What was found
DURING PERFORM NOSE WHEEL WELL MODIFICATION FOUND ANGLE CRACK AT STA 260 - 340 LBL 30. ACCOMPLISHED UPS EO-87000-REQ1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING PERFORM NOSE WHEEL WELL MODIFICATION FOUND ANGLE CRACK AT STA 260 - 340 LBL 30. ACCOMPLISHED UPS EO-87000-REQ1.