What was found
FUSELAGE STRINGER 25R BETWEEN FS1051.30 AND FS1069.75 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-03, FIGURE 53-61-03-991-806, ITEM 23A (REV. 38 DATED JUL. 25, 2020)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE STRINGER 25R BETWEEN FS1051.30 AND FS1069.75 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-03, FIGURE 53-61-03-991-806, ITEM 23A (REV. 38 DATED JUL. 25, 2020)