What was found
GOUGE ON EXTERNAL FUSELAGE SKIN AT FRAME 28 PLUS 2 INCHES BETWEEN S43-44L LOWER FWD FUSELAGE. FOUND WITHIN LIMITS IAW SRM 53-21-11. HFEC INSPECTION DONE IAW NTM 51-10-08. NO CRACK INDICATIONS FOUND.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
GOUGE ON EXTERNAL FUSELAGE SKIN AT FRAME 28 PLUS 2 INCHES BETWEEN S43-44L LOWER FWD FUSELAGE. FOUND WITHIN LIMITS IAW SRM 53-21-11. HFEC INSPECTION DONE IAW NTM 51-10-08. NO CRACK INDICATIONS FOUND.