What was found
DURING PHASE 48, INSPECTION FOUND FUSELAGE FRAME DAMAGED AT BS 727I ABOVE STRINGER 25 LEFT. INSTALLED REPAIR IAW SRM 51-70-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING PHASE 48, INSPECTION FOUND FUSELAGE FRAME DAMAGED AT BS 727I ABOVE STRINGER 25 LEFT. INSTALLED REPAIR IAW SRM 51-70-11.