What was found
CLIP ANGLE CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD. TEST RT SIDE, R & R CLIP ANGLE IAW SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLIP ANGLE CRACKED ON AFT SIDE OF REAR PRESSURE BULKHEAD. TEST RT SIDE, R & R CLIP ANGLE IAW SRM 51-42-06.