What was found
RIGHT FUSELAGE SKIN AT FRAME 32 ABOVE STRINGER 19 HAS A .0250 INCH CRACK ORIGINATING AT FASTENER. REPAIR I/P. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE SKIN AT FRAME 32 ABOVE STRINGER 19 HAS A .0250 INCH CRACK ORIGINATING AT FASTENER. REPAIR I/P. (M)