Casualties unknown

2026-03-05: GULFSTREAM 690C (YV1892) — INVERSIONES ALAS ALTAS C.A. — SVAD., VE

SVAD., VE

On March 5, 2026, a GULFSTREAM 690C (registration YV1892) operated by INVERSIONES ALAS ALTAS C.A. was involved in an aviation accident near SVAD., VE. Investigators recorded the probable cause as: The primary causal factor was the **permeability of the aerodrome perimeter**, specifically the lack of a continuous and robust fence to segregate aircraft movement areas from wildlife. This summary draws on records from the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela).

Sourcesthe Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela)Primary reportUpdated 1781150548Data APIEditorial standards

A Gulfstream Commander aircraft sustained significant damage after striking a flock of sheep during landing at an uncontrolled aerodrome in Falcón, Venezuela.

What happened

On March 5, 2026, a Gulfstream Commander 690C, registration YV1892, was performing a flight from General José Antonio Anzoátegui International Airport to Adicora Aerodrome. The aircraft was carrying seven people, including two crew members and five passengers.

During the final approach at Adicora, the pilot performed a low pass over runway 08 to ensure the surface was clear of obstacles. Following the landing roll, after approximately 280 meters of travel, a flock of between 15 and 20 sheep suddenly crossed the runway. The crew was unable to avoid the impact. The pilot maintained control to keep the aircraft centered on the runway, and the crew immediately shut down the fuel, electrical, and hydraulic systems. There were no fatalities or injuries, though the aircraft sustained significant damage.

The investigation

The investigation involved a physical inspection of the aircraft and its engines, non-destructive testing (NDT), and interviews with the crew. Investigators examined the airframe, landing gear, and the two Garrett Aireresearch TPE3X31-5-254K turboprop engines.

Technical inspections revealed several points of impact damage:

  • Both propellers exhibited bent blades due to the collision with the animals.
  • The DME/transponder antenna was detached from the lower fuselage.
  • Damage was found on the left main landing gear drag brace and the right main landing gear door.
  • The right engine radiator air intake grilles were deformed, and a hydraulic brake line was ruptured.

Detailed inspection of the engines via NDT revealed that the right engine's torque shaft was fractured and the torque sensor was damaged due to debris generation from a cam assembly failure.

Probable cause

The primary causal factor was the **permeability of the aerodrome perimeter**, specifically the lack of a continuous and robust fence to segregate aircraft movement areas from wildlife. This infrastructure failure, combined with the uncontrolled nature of the aerodrome and the absence of Air Traffic Control (ATC) to provide warnings, allowed the sheep to enter the runway area.

Investigation report by the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela). Original record: https://www.mppt.gob.ve/download/190038/. This page is a structured re-presentation; facts and quotes are in the Junta de Investigacion de Accidentes de Aviacion Civil (JIAAC), Venezuela - MppT.