What was found
ULTRASONIC INSP DETECTED ONE CRACK AT RBL 5.7 BEHIND STIFFENER AT WL 195-207 FS 178. CUT OUT DAMAGED AREA, FABED FILLERS AND DOUBLER; INSTALLED FILLERS AND DOUBLER IAW SRM 53-10-08 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ULTRASONIC INSP DETECTED ONE CRACK AT RBL 5.7 BEHIND STIFFENER AT WL 195-207 FS 178. CUT OUT DAMAGED AREA, FABED FILLERS AND DOUBLER; INSTALLED FILLERS AND DOUBLER IAW SRM 53-10-08 AND 51-40-02.