What was found
A 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCHES BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCHES BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201.