What was found
UPPER FUSELAGE SKIN DENTED BETWEEN STA 210.000 AND 220.000 (4.000 BELOW MAIN CARGO DOOR LWR JAMB) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DWG W90-R09, REV:IR DATED 11-22-04, FAA FORM 8110-3 DATED 11-29-04. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. SMOOTHED BLENDED DAMAGE TWO PLCS WITH R1.0 MIN IAW DWG W90-R09. FABRICATED REPAIR DOUBLER (AL7075-T6 0.090) IAW DWG W90-R09. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 1. INSTALLED REPAIR DOUBLER WITH NEW FASTENERS IAW DWG W90-R09, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1.