What was found
INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF ATTACH ANGLE UPPER END AT STA 980 JUST BELOW LONGERON 15L, AFT LAV OUTBOARD WALL. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF ATTACH ANGLE UPPER END AT STA 980 JUST BELOW LONGERON 15L, AFT LAV OUTBOARD WALL. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 3.