What was found
DURING THE REMOVAL OF J616 FOUND CRACK IN THE RH WHEEL BAY ON THE PRESSURE BULKHEAD PANEL WHERE THE PLUG AND JACK CONNECT TOGETHER. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING THE REMOVAL OF J616 FOUND CRACK IN THE RH WHEEL BAY ON THE PRESSURE BULKHEAD PANEL WHERE THE PLUG AND JACK CONNECT TOGETHER. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS