What was found
ROA - DURING CX-3 CHECK, FOUND 1 INCH CRACK ON FUSELAGE SKIN AT BS 727 PLUS B PLUS 10 STRINGER 17 RIGHT. DETECTED BY VISUAL/EDDY CURRENT. INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-3 CHECK, FOUND 1 INCH CRACK ON FUSELAGE SKIN AT BS 727 PLUS B PLUS 10 STRINGER 17 RIGHT. DETECTED BY VISUAL/EDDY CURRENT. INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (M)