What was found
EXTERNAL FUSELAGE SKIN DENTED AT THREE EACH LOCATIONS FRAME 23 & 24, STRINGER 23L & 24L. FOUND DENTS TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG 115. FABRICATED REPAIR DOUBLER & INSTALLED 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.
EXTERNAL FUSELAGE SKIN DENTED AT THREE EACH LOCATIONS FRAME 23 & 24, STRINGER 23L & 24L. FOUND DENTS TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG 115. FABRICATED REPAIR DOUBLER & INSTALLED IAW SRM 53-00-11 FIG 232 PG 505 - 506.