As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THERE IS A 2.75 INCH CRACK IN LT FUSELAGE BETWEEN FRAMES 35 AND 36 AT STR 19, 6 INCHES FORWARD OF FRAME 38. CRACK RUNS STRAIGHT ALONG EDGE OF INNER LAP JOINT. REPAIRED SAID CRACK BY CUTTING OUT DAMAGE AND RIVETING PATCH IAW BAE FAX REF BARA/AVRO/3667/99 DATED JULY 6, 1999. (X)