What was found
FWD RT WING ROOT, SPLICE FITTING AT FUSELAGE TO WING FRONT SPAR LWR CHORD IS CRACKED BETWEEN TWO FASTENER HOLES. NDT VERIFIED STA 1156 XCW 118. REMOVED AND REPLACED DOUBLER PER EA 58-5710-59060.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FWD RT WING ROOT, SPLICE FITTING AT FUSELAGE TO WING FRONT SPAR LWR CHORD IS CRACKED BETWEEN TWO FASTENER HOLES. NDT VERIFIED STA 1156 XCW 118. REMOVED AND REPLACED DOUBLER PER EA 58-5710-59060.