What was found
NOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 RIGHT TUNNEL, APPROXIMATELY 14 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 RIGHT TUNNEL, APPROXIMATELY 14 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5.