What was found
INSPECTION FOUND A 1.6 INCH CRACK AT BOTTOM OF LEFT CURVED SIDEWALL SUPPORT ANGLE MOUNTED TO FORWARD SIDE OF CIRCUMFERENTIAL STA 950D. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.6 INCH CRACK AT BOTTOM OF LEFT CURVED SIDEWALL SUPPORT ANGLE MOUNTED TO FORWARD SIDE OF CIRCUMFERENTIAL STA 950D. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-3.