What was found
FUSELAGE FRAME FS 883.5 RHS LOWER INNER CHORD CRACK. CRACK WAS LOCATED ON THE LOWER END OF THE .25 RADIUS TRANSITION BETWEEN CHORD FLANGES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME FS 883.5 RHS LOWER INNER CHORD CRACK. CRACK WAS LOCATED ON THE LOWER END OF THE .25 RADIUS TRANSITION BETWEEN CHORD FLANGES.