As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK WAS FOUND DURING VISUAL INSPECTION OF UPPER LT ENGINE COWLING P/N MY20 551.30-2. CRACKS LOCATED IN THE SHEET METAL STRUT AT THE LOCATION OF THE BOLT WHICH SECURES THE ATTACH FITTING TO THE COWLING. REPAIRED CRACK IN ACCORDANCE WITH FAA FORM 8110-3 DATED 2/11/2010 AND DOCUMENT 96-43-3, REV A DATED 2/11/2010.