What was found
FOUND FUSELAGE FRAME CRACKED AT FS 397.5, STRINGER 21. REPAIRED FRAME IAW L-188 SRM 53-2-3, FIG 2. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND FUSELAGE FRAME CRACKED AT FS 397.5, STRINGER 21. REPAIRED FRAME IAW L-188 SRM 53-2-3, FIG 2. (M)