What was found
DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 40 BETWEEN STRINGER 19R AND 20R SKIN WITH DENT OUT OF LIMITS. INSTALLED REPAIR IAW SRM 53-30-3 FIG 13. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 40 BETWEEN STRINGER 19R AND 20R SKIN WITH DENT OUT OF LIMITS. INSTALLED REPAIR IAW SRM 53-30-3 FIG 13. (M)