What was found
INSPECTION 3C, CRACK ON FRAME CLIP IN AFT FUSELAGE BS 2140, X=-10. PERFORMED FRAME CLIP/ANGLE REPAIR IN AFT FUSELAGE AT STA X=2140, X=-10. REF SRM 53-70-07, REPAIR 1, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION 3C, CRACK ON FRAME CLIP IN AFT FUSELAGE BS 2140, X=-10. PERFORMED FRAME CLIP/ANGLE REPAIR IN AFT FUSELAGE AT STA X=2140, X=-10. REF SRM 53-70-07, REPAIR 1, FIGURE 201.