What was found
INSPECTION FOUND A 1 INCH CRACK IN AFT CHANNEL OF RT NLG WHEEL WELL FORWARD FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, AND 51-10-6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN AFT CHANNEL OF RT NLG WHEEL WELL FORWARD FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, AND 51-10-6.