17 fatalities

1985-06-23: Embraer EMB-110 Bandeirante (PT-GJN) — Transportes Aéreos Regionais da Bacia Amazônica - TABA — Juara, Brazil

Juara, BrazilLanding (descent or approach)

On June 23, 1985, an Embraer EMB-110 Bandeirante (registration PT-GJN) operated by Transportes Aéreos Regionais da Bacia Amazônica - TABA was involved in an aviation accident near Juara, Brazil during landing or approach. 17 people were killed. Investigators recorded the probable cause as: A left engine faulty fuel injection nozzle caused a blow torch effect, damaging compressor turbine vane ring and causing thermal fatigue and loss of one of the turbine blades. The resulting imbalance ruptured the starting control bypass fuel return. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 6 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781218363Data APIEditorial standards

An aircraft declared an emergency after left engine failure during climb, then went out of control on final approach, struck the ground, veered into a fire truck, and burned. All 17 occupants were killed.

Emergency Declaration

After departing from Juara Airport, the crew of an aircraft declared an emergency during the climb due to a failure of the left engine. Air traffic control cleared the crew to return to the airport, and rescue teams were dispatched to stand by.

Loss of Control

On final approach, during the last segment of the landing, the aircraft went out of control and struck the ground. It then veered off the runway and collided with an emergency vehicle, identified as a fire bombers truck, before coming to rest in flames.

Fatalities

All 17 occupants aboard the aircraft were killed. No injuries were reported on the ground.

Probable Cause

Investigation determined the probable cause to be a faulty fuel injection nozzle in the left engine, which created a blow torch effect. This effect damaged the compressor turbine vane ring, leading to thermal fatigue and the loss of one turbine blade. The resulting imbalance ruptured the starting control bypass fuel return line.