What was found
DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE.- SPLICE FITTING CRACKED 1", L-17L, STA 1566.000. REPAIRED PER ALL APPROVED DATA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE.- SPLICE FITTING CRACKED 1", L-17L, STA 1566.000. REPAIRED PER ALL APPROVED DATA.