What was found
(CAN) DURING INSPECTION CARRIED OUT IAW AD 64-21-04, CRACK WAS FOUND ON THE REINFORCEMENT ANGLE AT THE AFT END OF THE RIB AT W.L. 201.575
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING INSPECTION CARRIED OUT IAW AD 64-21-04, CRACK WAS FOUND ON THE REINFORCEMENT ANGLE AT THE AFT END OF THE RIB AT W.L. 201.575