What was found
DURING C-CHECK, FOUND FUSELAGE SKIN BULGED AT OUTFLOW VALVE, (AD 92-22-08). REPAIRED AFT FUSELAGE SKIN PANEL AND DOUBLER IAW ABX REA D953-17704-MR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND FUSELAGE SKIN BULGED AT OUTFLOW VALVE, (AD 92-22-08). REPAIRED AFT FUSELAGE SKIN PANEL AND DOUBLER IAW ABX REA D953-17704-MR.