What was found
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INTERNAL SKIN PANEL BETWEEN FR28 TO FR29 & BETWEEN S35L TO S36L. REPAIRED INTERNAL SKIN PANEL BETWEEN FR28 TO FR29 & BETWEEN S35L TO S36L IAW A319 SRM 53-21-11 FIGURE 215, (SHEET 1).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INTERNAL SKIN PANEL BETWEEN FR28 TO FR29 & BETWEEN S35L TO S36L. REPAIRED INTERNAL SKIN PANEL BETWEEN FR28 TO FR29 & BETWEEN S35L TO S36L IAW A319 SRM 53-21-11 FIGURE 215, (SHEET 1).