As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TRANSFERRED FROM MIG 2C-40-0054076 EVIDENCE OF POSSIBLE LIGHTNING STRIKE FUSELAGE SEC 43, STA 500K S-1. GROUNDED - YES. REMOVED BLIND RIVET. REAMED HOLE/CUTOUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW B737-900ER SRM 53-00-01-2R-20 CATEGORY B REPAIR ALASKA STEVE NOTIFIED. REINSPECT THRESHOLD IS 50,000 CYCLES REPEAT EVERY 5,500 CYCLES TRACKED BY ENGINEERING. THIS CLOSES THIS DEFECT.