No fatalities

2004-02-04: Ilyushin II-18 (EX-005) — Expo Aviation — Colombo-Bandaranaike, Sri Lanka

Colombo-Bandaranaike, Sri LankaLanding (descent or approach)

On February 4, 2004, an Ilyushin II-18 (registration EX-005) operated by Expo Aviation was involved in an aviation accident near Colombo-Bandaranaike, Sri Lanka during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The crew entered an incorrect altimeter pressure setting, leading to an uncontrolled descent and subsequent impact with the water surface. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781200529Data APIEditorial standards

A cargo flight arriving from Dubai experienced a landing accident at Colombo-Bandaranaike Airport due to an altimeter setting error, resulting in a belly landing and significant aircraft damage.

What happened

During a nighttime cargo operation from Dubai to Colombo, the flight crew began their descent toward Bandaranaike International Airport using GPS and DME navigation. After receiving clearance to descend to FL150, the crew was provided with the local pressure settings of 1009 mb (QNH) and 756 mm Hg (QFE).

An error occurred during the setup of the cockpit instruments when the co-pilot entered a pressure value of 765 mm Hg into the altimeters instead of the correct 756 mm Hg. As the aircraft approached the airport, it was positioned only 60 meters above the sea at a distance of 14 km from the field. The descent continued until the landing gear made contact with the water surface approximately 10.7 km from the threshold of runway 04.

Following the initial impact with the water, the captain attempted a go-around procedure. However, while maintaining an altitude between 60 and 90 meters, the decision was made to continue the approach. Fearing that the undercarriage had sustained structural damage, the pilot executed a belly landing. The aircraft came to a stop 450 meters beyond the runway threshold and 50 meters to the right of the centerline, sliding for 2,230 meters. There were no fatalities among the seven occupants, though the aircraft was a total loss.

Findings

  • The primary cause of the low altitude during descent was the incorrect input of the QFE pressure setting into the altimeters by the co-pilot.

Probable cause

The crew entered an incorrect altimeter pressure setting, leading to an uncontrolled descent and subsequent impact with the water surface.