What was found
INSPECTION FOUND A .375 INCH CRACK IN FUSELAGE SKIN AT STA 1418, LONGERON 2R. REPAIRED IAW SRM 53-04, FIGURE 40.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .375 INCH CRACK IN FUSELAGE SKIN AT STA 1418, LONGERON 2R. REPAIRED IAW SRM 53-04, FIGURE 40.