What was found
CRACK FOUND AT FRAME 5A RIGHT TOP MOST HOLE EMANATING FROM RIVET HOLE TO EDGE OF DOUBLER APPROX .25 IN LENGTH.
WILL REPAIR CRACK AT FRAME 5A IAW EA 23-5310-EA-1480 REV. DATED 06/23/2016 FRAME PROCEDURE ON FAA FORM 337.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND AT FRAME 5A RIGHT TOP MOST HOLE EMANATING FROM RIVET HOLE TO EDGE OF DOUBLER APPROX .25 IN LENGTH.
WILL REPAIR CRACK AT FRAME 5A IAW EA 23-5310-EA-1480 REV. DATED 06/23/2016 FRAME PROCEDURE ON FAA FORM 337.