What was found
INSPECTION FOUND A 4.5 INCH CRACK IN FRAME AT STA 180, LONGERON 5L AND 6L. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 36.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4.5 INCH CRACK IN FRAME AT STA 180, LONGERON 5L AND 6L. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 36.