What was found
MAJOR REPAIR, EXTERNAL FUSELAGE, JUST IN FRONT OF TAIL JACKING POINT, 2 PUNTURES WITH DENT. FABRICATED 3 EACH FILLERS IAW SRM 53-10-12. INSTALLED REPAIR PARTS IAW STEP 20 TO STEP 22 OF SRM 53-10-12-201, PAR 13.C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAJOR REPAIR, EXTERNAL FUSELAGE, JUST IN FRONT OF TAIL JACKING POINT, 2 PUNTURES WITH DENT. FABRICATED 3 EACH FILLERS IAW SRM 53-10-12. INSTALLED REPAIR PARTS IAW STEP 20 TO STEP 22 OF SRM 53-10-12-201, PAR 13.C.