What was found
INSPECTION TYPE: C1, NR 1 PYLON UPPER AFT END HAS PN 57567901 CRACKED AT YN 384.942. REMOVED CRACK FROM FITTING BY REMOVING INTEGRAL STIFFNER IAW UPS. ENGINEERING FILE NR DC8-54-20038 AND SAA SK 730-344.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE: C1, NR 1 PYLON UPPER AFT END HAS PN 57567901 CRACKED AT YN 384.942. REMOVED CRACK FROM FITTING BY REMOVING INTEGRAL STIFFNER IAW UPS. ENGINEERING FILE NR DC8-54-20038 AND SAA SK 730-344.