Boeing 777 N864DA

Summary

On 2 January 2009 at about 15:28 local time, a Boeing 777 registered N864DA, operated by Delta Air Lines, was involved in an incident near Atlanta, Georgia, United States. 257 people were on board and nobody was injured. The aircraft was slightly damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

2 January 2009 at 15:28

Classification

Incident

Location

Atlanta, Georgia, United States

Nearest airport

Atlanta International Airport (KATL)

Coordinates

33.7502, -84.3906

Aircraft

Boeing 777

Registration

N864DA

Category

Airplane

Engines

2

Operator

Delta Air Lines

Operating rule

Part 121: Air Carrier

Phase of flight

Not recorded

Route

Atlanta → Tokyo Narita

Aircraft damage

Minor

NTSB number

ENG09IA002

Nobody was injured.

The fan blade fractured due to a fatigue crack that was the result of the combination of the breakdown of the fan blade lubrication system and residual fatigue life usage following the last overhaul of the fan blade. Contributing to the fracture was the inadequate lubrication schedule established by the engine manufacturer that was not reflective of the operator’s use of the engine.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The Boeing 777 airplane experienced a contained fan blade fracture in the No. 2, right, engine, a Rolls-Royce plc RB.211 Trent 895-17 turbofan, during the takeoff roll at the Hartsfield Jackson Atlanta International Aiport. The examination of the fan blade revealed it had fractured from a fatigue crack that had initiated at the intersection of the convex side aft corner of the shear key slot and bedding flank. The examination of the fan blade also revealed the plasma spray coating was deteriorated and the dry film lubricant was almost completely gone. A survey by the engine manufacturer of the operator's 777 engine usage indicated that because of the loads and lengths of the flights, the operator was operating their Trent 895-17 engines at higher thrust levels with correspondingly high fan rotational speeds, which were still within the engine's operating limits, than any other operator. The survey also indicated the operator was operating its 777 and Trent engines significantly more hours per cycle than any other Trent 895 operator. An analysis by the engine manufacturer indicated that the blade fracture was caused by a combination of the breakdown of the lubrication system and residual fatigue life usage in the blade root following the last overhaul coupled with the high operating stresses in the fan blade from the high thrust settings.

Quoted verbatim from the NTSB record.