What was found
PASSENGER CABIN FUSELAGE STIFFENER ANGLE CRACKED FWD OF R1 DOOR AT WL 240. ACFT GROUNDED. R & R ANGLE BETWEEN 12R AND 13R IAW SRM 51-40-02-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PASSENGER CABIN FUSELAGE STIFFENER ANGLE CRACKED FWD OF R1 DOOR AT WL 240. ACFT GROUNDED. R & R ANGLE BETWEEN 12R AND 13R IAW SRM 51-40-02-0G-0.