Casualties unknown

Pilot Reports Vacuum Failure and Vertigo Before In-Flight Breakup (N479KC)

Delight, AR, US

On August 6, 1993, a Piper PA-32-300 (registration N479KC) was involved in an aviation accident near Delight, AR. Investigators recorded the probable cause as: THE FAILURE OF THE VACUUM PUMP, AND AN INOPERATIVE TURN COORDINATOR. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE: THE PILOT'S LOSS OF CONTROL OF THE AIRPLANE AS A RESULT OF SPATIAL DISORIENTATION, THE PILOT EXCEEDING THE DESIGN STRESS LIMITS OF THE… 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 2026-07-04Data APIEditorial standards

After cancelling IFR and proceeding VFR, a pilot reported losing vacuum, experiencing vertigo, and difficulty holding heading. The airplane subsequently broke up in flight.

Incident Overview

A pilot flying an unspecified aircraft cancelled their IFR flight plan after being cleared for the localizer approach to Texarkana Airport, indicating an intention to proceed VFR to Nashville, Arkansas. Shortly thereafter, the pilot reported being in clouds, having lost vacuum pressure, and that the turn coordinator was inoperative. The pilot stated they were on the verge of vertigo.

Controllers's Response

An air traffic controller attempted to vector the pilot back to Texarkana, but noted the pilot was having difficulty maintaining a heading. The aircraft subsequently broke up in flight.

Aircraft Damage

Examination of the wreckage revealed the left wing spar was twisted upward and aft, the right wing spar was bent slightly downward and aft, and the vertical stabilizer spar was bent aft.

Vacuum Pump Examination

Laboratory examination of the vacuum pump determined that the drive shaft had sheared in torsion, the rotor had broken due to overstress, and the vanes were worn. The condition of the pump indicated failure consistent with the reported loss of vacuum.

Turn Coordinator Status

The turn coordinator, which exhibited an electrical impedance of 10,000 ohms, was found to be inoperative. However, investigators could not determine whether the unit had failed prior to the accident flight or during the flight.

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Frequently asked questions

What happened in the 6 Aug 1993 Piper PA-32-300 accident near Delight, AR?

After cancelling IFR and proceeding VFR, a pilot reported losing vacuum, experiencing vertigo, and difficulty holding heading. The airplane subsequently broke up in flight.

What aircraft was involved and where did it happen?

The accident on 6 Aug 1993 involved a Piper PA-32-300, registration N479KC, at Delight, AR.

What was the probable cause of the accident?

THE FAILURE OF THE VACUUM PUMP, AND AN INOPERATIVE TURN COORDINATOR. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE: THE PILOT'S LOSS OF CONTROL OF THE AIRPLANE AS A RESULT OF SPATIAL DISORIENTATION, THE PILOT EXCEEDING THE DESIGN STRESS LIMITS OF THE AIRPLANE, AND THE WEATHER CONDITIONS (CLOUDS).

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X13129. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.