What was found
VERTICAL CHORD ANGLE HAS A 1.75 INCH LONG CRACK AT FS 178, LBL 7, WL 184. REPAIRED PER DALFORT AVIATION XEA NR X2-53-162. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL CHORD ANGLE HAS A 1.75 INCH LONG CRACK AT FS 178, LBL 7, WL 184. REPAIRED PER DALFORT AVIATION XEA NR X2-53-162. (M)