What was found
NR 4 PYLON UPPER SPAR LATERAL STIFFENER IS CRACKED. INSTALLED REPLACEMENT ATTACH ANGLE IAW DC8 SRM 54-2-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 4 PYLON UPPER SPAR LATERAL STIFFENER IS CRACKED. INSTALLED REPLACEMENT ATTACH ANGLE IAW DC8 SRM 54-2-1.