What was found
DURING M CHECK, WING TO FUSELAGE ATTACH ANGLE WAS FOUND TO HAVE A 1.25 CRACK. REPAIRED PER EA 99-159285.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING M CHECK, WING TO FUSELAGE ATTACH ANGLE WAS FOUND TO HAVE A 1.25 CRACK. REPAIRED PER EA 99-159285.