As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURE INSPECTION IT WAS FOUND THE ENGINE #2 AIR INLET MODULE (REF /B/) INNER BARREL LOWER SKIN WITH SMALL DENTS LOCATED BETWEEN 5.0 AND 7.0 O’CLOCK. THE DENTS WERE EVALUATED AS PER SRM 71-61-01 AD53 AND WERE FOUND OUT LIMITS DUE TO THE DISTANCE BETWEEN THEM. DUE TO IT, THE DISCREPANCIES WAS REPAIRED IAW EMB ETD2025-190-902630 REV. A AND COOPESA ENGINEERING ORDER COO-EO-2025-21800-R01 DTD FEB 24 2025