What was found
INSPECTION FOUND A 2.5 INCH CRACK IN LEFT APU DOOR SKIN AT I/B EDGE, FS 1320, LONGERON 30. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-01, 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 2.5 INCH CRACK IN LEFT APU DOOR SKIN AT I/B EDGE, FS 1320, LONGERON 30. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 2 AND 51-30-2..