What was found
LT FUSELAGE LOWER SKIN, FORWARD SPAR FLANGE HAS (2) PULLED RIVETS WITH 1.2500 INCH CRACK AT F.S. 289.0 AND W.S. 29.06. REPAIRED CRACK AND RIVETS IAW SRM 53-90-18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT FUSELAGE LOWER SKIN, FORWARD SPAR FLANGE HAS (2) PULLED RIVETS WITH 1.2500 INCH CRACK AT F.S. 289.0 AND W.S. 29.06. REPAIRED CRACK AND RIVETS IAW SRM 53-90-18.