What was found
THE FUSELAGE SKIN AT STGR 21R AND BETWEEN STA 305 TO 315 WS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERM REPAIR IAW CRJ900 STRUCTURAL REPAIR MANUAL (SRM) 53-21-01-001-002-A01, FIGURE 53-21.-01-991-802, ITEM 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN AT STGR 21R AND BETWEEN STA 305 TO 315 WS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERM REPAIR IAW CRJ900 STRUCTURAL REPAIR MANUAL (SRM) 53-21-01-001-002-A01, FIGURE 53-21.-01-991-802, ITEM 1.