What was found
CRACKED ACCESS PANEL 211B, CONTROL STAND AT CONTROL CABIN. MEASURED DAMAGE AREA AND REPAIRED THE ACCESS PANEL WAS FOUND WITHIN LIMITS TO REPAIR THE LONGEST CRACK IN (4 IN2) IAW AMM 25-00-00-340-801, PROCEDURE 8E, METHOD 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED ACCESS PANEL 211B, CONTROL STAND AT CONTROL CABIN. MEASURED DAMAGE AREA AND REPAIRED THE ACCESS PANEL WAS FOUND WITHIN LIMITS TO REPAIR THE LONGEST CRACK IN (4 IN2) IAW AMM 25-00-00-340-801, PROCEDURE 8E, METHOD 1.