What was found
INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT STA 1087, LONGERON 2L. REPAIRED IAW SRM 53-04, FIGURE 27.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT STA 1087, LONGERON 2L. REPAIRED IAW SRM 53-04, FIGURE 27.