2 fatalities

2014-10-29: Short 360 (N380MQ) — SkyWay Enterprises — Sint Maarten, Dutch Antilles

Sint Maarten, Dutch AntillesTakeoff (climb)

On October 29, 2014, a Short 360 (registration N380MQ) operated by SkyWay Enterprises was involved in an aviation accident near Sint Maarten, Dutch Antilles during takeoff. 2 people were killed. Investigators recorded the probable cause as: The investigation believes the pilot flying experienced a loss of control while initiating a turn to the required departure heading after takeoff. Flap retraction and associated acceleration caused a somatogravic illusion. 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 1781193327Data APIEditorial standards
Aircraft registered N380MQ
Aircraft registered N380MQ. Photo: CC BY-SA 4.0, via Wikimedia Commons

A Shorts SD3-60 cargo aircraft, registration N380MQ, crashed into the sea shortly after takeoff from Princess Juliana International Airport on October 29, 2014, fatally injuring the two crewmembers. The investigation cited a somatogravic illusion and insufficient crew resource management as key factors.

Accident

On October 29, 2014, at about 1840 Atlantic Standard Time, a Shorts SD3-60, United States registered N380MQ, was destroyed when it crashed into the sea shortly after takeoff from Runway 28 at Princess Juliana International Airport, Sint Maarten, Dutch Antilles. The two crewmembers on board sustained fatal injuries. The aircraft was operated by SkyWay Enterprises Inc. on a scheduled FedEx contract cargo flight to Luis Munoz Marin International Airport, San Juan, Puerto Rico.

At 1839 local, Juliana Tower cleared the aircraft for takeoff from Runway 28 with instructions to maintain heading 230 until passing 4000 feet. At 1840 local, the tower observed the aircraft descending visually, and the radar target and data block disappeared. No distress calls were received. Night conditions and rain prevailed at the time of the accident.

Coast Guard search crews discovered aircraft debris close to the shoreline about 1½ hours later.

Investigation

The Sint Maarten Civil Aviation Authority initiated an investigation in accordance with ICAO Annex 13, joined by Accredited Representatives and advisors from the United States (NTSB/FAA), the United Kingdom (AAIB and Shorts Brothers PLC), and Canada (TSB, TC, PWC). The investigation was organized into groups: Operations, Accident Site and Wreckage, Powerplants, Aircraft Maintenance, Air Traffic Services, Meteorology, and GPS Study.

Flight recorders were not installed nor required on this cargo-configured aircraft; the original FDR and CVR had been removed following conversion to cargo-only operations. A handheld GPS recovered from the submerged wreckage was successfully downloaded. Data showed the aircraft passed the departure runway threshold on takeoff and attained a maximum GPS-recorded altitude of 433 feet at 119 knots groundspeed at 18:39:30. The two remaining data points were over the sea and recorded decreasing altitude and increasing airspeed.

The wreckage was recovered and examined by technical experts. Assessment concluded there were no airframe or engine malfunctions that would have affected the airworthiness of the aircraft; the aircraft struck the sea while under normal engine operation.

Operations and human performance investigators evaluated the evidence and extensive interviews. The investigation concluded that the aircraft departed from the expected flight path in an unusual attitude. The pilot flying most likely experienced a somatogravic illusion as a result of a stressful takeoff and acceleration from flap retraction. The pilot’s reaction to pitch down while initiating a required heading change led to an extreme unusual attitude. Circumstances indicate the pilot monitoring did not perceive, respond, or intervene to correct the flight path and recover from the unusual attitude. The aircraft exceeded normal maneuvering parameters, the crew experienced a loss of control, and lacking adequate altitude for recovery, the aircraft crashed into the sea.

Probable Cause

The investigation believes the pilot flying experienced a loss of control while initiating a turn to the required departure heading after takeoff. Flap retraction and its associated acceleration combined to set in motion a somatogravic illusion for the pilot flying. The pilot flying’s reaction to pitch down while initiating a turn most likely led to an extreme unusual attitude and the subsequent crash. Pilot monitoring awareness of the imminent loss of control and any attempt to intervene could not be determined. Evidence shows that crew resource management (CRM) performance was insufficient to avoid the crash. Contributing factors to the loss of control were environmental conditions including departure from an unfamiliar runway with loss of visual references (black hole), night and rain with gusting winds.