What was found
DURING HEAVY MAINTENANCE, CRACK INDICATIONS FOUND IN THE FRAMES 35 - 36 LONGITUDINAL BEAM & PRESSURE PANEL FASTENER HOLES. REPAIRED IAW EC A17-1066-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY MAINTENANCE, CRACK INDICATIONS FOUND IN THE FRAMES 35 - 36 LONGITUDINAL BEAM & PRESSURE PANEL FASTENER HOLES. REPAIRED IAW EC A17-1066-01.