUSELAGE SKIN DENTED AT THREE PLACES BETWEEN FRAMES 23 & 24 AND STRINGERS 23 & 24L. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG.115. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG.232 PG. 505-506.