What was found
AFTER REMOVAL OF SHIM TO COMPLY WITH TB 206L-94-169. FORWARD BULKHEAD FOUND CRACKED AT RT UPPER AND RT LOWER ATTACH FITTING AREAS. SUSPECT DUE TO STRESS FROM WORKING RIVETS IN INTERCOSTAL ASSEMBLY.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL OF SHIM TO COMPLY WITH TB 206L-94-169. FORWARD BULKHEAD FOUND CRACKED AT RT UPPER AND RT LOWER ATTACH FITTING AREAS. SUSPECT DUE TO STRESS FROM WORKING RIVETS IN INTERCOSTAL ASSEMBLY.