Casualties unknown

2010-11-28: Boeing 747-200 (N482EV) — Evergreen International Airlins, Inc. — About 4 nm Southwest of Chubu Centrair International Airport, JP

About 4 nm Southwest of Chubu Centrair International Airport, JP

On November 28, 2010, a Boeing 747-200 (registration N482EV) operated by Evergreen International Airlins, Inc. was involved in an aviation accident near About 4 nm Southwest of Chubu Centrair International Airport, JP. Investigators recorded the probable cause as: It is possible that the serious incident occurred because the fractured 1st stage LPT rotor blades in the No.2 engine damaged the downstream components during takeoff climb. This summary draws on records from the Japan Transport Safety Board (JTSB); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Japan Transport Safety Board (JTSB)Primary reportUpdated 1785096185Data APIEditorial standards
Aircraft registered N482EV
Aircraft registered N482EV. Photo: tataquax from Japan / CC BY-SA 2.0, via Wikimedia Commons

On November 28, 2010, Evergreen International Airlines Flight 238 experienced a No. 2 engine failure during climb, resulting in strong vibrations and a return landing. No injuries occurred.

Incident Summary

At 06:00 Japan Standard Time on November 28, 2010, a Boeing 747-200 freighter, registered N482EV, operated by Evergreen International Airlines, Inc., departed from runway 36 of Chubu Centrair International Airport as scheduled cargo flight 238, bound for Anchorage International Airport, USA. During the takeoff climb, the No. 2 engine thrust indication dropped and the aircraft experienced strong vibrations. The crew shut down the engine, jettisoned fuel, and returned to the airport, landing at 07:14. The three crew members—the pilot in command, first officer, and flight engineer—were uninjured.

Flight History

According to air traffic control communications and radar tracking, the aircraft pushed back from Spot 117 around 01:55 but returned for maintenance after a brief delay. After corrective actions, it pushed back again around 05:13 and taxied to runway 36, receiving takeoff clearance at 06:00. While climbing through approximately 3,500 feet, about 4 nautical miles southwest of the airport, the crew reported an engine problem and requested fuel dumping for a return. At around 06:07, they confirmed that the No. 2 engine had been shut down. The aircraft landed on runway 36 at 07:14.

Aircraft Damage

The No. 2 engine sustained extensive internal damage. Borescope inspections revealed that the fan blades showed no signs of foreign object ingestion, and the combustion chamber and high-pressure turbines were normal. However, the low-pressure turbine section suffered severe damage: the 1st stage LPT rotor blades (LPT3) were fractured, and downstream stator vanes and rotor blades were progressively damaged. All LPT6 blades were fractured with broken stator vanes. Turbine exhaust case struts were partially fractured, and a small rupture was found in the engine case at the 1 o'clock position. Additionally, fairings of the flap driving system and the inboard aileron had minor collision marks.

Probable Cause

It is possible that the serious incident occurred because the fractured 1st stage LPT rotor blades in the No. 2 engine damaged the downstream components during takeoff climb.

Investigation report by the Japan Transport Safety Board (JTSB). Original record: https://jtsb.mlit.go.jp/eng-air_report/N482EV.pdf. This page is a structured re-presentation; facts and quotes are in the Japan Transport Safety Board (JTSB) - Ministry of Land, Infrastructure, Transport and Tourism.