What was found
INSPECTION FOUND A .25 AND .125 INCH CRACK IN FUSELAGE SKIN AT LONGERON 1R STA 1337.5. A REPAIR WAS INSTALLED IAW ECRA 5331-01009 AND SRM 53-04, FIGURE 38, VIEW H.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 AND .125 INCH CRACK IN FUSELAGE SKIN AT LONGERON 1R STA 1337.5. A REPAIR WAS INSTALLED IAW ECRA 5331-01009 AND SRM 53-04, FIGURE 38, VIEW H.