What was found
INSPECTION FOUND A 3 INCH CRACK IN LT AND RT DRAG ANGLES BELOW NR 2 ENGINE AT THIRD BANJO FITTING. THE CRACKS WERE STOP DRILLED AND REPAIR ANGLES WERE INSTALLED IAW SRM 55-20-00, FIGURE 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN LT AND RT DRAG ANGLES BELOW NR 2 ENGINE AT THIRD BANJO FITTING. THE CRACKS WERE STOP DRILLED AND REPAIR ANGLES WERE INSTALLED IAW SRM 55-20-00, FIGURE 3.