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

November 10, 2001 · Bell 407 · N517R

Erath, LA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
November 10, 2001
Injury Outcomes
No injuries (1 uninjured)
Location
Erath, LA
Aircraft
Bell 407
Tail Number
N517R
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW02LA033

The pilot inadvertently applied full right pedal while the helicopter was in cruise flight, resulting in a left yaw, the baggage compartment door became open, and the main rotor tie down rope exited the helicopter. The departing rope became entangled in the tail rotor system. Subsequently, the pilot lost anti-torque authority and performed an autorotative landing to an open field.

NTSB Probable Cause

The pilot's inadvertant application of full right pedal which resulted in the baggage compartment door to open in-flight and a tie down rope to become entangled in the tail rotor drive system, and the failure of the tail rotor drive shaft resulting in the loss of anti-torque control.

Full Narrative

On November 10, 2001, approximately 1515 central standard time, a Bell 407 helicopter, N517R, registered to and operated by Industrial Helicopters Inc., of Lafayette, Louisiana, was substantially damaged while in cruise flight in the vicinity of Erath, Louisiana. The commercial pilot was not injured. Visual meteorological conditions prevailed and a company VFR flight plan was filed for the 14 Code of Federal Regulations Part 91 positioning flight. The flight originated at 1500 from an offshore platform, South Marsh 253. According to the pilot, he inadvertently applied full right pedal while the helicopter was in cruise flight, resulting in a left yaw. The baggage compartment door opened and the main rotor tie down rope to exited the helicopter. The departing rope became entangled in the tail rotor system. Subsequently, the pilot lost anti-torque authority and performed an autorotative landing to an open field.

Flight

Event TypeAccident
Event Time15:15 CST
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 407
Tail NumberN517R
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C47B · Turboshaft · 650
Seats7

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 61 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind320° @ 6 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point52
Altimeter30.20 inHg
Observation Time20:55
Weather SourceWFAC

Appendix: Source Data