What was found
FUSELAGE FRAME AT BS 188, OTBD CHORD CRACKED AT WL 208 AND LBL 36. REMOVED, FABRICATED, AND INSTALLED FRAME OTBD CHORD AND WEB SECTION PER SRM 51-10-1, 51-20-1, AND 51-30-2. DOCUMENTED ON N/R 2-387.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT BS 188, OTBD CHORD CRACKED AT WL 208 AND LBL 36. REMOVED, FABRICATED, AND INSTALLED FRAME OTBD CHORD AND WEB SECTION PER SRM 51-10-1, 51-20-1, AND 51-30-2. DOCUMENTED ON N/R 2-387.