Casualties unknown

Northwest Flight 255 Crashes After Takeoff at Detroit Metro Airport (N312RC)

Romulus, MI, US

On August 17, 1987, a Mcdonnell Douglas DC-9-82 (registration N312RC) was involved in an aviation accident near Romulus, MI. 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

Northwest Airlines Flight 255 crashed after takeoff from Detroit Metro Airport. The flaps and slats were not deployed, and the central aural warning system lacked power. Stall warnings activated, but the takeoff warning did not sound.

Accident Summary

Northwest Airlines Flight 255 (NW255) crashed after taking off from runway 3C at Detroit Metro Airport. Witnesses reported that the aircraft rotated for takeoff 1,200 to 1,500 feet from the end of the 8,500-foot runway and lifted off near the runway end. After liftoff, the wings rocked left and right, and the aircraft failed to climb normally. An 18-foot section of the left wing separated when it contacted a light pole 2,760 feet beyond the runway end. The aircraft then rolled steeply to the left, striking poles, a building, and automobiles before crashing into a railroad embankment. The aircraft was destroyed.

Investigation Findings

The investigation revealed that the flaps and slats were in the up/retract position and had not been deployed for takeoff. Neither pilot recited the items of the taxi checklist. Stall warnings were annunciated, but an aural takeoff warning was not annunciated by the Central Aural Warning System (CAWS). It was confirmed that 28-volt DC power was not provided to CAWS power supply #2. The loss of electrical power was traced to a circuit breaker, but no malfunction of the circuit breaker was found.

Flight Operations

Flight 255 was a scheduled passenger service. The crew did not perform the taxi checklist as required. The lack of flap and slat deployment prevented the aircraft from achieving normal climb performance after takeoff.

Aircraft Systems

The flaps and slats are critical for generating lift at low speeds. Their retracted position during takeoff significantly degraded aerodynamic performance. The CAWS failed to provide the aural takeoff warning due to missing power to supply #2. The reason for the circuit breaker condition could not be determined.

For further information, see NTSB/AAR-88/05.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X31759. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.