Casualties unknown

2014-10-12: Cirrus SR20 (N176CD) — KOREA PILOT SCHOOL — At Nishikata, Ibusuki city, Kagoshima prefecture, JP

At Nishikata, Ibusuki city, Kagoshima prefecture, JP

On October 12, 2014, a Cirrus SR20 (registration N176CD) operated by KOREA PILOT SCHOOL was involved in an aviation accident near At Nishikata, Ibusuki city, Kagoshima prefecture, JP. Investigators recorded the probable cause as: It is highly probable that the accident was occurred as a result of the engine of N176CD halt during the flight and not being able to start in the air, resulting in the damage of the aircraft during the forced landing. 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

On October 12, 2014, a Cirrus SR20 (N176CD) experienced an engine halt during a ferry flight from Saipan to Gimpo, forcing a landing in a grass field in Kagoshima Prefecture. The pilot was uninjured; the aircraft was destroyed.

Overview

On Sunday, October 12, 2014, at approximately 14:30 Japan Standard Time, a Cirrus SR20 aircraft registered as N176CD and owned by Korea Pilot School sustained damage during a forced landing in a grass field in Nishikata, Ibusuki City, Kagoshima Prefecture, Japan. The aircraft was being ferried from Saipan International Airport to Gimpo International Airport in the Republic of Korea. The pilot, who was contracted for the ferry flight, was the sole occupant and reported no injuries. The aircraft was destroyed but did not catch fire.

Flight Details

The aircraft departed Saipan International Airport at about 05:37 JST under visual flight rules, with an intended route via NATSS, G339 airway, Kagoshima VORTAC, A582 airway, and Anyang VOR. The flight plan indicated a total estimated elapsed time of 12 hours 30 minutes, with fuel onboard for 15 hours 35 minutes. Prior to departure, the pilot filled the main wing tanks with a total of 56 gallons, the front ferry tank with 38 gallons, and the rear ferry tank with 70 gallons, for a total of 164 gallons. After takeoff, the pilot sequentially used the right wing tank, left wing tank, and then switched to the rear ferry tank about one hour after departure.

Engine Failure and Forced Landing

At around 14:19 JST, while approaching the KINKO reporting point near Kinko Bay, the pilot noticed the engine sound surging and the fuel flow gauge fluctuating. The aircraft, which had been maintaining altitude via autopilot, began to descend. The pilot, suspecting low fuel in the rear ferry tank, switched to the front ferry tank but the surging continued. Approximately 15 to 20 seconds later, the engine stopped and the fuel flow indicator showed zero. The propeller continued windmilling at about 1,500 rpm.

The pilot attempted to restart the engine by activating the auxiliary fuel pump in the BOOST position and following the airstart procedures from the Pilot's Operating Handbook, but the engine did not restart. He then switched to the right and left wing tanks and attempted airstart procedures again, without success. At 14:19:53, the pilot declared an emergency to Kagoshima Radar and requested radar vectors to the nearest airport. The aircraft continued descending, and at 14:29:46, its groundspeed became zero. The forced landing occurred in a grass field.

Probable Cause

According to the Japan Transport Safety Board, it is highly probable that the accident resulted from the engine halting during flight and the inability to restart it in the air, leading to damage during the forced landing. The engine halt was somewhat likely caused by fuel exhaustion in the rear ferry tank, leading to power loss. When the pilot opened the fuel selector valve for the front ferry tank (which still contained fuel) without closing the rear ferry tank's valve, air from the empty rear tank entered the fuel line due to suction from the engine-driven fuel pump, hindering fuel supply. The inability to restart the engine in the air was somewhat likely because the air in the fuel line made it difficult for the engine-driven fuel pump to suck fuel, and the auxiliary fuel pump could not quickly remove the air that obstructed the pump's suction.

Investigation report by the Japan Transport Safety Board (JTSB). Original record: https://jtsb.mlit.go.jp/eng-air_report/N176CD.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.