What was found
UPPER CUSP EXTRUSION FITTING CRACKED 1.000, STA 857.000 L-19R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER CUSP EXTRUSION FITTING CRACKED 1.000, STA 857.000 L-19R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9.