What was found
FUSELAGE SKIN CRACKED AT FASTENER ON RT SIDE ABOVE PYLON, BS 1087. REPAIR WAS ACCOMPLISHED IAW PRI 542147-14, REV 0 AND COMPLIED WITH ER/A 542147-14 REV ORIGINAL. LOG PAGE 2262164 FOR RESTRICTED REPAIR INSTRUCTIONS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT FASTENER ON RT SIDE ABOVE PYLON, BS 1087. REPAIR WAS ACCOMPLISHED IAW PRI 542147-14, REV 0 AND COMPLIED WITH ER/A 542147-14 REV ORIGINAL. LOG PAGE 2262164 FOR RESTRICTED REPAIR INSTRUCTIONS.