What was found
DURING C-CHECK, FOUND 2 INCH CRACK IN WEB LT SIDE AT LT MAIN WHEEL WELL. REPAIRED WEB IAW DC-8 SRM 53-2-0, FIG 1B SHT 3. TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 55-1-8, 55-1-12, 51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND 2 INCH CRACK IN WEB LT SIDE AT LT MAIN WHEEL WELL. REPAIRED WEB IAW DC-8 SRM 53-2-0, FIG 1B SHT 3. TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 55-1-8, 55-1-12, 51-1-20D.