What was found
LOWER FUSELAGE SKIN FOUND DENTED AT FRAMES 23 - 24, STRINGER 41 - 42L. FOUND OUT OF THE LIMITS IAW SRM 53-10-12-101. CUT OUT DAMAGE IAW SRM 53-10-12-201 PARA 11 FIG 208. INSTALL THE REPAIR PARTS IAW SRM 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE SKIN FOUND DENTED AT FRAMES 23 - 24, STRINGER 41 - 42L. FOUND OUT OF THE LIMITS IAW SRM 53-10-12-101. CUT OUT DAMAGE IAW SRM 53-10-12-201 PARA 11 FIG 208. INSTALL THE REPAIR PARTS IAW SRM 51-40-21.