No fatalities

2008-04-21: Embraer EMB-110 Bandeirante (PT-OCV) — Rico Linhas Aéreas - Rondonia Importaçao e Comercio — Coari, Brazil

Coari, BrazilLanding (descent or approach)

On April 21, 2008, an Embraer EMB-110 Bandeirante (registration PT-OCV) operated by Rico Linhas Aéreas - Rondonia Importaçao e Comercio was involved in an aviation accident near Coari, Brazil during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The failure of the right engine was the result of the failure of the fuel pump due to poor maintenance and a possible use beyond prescribed limits. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781197507Data APIEditorial standards

A twin-engine aircraft suffered a right engine failure due to fuel pump failure from poor maintenance. Overloaded by 503 kg, the crew attempted to divert but landed long, veered off the runway, and struck a ditch. Nine occupants were injured; the aircraft was destroyed.

Incident Overview

A twin-engine aircraft departed Manaus-Eduardo Gomes Airport on a flight to Carauari, carrying 15 passengers and two pilots. Approximately 50 minutes into the flight, while cruising at 8,500 feet, the right engine failed. The crew made several attempts to restart the engine but without success. After informing air traffic control, they were cleared to divert to Coari Airport, located about 37 km from their position.

Approach and Landing

Because the aircraft was overloaded and operating with one engine inoperative, the crew approached Coari Airport runway 28 at a speed higher than the reference speed. The aircraft touched down approximately 700 meters past the runway 28 threshold; the runway length is 1,600 meters. After touchdown, directional control was lost. The airplane veered off the runway to the left, contacted a drainage ditch, tearing off the landing gear, and came to rest 20 meters further.

Occupants and Damage

All 17 occupants evacuated the aircraft. Nine sustained injuries. The aircraft was damaged beyond repair.

Probable Cause

The official investigation determined that the right engine failure resulted from fuel pump failure due to poor maintenance and possible use beyond prescribed limits. The presence of iron oxide inside and outside the fuel pump and lack of cleanliness of internal components indicated probable lack of maintenance. When the right engine stopped, generator No. 1 became responsible for powering the electrical system but was not in good working order; it ceased functioning, leaving only the battery. The crew did not monitor the electrical system and only realized the failure when attempting to extend the landing gear. The emergency hydraulic system was used to lower the gear, but the crew did not return the system selection valve to the normal position, resulting in inoperative brakes and steering after landing. The chain of failures was associated with not reading the checklist after engine failure.

Contributing factors identified include: poor flight preparation; failure to follow standard operating procedures; decision to initiate flight with an overloaded aircraft (by 503 kg); failure to follow checklists during emergencies; lack of effective personnel training by the company; overload and single-engine operation forcing a higher approach speed; improper control use leading to landing 700 meters past the threshold; focus on engine failure leading to neglect of electrical system failures; operations clearing the overloaded flight; lack of flight preparation regarding total weight; and lack of maintenance by the operator.