Premium research interface

The modern interface for aviation safety intelligence.

Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.

63k+
Reports indexed
1940-2026
Coverage
Recent
Last data refresh
Featured Report

Loading…

Loading featured report…

Loading…
Open Report

Safety trends by operating rule

Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.

Loading trend charts…

Browse the aviation graph

Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.

Last Data Update

By Decade

By Month

Aircraft Manufacturer

More manufacturers

Airports

More airports

Operators

More operators

About

Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.

The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.

FAQs

NTSB Report

December 14, 2005 · Aerospatiale SA-319B · N3194K

Escalante, UT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 14, 2005
Injury Outcomes
2 injuries (2 serious injuries), 4 uninjured
Location
Escalante, UT
Aircraft
Aerospatiale SA-319B
Tail Number
N3194K
Operator
Bureau of Land Management
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
SEA06TA028

The helicopter was manufactured in France for the French Army Air Force. Thirty years later, it was imported to California and given a Certificate of Airworthiness in the normal category by the Anchorage, Alaska, FAA FSDO. The helicopter was flying under contract for the Bureau of Land Management (Public Use) in southern Utah in support of an eradication of feral cattle program. The pilot said that he touched down on a sloping rock outcrop when the helicopter began to oscillate. The pilot pulled up on the collective and the aircraft "suddenly self-destructed." Five of the occupants exited the helicopter under their own power, however, one had been struck by a rotor blade and remained buckled in his seat unconscious. The ground resonance event separated the transmission/rotor system, the engine from the fuselage, and one main rotor blade impacted the cabin. The pilot said that he had experienced at least two incipient ground resonance events with this helicopter during the previous 18 months. During a post-accident examination, numerous maintenance discrepancies were identified, including: improper tire inflations, improper main landing gear hydraulic shock strut pressures, and differential functioning of the main rotor blade drag dampers. The manufacturer's representative said that all of these items have narrow operational tolerances if ground resonance events are to be avoided. Additionally, the landing surface was a "bowl shaped" rock formation with the right main landing wheel up sloped approximately 5 degrees and the nose wheel 3-5 inches nose low.

NTSB Probable Cause

The pilot's inadequate remedial action when ground resonance was encountered during landing. Contributing factors were the rough/uneven terrain and company inadequate maintenance.

Full Narrative

On December 14, 2005, at 1457 mountain standard time, an Aerospatiale SA-319B, Alouette III helicopter, N3194K, was destroyed by ground resonance encountered during a landing attempt in the Grand Staircase-Escalante National Monument, near Escalante, Utah. The commercial pilot and three passengers were not injured; however, two passengers were seriously injured. The helicopter was being operated under contract to the Bureau of Land Management (BLM) by High Country helicopters LLC. of Cedar City, Utah, as a public use flight. Visual meteorological conditions prevailed for the cross-country flight that had originated at Page, Arizona, approximately 30 minutes before the accident. No flight plan had been filed; BLM personnel stated that the purpose of the flight was to distribute hunters for eradication of feral cattle. The pilot stated that he was moving hunting personnel from one location to another. He said that he "took about 5 seconds to settle all three tires to a stable footing and then put the collective down to a full-flat pitch." He said the "aircraft settled into a stable position when suddenly we experienced some ground resonance." The pilot said that he pulled the collective up to lift the helicopter off the ground and "suddenly it self-destructed." The ground resonance event separated the transmission/rotor system, the engine from the fuselage, and one main rotor blade impacted the cabin and struck the helmet of at least one rear seat occupant. Five of the occupants exited the aircraft under their own power, however, the occupant struck by the rotor blade was unconscious and remained buckled in his seat. The pilot said that he had experienced at least two incipient ground resonance events with this helicopter during the previous 18 months. The helicopter was manufactured in France on January 1, 1972, under contract for the French Army Air Force, and after it was decommissioned, it was sold to a company in California in 2002. On December 16, 2002, the helicopter received a Certificate of Airworthiness in the normal category from the Anchorage, Alaska, Federal Aviation Administration (FAA) Flight Standards District Office (FSDO). On March 17, 2005, it was put on a Part 135 certificate by the Salt Lake City, Utah, FAA FSDO. On May 12, 2005, the helicopter was approved and given a Department of Interior, Interagency Data Card, OAS-36B; this card made the helicopter eligible for the BLM contract. On February 8 and 9, 2006, three FAA inspectors, two Department of Interior Air Safety Investigators, and a manufacturer's representative examined the helicopter in Cedar City, Utah. They identified numerous maintenance discrepancies including: improper tire inflations, improper main landing gear hydraulic shock strut pressures, and differential functioning of the main rotor blade drag dampers (tested by hand). The manufacturer's representative said that all of these items have narrow operational tolerances if ground resonance events are to be avoided. Additionally, the landing surface was a "bowl shaped" rock formation with the right main landing wheel up sloped approximately 5 degrees and the nose wheel 3-5 inches nose low.

Flight

Event TypeAccident
Event Time14:57 MST
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftAerospatiale SA-319B
Tail NumberN3194K
Aircraft CategoryHeli
DamageSubstantial
OperatorBureau of Land Management
Engines1
Engine TypeTurboshaft
Engine DetailsTurbomeca · Astazou XIV-B · Turboshaft · 880
Seats7

People & Injuries

Injury Summary2 injuries (2 serious injuries), 4 uninjured
Fatal0
Serious2
Minor0
Uninjured4
Total6
Crew 1Age 42 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point43 C / 7 C
Altimeter30.20 inHg
Observation Time21:56
Weather SourceWFAC

Appendix: Source Data