What was found
CONTINUED CRACK ON AFTER TO PREVIOUS REPAIR AT DOOR JAMB AT STA Y=46, X=29 AT NOSE WHEEL WELL STRUCTURE. DOOR JAMB WAS REPAIRED IAW ETI-88-15-033, REV 4 AND ER/A 531399-14, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CONTINUED CRACK ON AFTER TO PREVIOUS REPAIR AT DOOR JAMB AT STA Y=46, X=29 AT NOSE WHEEL WELL STRUCTURE. DOOR JAMB WAS REPAIRED IAW ETI-88-15-033, REV 4 AND ER/A 531399-14, REV ORIGINAL.