What was found
NR 1 STRUT SIDE SKIN PANEL AT FWD TORQUE BOX ACCESS HOLE FOUND CRACKED WITH STOP DRILL. REPAIRED IAW 54-53-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 STRUT SIDE SKIN PANEL AT FWD TORQUE BOX ACCESS HOLE FOUND CRACKED WITH STOP DRILL. REPAIRED IAW 54-53-01.