Casualties unknown

2026-01-23: DOUGLAS MD-88 (YV648T) — RUTAS AEREAS, C.A. (RUTACA — SVMI., VE

SVMI., VE

On January 23, 2026, a DOUGLAS MD-88 (registration YV648T) operated by RUTAS AEREAS, C.A. (RUTACA was involved in an aviation accident near SVMI., VE. Investigators recorded the probable cause as: The probable cause of the incident was the presence of foreign object debris (a compass mirror) located within the landing gear lever mechanism, which prevented the full retraction of the gear. This summary draws on records from the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela); 1 related events involving the same aircraft type or operator are linked below.

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

A Rutaca Airlines McDonnell Douglas MD80 experienced a landing gear retraction failure due to a compass mirror lodged in the gear handle mechanism.

What happened

On an unnamed date, a Rutaca Airlines McDonnell Douglas MD80, registration YV648T, departed from General Manuel Carlos Piar International Airport (SVPR) in Puerto Ordaz, Venezuela, bound for Maiquetia International Airport (SVMI). The flight was carrying 89 passengers and 8 crew members.

Shortly after takeoff from runway 08, the captain instructed the first officer to retract the landing gear. The first officer observed that the landing gear lever remained partially engaged and failed to complete its normal retraction cycle. Following established procedures, the crew climbed to 2,000 feet and performed the necessary checks outlined in the Quick Reference Handbook (QRH). When the malfunction could not be corrected, the captain decided to return to the departure airport.

The aircraft successfully performed a landing on runway 08 at Puerto Ordaz. All passengers and crew members were unharmed, and the aircraft sustained no damage during the landing, though the mechanical failure persisted.

The investigation

The investigation focused on the Gear Handle Position Interlock mechanism. Inspectors examined the landing gear lever assembly and identified a piece of foreign object debris (FOD) obstructing the movement. Specifically, the mirror from the first officer's compass was found lodged within the retraction lever mechanism. Maintenance personnel subsequently removed the debris, reinstalled the compass mirror, and performed successful operational tests of the landing gear extension and retraction cycles.

Probable cause

The probable cause of the incident was the presence of foreign object debris (a compass mirror) located within the landing gear lever mechanism, which prevented the full retraction of the gear.

Investigation report by the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela). Original record: https://www.mppt.gob.ve/download/189507/. This page is a structured re-presentation; facts and quotes are in the Junta de Investigacion de Accidentes de Aviacion Civil (JIAAC), Venezuela - MppT.