What was found
FUSELAGE STRINGER CLIP BS 706, S10L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE STRINGER CLIP BS 706, S10L CRACKED. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. NO CRACKS NOTED.