What was found
AFT FUS EXT SKIN CORRODED (STA 1730.000 - 1740.000 L-28R TO L-30R). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 02-29-08, AD2007-02-02, S/B DC8 S3A080, DWG DOUGLAS SR08530032 AND BOEING MSG 1-7761393332 DATE3D 02-29-08, SEMAN DWG ED-4715 DATED 02-21-08. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.063") (2EA) FILLER (AL7075T6 0.050") (10EA) FINGER DOUBLER (AL7075 0.032") IAW SEMAN DWG NR ED-4715, DOUGLAS DWG SR0850032. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4715, SR08530032, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE) STA 1690.000 - 1766). THIS IS A TEMPORARY REPAIR FORM 24 MONTHS IAW FAA FORM 8100-9 DATED FEB 29-2008