What was found
2S CHECK - EVIDENCE OF REWORK ON FUSELAGE SKIN AT FR66+8 INCHES, S43L. ACCOMPLISHED PERMANENT REPAIR BETWEEN FR66 TO FR67 & BETWEEN S41L TO S44L IAW A319 SRM 53-41-11 PARAG 5.E FIG 207 PAGS 313/314.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
2S CHECK - EVIDENCE OF REWORK ON FUSELAGE SKIN AT FR66+8 INCHES, S43L. ACCOMPLISHED PERMANENT REPAIR BETWEEN FR66 TO FR67 & BETWEEN S41L TO S44L IAW A319 SRM 53-41-11 PARAG 5.E FIG 207 PAGS 313/314.