What was found
AFT FUSELAGE AT INTERNAL FRAME AREA, RIGHT SIDE AT BS 1144 APPROX, COVER CRACK AT UPPER SIDE. REMOVED DAMAGE, PREPPED AREA, APPLIED REPAIR, PRIED REPAIRED AREA IAW B717 SRM 51-70-09, 51-22-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE AT INTERNAL FRAME AREA, RIGHT SIDE AT BS 1144 APPROX, COVER CRACK AT UPPER SIDE. REMOVED DAMAGE, PREPPED AREA, APPLIED REPAIR, PRIED REPAIRED AREA IAW B717 SRM 51-70-09, 51-22-01.