What was found
AT C-CHECK, CORROSION ON UPPER WALL OF RIGHT RAM AIR PLENUM CHAMBER 18 INCHES FROM AFT END. SHOT PEENED DAMAGED AREA, COLD WORKED FASTENER HOLES, INSTALLED DOUBLER REPAIR PER SRM 57-30-3, 14' BY 4' AND 11' BY 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, CORROSION ON UPPER WALL OF RIGHT RAM AIR PLENUM CHAMBER 18 INCHES FROM AFT END. SHOT PEENED DAMAGED AREA, COLD WORKED FASTENER HOLES, INSTALLED DOUBLER REPAIR PER SRM 57-30-3, 14' BY 4' AND 11' BY 4.