What was found
INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 120-150 BETWEEN LONGERON 24 AND 25R. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 12B, 51-30-2, AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 120-150 BETWEEN LONGERON 24 AND 25R. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 12B, 51-30-2, AND 51-30-5.