What was found
FUSELAGE SKIN CRACKS AROUND 2 RIVETS AT FRAME 75 BETWEEN STGR 01R-02R. C/A: ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN CRACKS AT FRAME 75 BETWEEN STRINGERS 01R-02R, IAW EMB 145 SRM 53-31-01RE FIGURE 219 SHEET 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKS AROUND 2 RIVETS AT FRAME 75 BETWEEN STGR 01R-02R. C/A: ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN CRACKS AT FRAME 75 BETWEEN STRINGERS 01R-02R, IAW EMB 145 SRM 53-31-01RE FIGURE 219 SHEET 2.