No fatalities

2005-10-18: Cessna 208B Grand Caravan (N978FE) — Federal Express - FedEx — Round Rock, United States of America

Round Rock, United States of AmericaFlight

On October 18, 2005, a Cessna 208B Grand Caravan (registration N978FE) operated by Federal Express - FedEx was involved in an aviation accident near Round Rock, United States of America in flight. No fatalities were reported. Investigators recorded the probable cause as: The loss of engine power due to the failure of the engine-driven fuel pump. A contributing factor was the inadequate inspection of the engine driven fuel pump. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781199263Data APIEditorial standards
Aircraft registered N978FE
Aircraft registered N978FE. Photo: Aeroprints.com / CC BY-SA 3.0, via Wikimedia Commons

An aircraft experienced total power loss after takeoff due to engine-driven fuel pump failure. Investigation revealed worn splines and inadequate prior inspection.

Incident Details

A pilot reported an engine failure and total power loss shortly after leveling off at 7,000 feet during an evening flight. The aircraft had been fueled with 65 gallons of Jet-A prior to departure. The pilot, who had accumulated 6,600 flight hours, stated that no abnormalities were noted during engine start or takeoff. After the power loss, the pilot attempted both an air start and a battery-assisted engine restart, but neither was successful.

Investigation Findings

An inspection of the engine, conducted on November 30, 2005, revealed a reddish-brown stain beneath the fuel pump/fuel control unit on the accessory gearbox. When the accessory gearbox was turned, rotation of the drive splines in the fuel pump (splines for the fuel control unit) was not observed. The fuel pump unit was subsequently removed, and reddish-brown staining was present between the fuel pump and the accessory gearbox. The fuel pump drive splines were found to be worn, as were the internal splines on the fuel pump drive coupling. The wear prevented full engagement of the spline drives. Both pieces exhibited evidence of fretting with reddish-brown material present.

At the time of the incident, the airframe had accumulated approximately 130 hours since a maintenance inspection that had included inspection of the fuel pump. The engine had a total time of 9,852 hours, with 5,574 hours since overhaul.

Probable Cause

The investigation determined that the loss of engine power was due to the failure of the engine-driven fuel pump. A contributing factor was the inadequate inspection of the engine-driven fuel pump.