Casualties unknown

Airline Pilot Loses Control During Crosswind Landing (N648AE)

Dallas, TX, US

On February 24, 2007, an Embraer EMB-145LR (registration N648AE) was involved in an aviation accident near Dallas, TX. Investigators recorded the probable cause as: The pilot's failure to maintain directional control of the airplane while landing with a crosswind. A contributing factor was the prevailing crosswind. 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 2026-06-10Data APIEditorial standards

During a landing on a 7,752-foot runway with a 27-knot crosswind gusting to 38 knots, the pilot lost control and the airplane departed the right side of the runway. Flight data revealed uneven brake pressure and thrust reverser use.

Incident Overview

An airline transport pilot, holding 4,274 hours of flight experience, lost control of the airplane while landing on a runway measuring 7,752 feet in length and 150 feet in width. The prevailing crosswind caused the aircraft to drift off the right side of runway 31R.

Flight Data Recorder Analysis

Analysis of the flight data recorder (FDR) and cockpit voice recorder (CVR) provided detailed insights into the landing sequence. For the first ten seconds after touchdown, the number 3 brake received more brake pressure than the number 1 brake. Additionally, during the four seconds that thrust reversers were utilized, the number 2 engine achieved a higher N1 (fan speed) than the number 1 engine.

Wind Conditions

Just prior to touching down, the air traffic control tower reported winds from 250 degrees at 27 knots, with gusts reaching 38 knots. The operator used tabular data to determine the crosswind component, rather than utilizing a graph. When the graph was consulted, the crosswind component was calculated to be approximately 33 knots.

Aircraft Performance Limitations

According to the Airplane Flight Manual, the maximum demonstrated crosswind for this airplane is 30 knots. The actual crosswind component, as determined by the graph, exceeded this limit.

Conclusion

The factors identified during the investigation include the asymmetric application of brakes and thrust reversers, as well as the crosswind component exceeding the aircraft's demonstrated capability.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20070228X00237. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.