What was found
A 1 INCH CRACK WAS FOUND IN THE WEB OF THE UPPER FRAME EMANATING FROM A FASTENER HOLE COMMON TO THE UPPER AND LOWER FRAME LAP JOINT. THE CRACK WAS STOP DRILLED AND THE FRAME REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A 095286-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1 INCH CRACK WAS FOUND IN THE WEB OF THE UPPER FRAME EMANATING FROM A FASTENER HOLE COMMON TO THE UPPER AND LOWER FRAME LAP JOINT. THE CRACK WAS STOP DRILLED AND THE FRAME REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A 095286-14.