What was found
NR 2 PYLON, FR 8, RT SIDE, EXTERNAL SKIN PANEL CRACKED. ACCOMPLISHED WELD REPAIR IAW SRM 54-50-00-101-C1, FIGURE 105.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 PYLON, FR 8, RT SIDE, EXTERNAL SKIN PANEL CRACKED. ACCOMPLISHED WELD REPAIR IAW SRM 54-50-00-101-C1, FIGURE 105.