What was found
DURING AGING ACFT INSPECTION, FOUND A CRACK IN THE SECOND FASTENER ABOVE S26R COMMON TO THE FUSELAGE FRAME AT BS 492.4. THE CRACK WAS REMOVED BY DRILLING UP THE FASTENER HOLE IN DIAMETER WITH FINAL HOLE SIZE OF 0.875".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING AGING ACFT INSPECTION, FOUND A CRACK IN THE SECOND FASTENER ABOVE S26R COMMON TO THE FUSELAGE FRAME AT BS 492.4. THE CRACK WAS REMOVED BY DRILLING UP THE FASTENER HOLE IN DIAMETER WITH FINAL HOLE SIZE OF 0.875".