What was found
FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 79 BETWEEN STRINGERS 3L-4L. FABRICATED AND INSTALLED BUSHING RE-PAIR AT FRAME 79 BETWEEN STRINGERS 3L-4L, IAW EMB145 SRM 53-32-01-RE AND EO1-53-20-0424.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 79 BETWEEN STRINGERS 3L-4L. FABRICATED AND INSTALLED BUSHING RE-PAIR AT FRAME 79 BETWEEN STRINGERS 3L-4L, IAW EMB145 SRM 53-32-01-RE AND EO1-53-20-0424.