What was found
POSSIBLE CRACK AT RT STA 883.5 FRAME CHORD TRANSITION RADIUS. MADE 0.040 CUTOUT, COLD WORKED HOLE, DRILLED DOUBLER, TREATED AND PRIMED DOUBLER, INSTALLED REPAIR ANGLE IAW 51-40-02, EO 6753A038, 53-A0209, NDT PART G 51-00-16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
POSSIBLE CRACK AT RT STA 883.5 FRAME CHORD TRANSITION RADIUS. MADE 0.040 CUTOUT, COLD WORKED HOLE, DRILLED DOUBLER, TREATED AND PRIMED DOUBLER, INSTALLED REPAIR ANGLE IAW 51-40-02, EO 6753A038, 53-A0209, NDT PART G 51-00-16.