Casualties unknown

Nose Gear Indication Prompts Return to Maracaibo for RAV DC-9-82 (YV3499)

AEROPUERTO INTERNACIONAL “LA, VE

On November 12, 2023, a DOUGLAS AIRCRAFT DC‐9‐82 (registration YV3499) operated by RUTAS AEREAS DE VENEZUELA RAV, was involved in an aviation accident near AEROPUERTO INTERNACIONAL “LA, VE. This summary draws on records from the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela); 5 related events involving the same aircraft type or operator are linked below.

Sourcesthe Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela)Primary reportUpdated 2026-09-08Data APIEditorial standards

A RAV DC-9-82 returned to Maracaibo after the nose gear failed to indicate locked during climb. Investigation found low nitrogen in the strut, traced to a leaking charge valve. All occupants uninjured.

Incident Overview

A DC-9-82 operated by Rutas Aéreas De Venezuela RAV, S.A. departed Maracaibo's La Chinita International Airport (SVMC) en route to Simón Bolívar International Airport in Maiquetía (SVMI). The aircraft carried a crew of six—one pilot, one first officer, and four cabin crew—along with 115 passengers, totaling 121 persons on board. The planned flight time was 50 minutes.

Nose Gear Malfunction

During initial climb and landing gear retraction, the flight crew observed a cockpit indication that the nose landing gear had not transitioned and locked into its bay. In accordance with the Quick Reference Handbook (QRH), the pilots executed the prescribed procedures and requested clearance from approach control to return to the departure airport. The aircraft landed safely at SVMC at 12:15 UTC.

Occupant and Aircraft Status

All passengers and crew members were uninjured. The aircraft sustained no damage beyond the landing gear system anomaly described.

Investigation Findings

Investigators from the Junta Investigadora de Accidentes (JIA) conducted inspections and troubleshooting. They identified that the nose gear strut contained low levels of nitrogen gas. The nitrogen loss was attributed to a leak through the strut's charging and servicing valve; no other leakage points were detected. The valve was serviced, and the strut was recharged with hydraulic oil and nitrogen. Subsequent functional tests of the nose landing gear system produced satisfactory results, confirming proper operation.

Contributing Factors

No causal factors were explicitly stated in the investigation report. The finding of low nitrogen in the strut due to a leaking valve was noted as the direct condition that likely affected the gear transition indication.

Investigation report by the Venezuelan Civil Aviation Accident Investigation Board (JIAAC Venezuela). Original record: https://www.mppt.gob.ve/download/179404/. This page is a structured re-presentation; facts and quotes are in the Junta de Investigacion de Accidentes de Aviacion Civil (JIAAC), Venezuela - MppT.