1 fatality

Aircraft Collides with Mountain During Approach to Greenville-Spartanburg Airport (N59771)

Brevard, United States of AmericaFlight

On November 12, 1982, a Piper PA-31-350 Navajo Chieftain (registration N59771) operated by Hill-Williford Aviation was involved in an aviation accident near Brevard, United States of America in flight. One person was killed. Investigators recorded the probable cause as: Occurrence #1: in flight collision with terrain/water. Phase of operation: descent - normal. Findings: 1. (f) comm/nav equipment - inoperative; 2. (f) maintenance - not performed - company maintenance personnel; 3. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary report: the U.S. National Transportation Safety Board (NTSB) historical archiveUpdated 2026-07-04Data APIEditorial standards

During a missed approach at Asheville, the flight was cleared to Greenville-Spartanburg. Radar contact was lost en route. The pilot verified position and was cleared to descend to 2,700 feet for an ILS approach. The aircraft impacted a mountain at 3,200 feet, killing the pilot. Investigation revealed uncorrected mechanical issues with navigation equipment.

Accident Overview

After a missed approach at Asheville, the flight was cleared to the Greenville-Spartanburg Airport at Greer, South Carolina. En route to Greer, radar contact was lost. In response to a query from Atlanta Air Route Traffic Control Center (ARTCC), the pilot verified his position as being on the 235° radial of the Spartanburg VOR and 11.9 miles southwest. He was then cleared to descend to 2,700 feet and execute an Instrument Landing System (ILS) approach. The aircraft impacted a mountain at the 3,200 feet level. The wreckage was found on the 235° radial of the Sugarloaf Mountain VORTAC and at 24 miles.

Maintenance History

Review of the aircraft's logbook revealed that mechanical irregularities reported were not corrected for long periods of time. No corrective action was listed for an "outer marker inop aural and visual (needs to be fixed now, since ADF is also inoperative) and 'light in #2 VOR head out'." The marker beacon was described as inoperative on three dates beginning 22 August 1981, and the ADF was described as inoperative on seven dates beginning 8 May 1981. No corrective action was listed for any entry about the marker beacon or ADF.

Pilot and Outcome

The pilot, sole on board, was killed.

Probable Cause

The official probable cause findings state: Occurrence #1: in flight collision with terrain/water. Phase of operation: descent - normal. Findings: 1. (f) comm/nav equipment - inoperative; 2. (f) maintenance - not performed - company maintenance personnel; 3. (f) operation with known deficiencies in equipment - attempted - pilot in command; 4. (f) company-induced pressure - company/operator management; 5. (f) light condition - dark night; 6. (f) weather condition - low ceiling; 7. (f) missed approach - performed - pilot in command; 8. (c) IFR procedure - improper - pilot in command; 9. (c) flight/navigation instrument(s) - improper use of - pilot in command; 10. (f) company-induced pressure - company/operator management; 11. (f) excessive workload (task overload) - pilot in command.

Frequently asked questions

What happened in the 12 Nov 1982 Piper PA-31-350 Navajo Chieftain accident near Brevard, United States of America?

During a missed approach at Asheville, the flight was cleared to Greenville-Spartanburg. Radar contact was lost en route. The pilot verified position and was cleared to descend to 2,700 feet for an ILS approach. The aircraft impacted a mountain at 3,200 feet, killing the pilot. Investigation revealed uncorrected…

Were there any fatalities in the 12 Nov 1982 Piper PA-31-350 Navajo Chieftain accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 12 Nov 1982 involved a Piper PA-31-350 Navajo Chieftain, registration N59771, operated by Hill-Williford Aviation, at Brevard, United States of America.

What was the probable cause of the accident?

Occurrence #1: in flight collision with terrain/water. Phase of operation: descent - normal. Findings: 1. (f) comm/nav equipment - inoperative; 2. (f) maintenance - not performed - company maintenance personnel; 3. (f) operation with known deficiencies in equipment - attempted - pilot in command; 4. (f)…