What was found
INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1308.5, AT CABIN FLOOR. THE SKIN WAS REPAIRED BY FABRICATING AND INSTALLING A DOUBLER IAW SRM'S 51-21-01 AND 53-00-01, FIGURE 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1308.5, AT CABIN FLOOR. THE SKIN WAS REPAIRED BY FABRICATING AND INSTALLING A DOUBLER IAW SRM'S 51-21-01 AND 53-00-01, FIGURE 4.