No fatalities

Helicopter Rolls Over During Aborted Takeoff from Rooftop Helipad (N143CF)

Dallas, TX, US

On September 4, 2003, an Agusta A109E (registration N143CF) was involved in an aviation accident near Dallas, TX. No fatalities were reported. Investigators recorded the probable cause as: The reported loss of engine power for undetermined reasons. A contributing factor was the failure to maintain clearance with the safety fence during the aborted takeoff, which resulted in a dynamic rollover of the helicopter. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A helicopter experienced a loss of engine power during departure from a rooftop helipad, leading to an aborted takeoff. The helicopter struck a safety fence, rotor blades contacted the pad, and it rolled over. No cause was found.

Incident Overview

During a departure from a rooftop helipad, the pilot reported a loss of engine power. The takeoff was aborted, during which a main landing gear struck a safety fence. Subsequently, the main rotor blades contacted the helipad surface, the helicopter rolled over, and it came to rest on the helipad.

Pre-departure and Hover

According to the pilot and medical crew, engine startup and before-takeoff checks were normal. The pilot performed a hover at an altitude of 3 to 4 feet above the helipad to verify engine and systems before departure. As the helicopter began to transition over the edge of the rooftop, the engine warning horn sounded, and warning and caution lights illuminated.

Sequence of Events

The medical crew reported that the engine and rotor noise suddenly decreased, and they noticed a slight drop in altitude. After the helicopter came to rest, the engines were still running at an unknown power level. The pilot and medical crew then shut down the engines.

Post-Accident Examination

Functional tests and examinations of the engines and helicopter systems revealed no anomalies. The reason for the reported loss of engine power was not determined.

Frequently asked questions

What happened in the 4 Sept 2003 Agusta A109E accident near Dallas, TX?

A helicopter experienced a loss of engine power during departure from a rooftop helipad, leading to an aborted takeoff. The helicopter struck a safety fence, rotor blades contacted the pad, and it rolled over. No cause was found.

Were there any fatalities in the 4 Sept 2003 Agusta A109E accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 4 Sept 2003 involved an Agusta A109E, registration N143CF, at Dallas, TX.

What was the probable cause of the accident?

The reported loss of engine power for undetermined reasons. A contributing factor was the failure to maintain clearance with the safety fence during the aborted takeoff, which resulted in a dynamic rollover of the helicopter.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030911X01517. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.