Casualties unknown

Dual Engine Power Rollback During Cruise Flight at FL330 (N823NK)

Wichita, KS, US

On June 4, 2002, a Mcdonnell Douglas MD-82 (registration N823NK) was involved in an aviation accident near Wichita, KS. Investigators recorded the probable cause as: The engine inlet probes became blocked due to ice crystals, resulting in a false engine pressure ratio (EPR) indication and subsequent retarding of the throttles by the autothrottle system. 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
Aircraft registered N823NK
Aircraft registered N823NK. Photo: Aero Icarus from Zürich, Switzerland / CC BY-SA 2.0, via Wikimedia Commons

An airplane experienced a rollback of engine power on both engines and stalled during cruise at FL330. The crew restarted the engines and made a precautionary landing. Investigation found ice crystals blocked engine inlet probes, causing false EPR indications.

Incident Summary

An airplane encountered a sudden loss of power on both engines while in cruise flight at flight level 330 (FL330). The aircraft was operating on autopilot with the autothrottles engaged at the time. Following the power rollback, the airplane stalled. The flight crew successfully restarted the engines and performed a precautionary landing without any further incidents. Examination of the aircraft and its systems revealed no anomalies that could be attributed to the loss of power.

Weather Conditions and Engine Anti-Ice

Weather conditions at the cruise altitude were consistent with the presence of ice crystals. According to pilot interviews, engine anti-ice was not used prior to the loss of engine power.

Investigation Findings

The investigation determined that the engine inlet probes became blocked due to ice crystals. This blockage resulted in a false engine pressure ratio (EPR) indication, which caused the autothrottle system to retard the throttles. Digital flight data recorder (DFDR) data confirmed that the EPR indication increased while airspeed decreased, pitch attitude increased, altitude remained constant, and the autothrottles had reached the EPR limit.

Analysis of Flight Data

DFDR data showed that the power reduction, corresponding decrease in airspeed, and increase in pitch occurred over approximately five minutes before the engine power rollback. During this period, airspeed dropped from 271.75 knots to 209.25 knots, and pitch increased from 0.9 degrees to 4.91 degrees. In the 24 seconds immediately following the rollback, airspeed continued to decline to a low of 187 knots. The only engine performance parameter recorded by the DFDR was EPR.

Pilot Awareness

Interviews with the pilots indicated that their first indication of a problem occurred just before the airplane stalled.

Probable cause

The engine inlet probes became blocked due to ice crystals, resulting in a false engine pressure ratio (EPR) indication and subsequent retarding of the throttles by the autothrottle system.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020612X00866. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.