What was found
DURING C-CHECK, FOUND LEVEL 2 CORROSION IN ANGLE FROM STA 300 TO 320 AND L24L NR 4 PIT. REPAIRED ANGLE AND OUTER SKIN IAW DC-8 SRM 53-2-0 FIG 1B AND 53-2-1 FIG 1. INSTALLED REPAIRED PARTS IAW DC-8 SRM 51-1-8, 51-1-17, 51-1-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND LEVEL 2 CORROSION IN ANGLE FROM STA 300 TO 320 AND L24L NR 4 PIT. REPAIRED ANGLE AND OUTER SKIN IAW DC-8 SRM 53-2-0 FIG 1B AND 53-2-1 FIG 1. INSTALLED REPAIRED PARTS IAW DC-8 SRM 51-1-8, 51-1-17, 51-1-21.