What was found
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 1121, FIFTEEN INCHES BELOW RT NEGATIVE PRESSURE LOUVERS. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 1121, FIFTEEN INCHES BELOW RT NEGATIVE PRESSURE LOUVERS. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2.