What was found
DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "B" DOOR JAMB WORN AT STATION 503.000 LONGERON 27-28 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, SRM 51-3-1, FAA FORM 8110-3 08378 DATED 07/11/08, SEMAN DRAWING ED4808 DATED 06/20/08, DC8 SRM 51-1-21, SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B. (S)