What was found
PIT - Q5 - FAIL SAFE CHORD, .75 INCH CRACK, STA 380 AT STR 15R. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM 51-70-11, FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - Q5 - FAIL SAFE CHORD, .75 INCH CRACK, STA 380 AT STR 15R. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM 51-70-11, FIG 1.