What was found
INSPECTION FOUND RIVETS POPPED AND FUSELAGE SKIN CORRODED AT STA 948. THE LAST THREE INCHES OF L22R WAS CORRODED THROUGH. THE LONGERON WAS REMOVED AND REPLACED AND THE SKIN WAS REPAIRED IAW SRM 53-02, FIGURE 2A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND RIVETS POPPED AND FUSELAGE SKIN CORRODED AT STA 948. THE LAST THREE INCHES OF L22R WAS CORRODED THROUGH. THE LONGERON WAS REMOVED AND REPLACED AND THE SKIN WAS REPAIRED IAW SRM 53-02, FIGURE 2A.