No fatalities

Serious Incident Involving DHC-8-202 OY-GRJ at Nuuk

Nuuk (BGGH), DK

On May 30, 2019, an aircraft (registration OY-GRJ) was involved in an aviation accident near Nuuk (BGGH), DK. No fatalities were reported. Investigators recorded the probable cause as: The actual loading of the aircraft beyond forward CG operational limitations reduced the aircraft rotation ability during the take-off roll resulting in an aborted take-off. This summary draws on records from the Danish Accident Investigation Board (Havarikommissionen); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Danish Accident Investigation Board (Havarikommissionen)Primary reportUpdated 2026-10-18Data APIEditorial standards
Aircraft registered OY-GRJ
Aircraft registered OY-GRJ. Photo: Gordon Leggett / CC BY-SA 4.0, via Wikimedia Commons

A De Havilland Canada DHC-8-202 experienced an aborted take-off due to a forward center of gravity beyond operational limits, reducing rotation ability. No injuries or damage reported.

History of the Flight

On 30 May 2019, a De Havilland Canada DHC-8-202, registration OY-GRJ, was operating a scheduled domestic passenger flight from Nuuk (BGGH) to Kangerlussuaq (BGSF) under instrument flight rules. The aircraft carried three crew members and 29 passengers. Before departure, an off-duty crew member moved from the cockpit jump seat to a passenger seat to mitigate a forward center of gravity issue. The commander served as pilot monitoring, while the first officer was pilot flying.

During the take-off roll on runway 05, the first officer applied normal backpressure to the elevator at the rotation callout but received no positive response. Full aft backpressure was then applied, but the aircraft did not rotate. The first officer aborted the take-off by retarding power levers to DISC and applying maximum anti-skid braking. The aircraft stopped approximately 50 meters before the runway end. After discussing the situation, the crew taxied back to the apron and requested an external inspection of the wheel brakes. The commander briefed the passengers.

Meteorological and Runway Information

The incident occurred during daylight in visual meteorological conditions. Nuuk Aerodrome Flight Information Service reported runway 05 in use, wind 330° at 5 knots, QNH 1014, temperature 10°C, dry runway, and visibility greater than 10 km. Before engine start, wind was reported as 330° at 3 knots.

Mass and Balance Analysis

Pre-flight mass and balance calculations using standard masses for crew, passengers, and carry-on baggage indicated the center of gravity was within aircraft limitations. However, post-flight calculations using actual masses showed the center of gravity was forward of the operational forward CG limitation. This exceeded the allowable limit and reduced the aircraft's ability to rotate during the take-off roll.

Conclusion

The serious incident resulted from the aircraft being loaded beyond its forward center of gravity operational limitation, which prevented normal rotation and led to an aborted take-off. No injuries or aircraft damage occurred.

Probable cause

The actual loading of the aircraft beyond forward CG operational limitations reduced the aircraft rotation ability during the take-off roll resulting in an aborted take-off.