4 fatalities

2015-04-12: Piper PA-31 Cheyenne (N119RL) — Aircraft Guaranty Owner Trustee (AG Corp) — Fort Lauderdale-Executive, United States of America

Fort Lauderdale-Executive, United States of AmericaLanding (descent or approach)

On April 12, 2015, a Piper PA-31 Cheyenne (registration N119RL) operated by Aircraft Guaranty Owner Trustee (AG Corp) was involved in an aviation accident near Fort Lauderdale-Executive, United States of America during landing or approach. 4 people were killed. Investigators recorded the probable cause as: A rapid onset of smoke and/or fire inflight for reasons that could not be determined due to the postimpact fire and the condition of the wreckage. 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 1781193073Data APIEditorial standards

A pilot reported smoke in the cockpit and declared a mayday before the airplane crashed short of the runway and burned. Engines were developing power at impact. Cause undetermined due to postcrash fire.

Accident Details

After an uneventful personal flight, the pilot contacted the air traffic control tower and was cleared to land. About 36 seconds later, the pilot reported "smoke in the cockpit." When asked to repeat, the pilot repeated the message. The tower controller cleared the pilot to land on any runway. Approximately 47 seconds after the initial smoke call, the pilot declared "mayday mayday mayday mayday mayday (unintelligible)." The airplane then crashed about ¼ mile short of the airport in a wooded area and burned. Security video showed the airplane pitch nose-down suddenly just before impact. The video revealed no visible smoke or fire trailing the airplane before ground impact.

Pilot Information

The pilot reported about 1,221 hours of total flight time on his Federal Aviation Administration first class medical certificate, issued about two months prior to the accident. He completed an initial training course for the airplane make and model one week before the accident.

Aircraft Information

The airplane had recently undergone an annual inspection and extensive upgrades to its avionics. Both the left and right engines displayed contact signatures to their internal components characteristic of engines developing significant power at the time of impact, likely in the mid-to-high power range. The engines displayed no indications of any pre-impact anomalies or distress that would have precluded normal engine operation. Both propeller assemblies broke free from the engine during the crash sequence and the blades on both engines revealed signatures consistent with the development of power at impact.

Investigation Findings

The center fuselage and cockpit areas were completely consumed in the postcrash fire. An examination of all remaining wires, wire bundles, switches, terminals, circuit breakers, electrical components, instruments, and avionics did not reveal evidence of precrash thermal distress. However, a small fire just before impact likely would not have had time to create thermal damage that would be discernable after an extensive postcrash fire.

Probable Cause

The official probable cause is a rapid onset of smoke and/or fire inflight for reasons that could not be determined due to the postimpact fire and the condition of the wreckage.