FLIGHT FINDINGSAVIATION OCCURRENCE MAP
Back to map

Tex Air Helcopters Eurocopter AS350B2 accident

24 May 2000 · Patterson, LA, United States

Eurocopter AS350B2 · Accident: airframe, component or system failure en route

From Morgan City, LA (no airport) to 0000 · EI 307B, GM

Report a problem

Event

NTSB case
FTW00LA153
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
Charter & commuter
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Eurocopter AS350B2

Aircraft type
Eurocopter AS350
Category
Helicopter
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N350JG
Onboard fatalities
Unknown
Route
From Morgan City, LA (no airport)To 0000 · EI 307B, GM
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 135: Air Taxi & Commuter
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
En route · cruise
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Airframe, component or system failure
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Pilot in command › Checklist, not followed
  • Pilot in command › Hydraulic system, inadvertent deactivation
  • Rotor system, tail rotor hub pitch change mechanism › Failure

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

The helicopter was in level flight at 1,000 feet msl, when the pilot felt a thump and a yaw. He moved the anti-torque pedals; however, there was no "tail rotor response." A pilot from another helicopter confirmed that the tail rotor was still turning. The pilot reported that he reviewed the emergency procedure for tail rotor failure and flew the helicopter to a nearby airport. The pilot stated that he maintained about 70 knots indicated airspeed and pressed the "HYD" test button for 5 seconds, then returned it to the normal position, as called for in the procedure. The pilot also reported that at this time he turned off the warning horn which alerts the pilot of low main rotor rpm or loss of hydraulic pressure. He completed three shallow approaches to burn off fuel and to see how the helicopter would respond to control movements. While turning left to downwind, during the fourth go-around, the pilot was having trouble controlling the left yaw when he realized the helicopter's hydraulic system had failed. The pilot initiated an autorotation downwind and instructed the passenger to "pull the [fuel flow control] lever off." When the helicopter touched down, "it slid with a yaw left and flipped over coming to rest on its left side." Examination of the cockpit revealed that the console hydraulic test switch (located next to the horn switch) was pressed in (hydraulics off). According to the manufacturer, the hydraulic test switch cuts off hydraulic power; however, the pilot would not lose control assist until the accumulators were depleted. The horn switch was not pressed in (warning horn deactivated, for the horn to function, the switch has to be pressed in). Post accident testing of the hydraulic system revealed no anomalies. Examination of the tail rotor system revealed that the spider bearing inner race was cut through the rotating housing. Examination of the tail rotor spider revealed that the bearing seal exhibited heat damage, and the bearing would not rotate due to small pieces of cage material loose in between the inner and outer races. No evidence of lubrication was present on the race or balls.

Probable cause

the failure of the tail rotor spider bearing, the pilot's failure to follow the proper emergency procedures as stated in the helicopter's checklist by not performing a run-on landing, and the inadvertent deactivation of the hydraulic system.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record FTW00LA153
Event ID
20001212X21000
Case number
FTW00LA153
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 7f31bdcb7e0ef2ce72ceba86eda569bb24274580cc963f1d255910c60875a32d; retrieved 2026-09-18T16:36:08.896Z.