As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXISTING FLUSH REPAIR ON SKIN BETWEEN FRAME 2-3 AD, CAUSED BY A FLIGHT TEST INSTALLATION CONFORM TO DRW A536-11822, GOT IN CONFLICTS WITH PTOF CONVERSION. REPAIR MODIFIED WITH A THIRD FASTENER ROW THROUGH ALL LAYERS CONFORM TO REPAIR DRW A536-11822 IAW. EA 6-5311-82922 AND RAS/DABRE/7005422/2005 ISSUE A.