What was found
INSPECTION FOUND AFT FUSELAGE EXTERNAL SKIN WITH RIVETS LOOSE AND PULLING THROUGH FROM STA 1342 TO 1348, RT SIDE. BULB ANGLES AND A DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3 AND 51-40-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND AFT FUSELAGE EXTERNAL SKIN WITH RIVETS LOOSE AND PULLING THROUGH FROM STA 1342 TO 1348, RT SIDE. BULB ANGLES AND A DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3 AND 51-40-4.