What was found
DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE TAIL SECTION STRUCTURE LONGERON 17 RT HAS CRACK DAMAGE STA 1770.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CRACKED LONGERON. FABRICATED NEW LONGERON, CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW LONGERON IAW DC8 SRM 53-1-0 PG 1, 53-5-1 FIG 7 SH 1, 51-2-0 FIG 50 SH 37, 51-1-20D, 51-1-21, 51-3-1.