As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
H-STAB ACCESS PANEL 311AB LANDING ON LH HAS A CRACK REMOVED DAMAGE IAW SRM 53-00-01 FIG 4 SHT 2. PERFORMED HFEC IAW SOPM 06-10-01-001. NO FURTHER CRACKS REMAIN. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO 8- 5310-T0350635 PT1 TITLE: FUSELAGE - MAIN FRAME - 311AB ACCESS DOOR CUTOUT LANDING CRACKED LH AFT FWD OF STA 2033. MAJOR REPAIR