What was found
EXTERNAL FUSELAGE SKIN HAS SUB-SURFACE CRACK INDICATION AT STR 10L BETWEEN STA 433-434. MAJOR REPAIR ACCOMPLISH PER AMM 53-31-96 FIG 602. AC OK FOR SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERNAL FUSELAGE SKIN HAS SUB-SURFACE CRACK INDICATION AT STR 10L BETWEEN STA 433-434. MAJOR REPAIR ACCOMPLISH PER AMM 53-31-96 FIG 602. AC OK FOR SERVICE.