What was found
AFTER REMOVAL OF FUSELAGE SKIN AT BS 590-660, FOUND TWO CRACKS AT BS 625, STR 16L. REPAIRED IAW SRM 53-00-03, FIG 201, REP 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL OF FUSELAGE SKIN AT BS 590-660, FOUND TWO CRACKS AT BS 625, STR 16L. REPAIRED IAW SRM 53-00-03, FIG 201, REP 1.