DENVER, CO, USA
N133JC
MCDONNELL DOUGLAS DC-10-40
WHILE CLIMBING THROUGH 38,000 FEET, THE AIRCRAFT EXPERIENCED AN UNCONTAINED FAN BLADE SEPARATION IN THE NO. 2 ENGINE. INVESTIGATION REVEALED THAT ONE OF THE FIRST-STAGE COMPRESSOR FAN BLADES (S/N EB2506) HAD SEPARATED ABOUT 8 INCHES ABOVE THE BLADE PLATFORM. FRAGMENTS FROM THE BLADE (#8) HAD EXITED THROUGH THE LEFT FAN COWL IN THREE PLACES AND HAD PENETRATED THE VERTICAL STABILIZER. THE BLADE SEPARATION STEMMED FROM A 0.34-INCH LONG FATIGUE CRACK THAT BEGAN IN A WELD ADJACENT TO A PATCH. THE FAN BLADE HAD BEEN PATCH-REPAIRED EARLIER, AND SUBJECTED TO FOUR NON-DESTRUCTIVE TESTS: X-RAY, FLUORESCENT PENETRANT, ULTRASONIC, AND EDDY CURRENT.
FATIGUE FAILURE AND SEPARATION OF A FIRST-STAGE COMPRESSOR FAN BLADE.
Source: NTSB Aviation Accident Database
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