What was found
CRACKED WEB GUSSETT INSIDE RIGHT WING LEADING EDGE BETWEEN PANELS 519C AND 520A ABOVE ANTI-ICE VALVE. REPAIRED IAW DC8 SRM 51-3-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED WEB GUSSETT INSIDE RIGHT WING LEADING EDGE BETWEEN PANELS 519C AND 520A ABOVE ANTI-ICE VALVE. REPAIRED IAW DC8 SRM 51-3-0.