What was found
INSPECTION FOUND A 2.25 INCH CRACK IN ANGLE INSIDE LT WING FIXED LEADING EDGE AT NOSE RIB, SLAT STA 0. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-1 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.25 INCH CRACK IN ANGLE INSIDE LT WING FIXED LEADING EDGE AT NOSE RIB, SLAT STA 0. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-1 AND 51-30-2.