What was found
THE RH UPPER TRANSCOWL WAS FOUND TO HAVE CRACK DAMAGE TO THE OUTER SKIN. PERFORMED PERM REPAIR IAW CRJ?00/900 STRUCTURAL REPAIR MANUAL (SRM) 54-21-05, FIGURE 54-21-05-991-801, ITEM 1 (REV.38 DATED JUL. 25, 2020).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE RH UPPER TRANSCOWL WAS FOUND TO HAVE CRACK DAMAGE TO THE OUTER SKIN. PERFORMED PERM REPAIR IAW CRJ?00/900 STRUCTURAL REPAIR MANUAL (SRM) 54-21-05, FIGURE 54-21-05-991-801, ITEM 1 (REV.38 DATED JUL. 25, 2020).