As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IAH - DURING C-CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WELL FORWARD CORNER FUSELAGE STRAP CRACKED AT FRAME 25. MAINTENANCE INSTALLED AN EXTERNAL DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5310-01088. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)