As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C DENTS IN FORWARD CARGO FUSELAGE FRAME STA 820, BETWEEN S22R AND S24R (2EA). REMOVED DAMAGE 2 PLACES UPPER L=1.0" W=1.160" LOWER 1.400 W=1.160 IAW EA757-5362-27-A1651. NDT ON REWORK AREA IAW NTM 51-00-00 PT.6 NO CRACKS NOTED. ENLARGED THE TRIM OUT BY .04" ON 2 PLACES UPPER L=1.04" W=1.2 PER EA 757-5362-27-A1651 STEP 3. ACCOMPLISHED ON FINAL EA 757- 5332-27-A1651 AND UPS B757-5310-26677-A.