What was found
EXTERNAL FUSELAGE SKIN CRACKED, BS 1076, LONGERON 14R. REPAIRED CRACKED AREA WITH FILLER END DOUBLER RT PANEL DUCT REMOVED AND REINSTALLED LEAK CHECK COMPLETED IAW AMM 36-00-00-863-804 IAW PRI 545666-14, REV 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERNAL FUSELAGE SKIN CRACKED, BS 1076, LONGERON 14R. REPAIRED CRACKED AREA WITH FILLER END DOUBLER RT PANEL DUCT REMOVED AND REINSTALLED LEAK CHECK COMPLETED IAW AMM 36-00-00-863-804 IAW PRI 545666-14, REV 2.