What was found
CRACK ON FRAME BS 235 BETWEEN STRINGERS 11-12L. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06, AND DWG 601R34032, REV -V. PRESSURE CHECKS GOOD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FRAME BS 235 BETWEEN STRINGERS 11-12L. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06, AND DWG 601R34032, REV -V. PRESSURE CHECKS GOOD.