What was found
RT FUSELAGE SKIN HAS A 2.5 INCH CRACK AROUND STA 666 JUST ABOVE S33R. CRACK VERIFIED IAW BOEING 767 NDT MANUAL PART 6 CHAP 51-00-11 PAGE 2-3. REPAIRED DAMAGED AREA IAW 767 SRM 53-00-01 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT FUSELAGE SKIN HAS A 2.5 INCH CRACK AROUND STA 666 JUST ABOVE S33R. CRACK VERIFIED IAW BOEING 767 NDT MANUAL PART 6 CHAP 51-00-11 PAGE 2-3. REPAIRED DAMAGED AREA IAW 767 SRM 53-00-01 FIG 201.