What was found
ROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND 2 CRACKS .875 INCH AND .125 INCH IN LENGTH AT FUSELAGE SKIN AT STRINGER 16L BS 727A. CONTAINED CRACKS AND INSTALLED DOUBLER, REPARIED PER SRM 53-30-3 FIG 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND 2 CRACKS .875 INCH AND .125 INCH IN LENGTH AT FUSELAGE SKIN AT STRINGER 16L BS 727A. CONTAINED CRACKS AND INSTALLED DOUBLER, REPARIED PER SRM 53-30-3 FIG 1. (M)