As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE HAS 5.0IN SKIN CRACK AT BS520 +11IN AT STR 4R. / [01] VERIFIED CRACK USING THE FOLLOWING METHODS<BR>ULTRASONIC PHASED ARRAY (UTPA) PER 737 NDT MANUAL; PART 4; 53-30-07<BR>MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION PER 737 NDT MANUAL; PART 6; 53-30-09;[02] C/W EA#22-153-01377;[03] C/W EA 22-153-01377;[04] C/W EA 22-153-01377 C/W;[05] C/W EA 22-153-01377