What was found
LEFT WING KRUGER BOX AREA, CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS APPROX 4" CRACK. REMOVED AND REPLACED REINFORCING ANGLE IAW SRM 51-40-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING KRUGER BOX AREA, CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS APPROX 4" CRACK. REMOVED AND REPLACED REINFORCING ANGLE IAW SRM 51-40-00.