Casualties unknown

Hard Landing During Approach Following Speed Decay and Delayed Thrust Application (N574AA)

Denver, CO, US

On March 21, 2006, a Mcdonnell Douglas DC-9-82 (registration N574AA) operated by American Airlines Inc was involved in an aviation accident near Denver, CO. Investigators recorded the probable cause as: the captain's failure to follow existing company procedures for stabilized approach. **This report was modified on May 23, 2007.**. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards
Aircraft registered N574AA
Aircraft registered N574AA. Photo: Ken Fielding / CC BY-SA 3.0, via Wikimedia Commons

During an approach, the aircraft experienced a hard landing after a speed decrease below Vref and a delayed throttle response. The flight crew had detected a sink rate but thrust did not increase until after touchdown.

Flight Details

The departure, en route, and initial approach phases of the flight were reported by the crew to be without incident. The aircraft was configured for landing with gear down and flaps set to 28 degrees. The landing weight was 127,000 pounds.

Approach and Landing

Air traffic control reported winds from 100 degrees at 6 knots. The aircraft exited a thin cloud layer with a base approximately 1,000 feet above ground level. At 100 feet above the runway, the captain detected a "sinker" and applied thrust to arrest the descent. The aircraft continued to sink during the flare and made a "very firm landing with no bounce."

Data Analysis

Digital Flight Data Recorder (DFDR) data showed that a few seconds before touchdown, airspeed decreased 6 knots below Vref, and pitch attitude changed from 2.1 degrees to 5.3 degrees. A vertical acceleration of 2.032 Gs was recorded at an airspeed of 129.2 knots. Vref was calculated at 135 knots. The pilot reported applying thrust upon detecting the sink rate, but DFDR data indicated that engine pressure ratios (EPRs) did not increase until 7 seconds after touchdown.

Company Procedures

The company's standard operating procedures define a stabilized approach as requiring the aircraft to be at approach speed (Vref plus additives), on the proper flight path with the proper sink rate, and at stabilized thrust. These conditions must be maintained throughout the remainder of the approach; otherwise, a go-around is required.

Cockpit Voice Recorder

The Cockpit Voice Recorder (CVR) contained four channels of audio, but none of the recorded audio was pertinent to the incident. The audio was consistent with the CVR being overwritten or recorded over by subsequent events.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060330X00368. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.