What was found
FUSELAGE SKIN DENT AT FRAME 23, BETWEEN STRINGER 24L & 25L, THAT IS OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW SRM 53-00-11 FIG 232 PRINCIPLE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DENT AT FRAME 23, BETWEEN STRINGER 24L & 25L, THAT IS OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW SRM 53-00-11 FIG 232 PRINCIPLE 2.