What was found
DURING AN OPERATIONAL TEST OF THE PASSENGER CREW DOOR DAMPING FUNCTION, FOUND A HARD IMPACT BETWEEN FUSELAGE AND BUFFER OF THE DOOR AT AFT GALLEY AREA. REPLACED THE DAMPER CYLINDER IAW AMM 52-13-14-400-001-B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING AN OPERATIONAL TEST OF THE PASSENGER CREW DOOR DAMPING FUNCTION, FOUND A HARD IMPACT BETWEEN FUSELAGE AND BUFFER OF THE DOOR AT AFT GALLEY AREA. REPLACED THE DAMPER CYLINDER IAW AMM 52-13-14-400-001-B.