What was found
PIT - DURING FC-6 CHECK INSPECTION, FOUND A 3.5 INCH CRACK IN THE RUDDER RIB NR 4 VERTICAL CHANNEL. INSTALLED DOUBLER REPAIR PER SRM 55-02-07 FIG 3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING FC-6 CHECK INSPECTION, FOUND A 3.5 INCH CRACK IN THE RUDDER RIB NR 4 VERTICAL CHANNEL. INSTALLED DOUBLER REPAIR PER SRM 55-02-07 FIG 3. (M)