What was found
INSPECTION FOUND A .25 INCH CRACK IN STIFFENER BETWEEN LONGERON 2L AND 3L AT STA 996. THE CRACK WAS STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN STIFFENER BETWEEN LONGERON 2L AND 3L AT STA 996. THE CRACK WAS STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2.