What was found
FUSELAGE EXTERIOR SKIN HAS 1" CRACK FROM FASTENER AT BS 1418 JUST BELOW STR 2 LT. REPAIRED IAW PRI 546964-14AD, REV 0 AND COMPLY WITH ER/A 546964-14AD, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR SKIN HAS 1" CRACK FROM FASTENER AT BS 1418 JUST BELOW STR 2 LT. REPAIRED IAW PRI 546964-14AD, REV 0 AND COMPLY WITH ER/A 546964-14AD, REV ORIGINAL.