As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE BOLT LOOSE AT RIGHT WING FORWARD SPAR. CHECK TORQUE ON THREE OTHER IN THAT SAME ROW. REPLACED 2 BOLTS FOUND TO BE TOO LONG. CHECK TORQUE ON REMAINING 3, CHECK OK. WITCOBOND 2 REPLACEMENT BOLTS, HOLES WITHIN LIMITS. AFT OF FR 26 WING TO FUSELAGE CLOSING ANGLE. (