What was found
FUSELAGE FS 364.00 HAS CORROSION FROM STR 25L TO 25R. REMOVED LIGHT CORROSION IAW SRM 51-21-06, STEPS 3B1 THROUGH 5. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-15 AND 53-00-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FS 364.00 HAS CORROSION FROM STR 25L TO 25R. REMOVED LIGHT CORROSION IAW SRM 51-21-06, STEPS 3B1 THROUGH 5. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-15 AND 53-00-00.