What was found
INSPECTION TYPE: SV, FUSELAGE BS 400 LT NOSE WHEEL AFT CORNER SKIN PANEL 2EA FASTENER HOLE FOUND CRACKED APPROX .1250" LENGTH AT THE LAYER IN 9 O/C DIRECTION, REFER TO NDT TEST REPORT. SKIN REPAIRED IAW RI 53-11-10244, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE: SV, FUSELAGE BS 400 LT NOSE WHEEL AFT CORNER SKIN PANEL 2EA FASTENER HOLE FOUND CRACKED APPROX .1250" LENGTH AT THE LAYER IN 9 O/C DIRECTION, REFER TO NDT TEST REPORT. SKIN REPAIRED IAW RI 53-11-10244, REV A.