What was found
Q1 CHECK - 2 CRACKS ON FUSELAGE FRAME INBOARD CHORD AT BS 616, WL 203, LBL 64.5. REPAIRED FUSELAGE FRAME INBOARD CHORD AT BS 616, WL 203, LBL 64.5 IAW TYPICAL REPAIR TR 737-5362-10-0023.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
Q1 CHECK - 2 CRACKS ON FUSELAGE FRAME INBOARD CHORD AT BS 616, WL 203, LBL 64.5. REPAIRED FUSELAGE FRAME INBOARD CHORD AT BS 616, WL 203, LBL 64.5 IAW TYPICAL REPAIR TR 737-5362-10-0023.