What was found
FLOOR SUPPORT ANGLE BETWEEN FRAMES 23 AND 24 IS CRACKED BETWEEN STRINGERS 14 AND 15R. INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FLOOR SUPPORT ANGLE BETWEEN FRAMES 23 AND 24 IS CRACKED BETWEEN STRINGERS 14 AND 15R. INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.