What was found
APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK PER SRM 53-00-07.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK PER SRM 53-00-07.