Accident · 1996-07-06

NTSB case DCA96MA068 · McDonnell Douglas MD-88 · Part 121

What the record says

Event date
1996-07-06
Event type
Accident
Highest injury level
Fatal injury
Aircraft
McDonnell Douglas MD-88 (N927DA)
Operating rule
Part 121
Operator
operator not named in the NTSB record

Probable cause

the fracture of the left engine's front compressor fan hub, which resulted from the failure of Delta Air Lines' fluorescent penetrant inspection process to detect a detectable fatigue crack initiating from an area of altered microstructure that was created during the drilling process by Volvo for Pratt & Whitney and that went undetected at the time of manufacture. Contributing to the accident was the lack of sufficient redundancy in the in-service inspection program. (NTSB Report AAR-98/01)

Source: NTSB case DCA96MA068

Flight crew

Flight-crew details for this event aren't in the NTSB database extract we hold (its coverage starts with 2008 events) — a gap in our data, not an absence of crew.

Facts as the NTSB records them — GroundCheck adds no judgement. Preliminary records may be revised as the investigation proceeds.

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