What was found
FATIGUE CRACK IN TENSION FITTING COMMON TO 1809.5 CHORD REPLACEMENT. OVERSIZED HOLE, COLD WORKED, INSTALLED OVERSIZED FASTENER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FATIGUE CRACK IN TENSION FITTING COMMON TO 1809.5 CHORD REPLACEMENT. OVERSIZED HOLE, COLD WORKED, INSTALLED OVERSIZED FASTENER.