HONOLULU, HI, USA
N104WA
MCDONNELL DOUGLAS DC-10-30F
AT ROTATION, THE FIRE BELL AND THE #2 ENGINE FIRE WARNING LIGHT CAME ON AND THE CREW NOTED A POWER LOSS ON THE #2 ENGINE. THE TAKEOFF WAS CONTINUED, THE ENGINE SECURED AND THE FIRE BOTTLES DISCHARGED. THE FIRE CONTINUED TO BURN. THE AIRCRAFT CIRCLED AND MADE A NORMAL APPROACH AND LANDING. THE AIRCRAFT BRAKE SYSTEM OVERHEATED DURING THE OVERWEIGHT LANDING, HOWEVER THERE WAS NO OTHER DAMAGE OR INJURIES. TEARDOWN OF THE ENGINE REVEALED THAT A COMPRESSOR BLADE HAD SEPARATED IN FATIGUE ON THE 6TH STAGE HPC ROTOR. THE FAILED BLADE THEN DAMAGED THE 7TH AND REMAINING STAGES AND IGNITED A TITANIUM CASE FIRE. THE ORIGIN OF THE FATIGUE APPEARED TO HAVE PROPAGATED FROM THE DOVETAIL AREA.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
