What was found
PANEL 485AL, TOP ATTACH ANGLE ON LT SIDE, 8TH HOLE FWD HAS A CRACK APPROX 3" LONG, JUST BELOW IT. R & R LT LONGERON ANGLE ON PANEL 485AL IAW SRM 54-55-51, FIG 205 AND SRM 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 485AL, TOP ATTACH ANGLE ON LT SIDE, 8TH HOLE FWD HAS A CRACK APPROX 3" LONG, JUST BELOW IT. R & R LT LONGERON ANGLE ON PANEL 485AL IAW SRM 54-55-51, FIG 205 AND SRM 51-40-21.