What was found
FUSELAGE SKIN CRACK BETWEEN FASTENER HOLES AT BS 2060,STRINGER-26R. REPAIR IAW SRM 53-30-03,FIGURE1. SUBMIT THE CRACKED SKIN TO MFG FOR ANALYSIS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACK BETWEEN FASTENER HOLES AT BS 2060,STRINGER-26R. REPAIR IAW SRM 53-30-03,FIGURE1. SUBMIT THE CRACKED SKIN TO MFG FOR ANALYSIS.