What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23)On October 18, 2000, 1517 local a us airways flight 1449 a folker F28MK0100 landed RW34 after reporting a hydraulic problem inbound and executed a missed approach. Upon landing the gear doors were observed open and draging on the runway. Company maintenance personnel met the aircraft on the runway, pinned the gear and towed the aircraft to the gate. Passengers were deplanned at the gate and no injuries were reported. An on scene investigation determined a loss of hydrulic fluid in the number 1 system occurred due to faulure of the aft gear right door actuator cylinder pn 12525-21 s/n MC1702. The cyliner upon examination appeared to be cracked prior to a complete failure at the rod end side of the actuator below the gland nut. A company special action tag was attached to the acrator for further analysis of the suspected failed part. The aircraft was ferried to a main maintenance base for repair and or replacement of the main gear doors.
As the FAA filed it
(-23)ON OCTOBER 18, 2000, 1517 LOCAL A US AIRWAYS FLIGHT 1449 A FOLKER F28MK0100 LANDED RW34 AFTER REPORTING A HYDRAULIC PROBLEM INBOUND AND EXECUTED A MISSED APPROACH. UPON LANDING THE GEAR DOORS WERE OBSERVED OPEN AND DRAGING ON THE RUNWAY. COMPANY MAINTENANCE PERSONNEL MET THE AIRCRAFT ON THE RUNWAY, PINNED THE GEAR AND TOWED THE AIRCRAFT TO THE GATE. PASSENGERS WERE DEPLANNED AT THE GATE AND NO INJURIES WERE REPORTED. AN ON SCENE INVESTIGATION DETERMINED A LOSS OF HYDRULIC FLUID IN THE NUMBER 1 SYSTEM OCCURRED DUE TO FAULURE OF THE AFT GEAR RIGHT DOOR ACTUATOR CYLINDER PN 12525-21 S/N MC1702. THE CYLINER UPON EXAMINATION APPEARED TO BE CRACKED PRIOR TO A COMPLETE FAILURE AT THE ROD END SIDE OF THE ACTUATOR BELOW THE GLAND NUT. A COMPANY SPECIAL ACTION TAG WAS ATTACHED TO THE ACRATOR FOR FURTHER ANALYSIS OF THE SUSPECTED FAILED PART. THE AIRCRAFT WAS FERRIED TO A MAIN MAINTENANCE BASE FOR REPAIR AND OR REPLACEMENT OF THE MAIN GEAR DOORS.