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

February 24, 1982 · Bell 206B · N2272D

Watrous, NM

Overview

Report Status
Preliminary report
Event Type
Accident
Date
February 24, 1982
Injury Outcomes
1 injury (1 fatality)
Location
Watrous, NM
Aircraft
Bell 206B
Tail Number
N2272D
Operator
Doolittle Enterprises
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
FTW82FQA15

THE HELICOPTER STRUCK POWER AND COMMUNICATION LINES AFTER TAKING OFF AT NIGHT. AFTER HITTING THE LINES, IT CRASHED INTO A RAILROAD GRADE AND BRIDGE. THE CRASH SITE WAS ABOUT ONE MILE FROM THE DEPARTURE POINT. AN INSPECTION OF THE ENGINE REVEALED NO PREIMPACT MALFUNCTION. IT WAS NOTED THAT THE CIRCUIT BREAKERS FOR THE FUEL BOOST PUMP AND THE MASTER CAUTION SYSTEMS WERE OPEN. A TOXICOLOGICAL CHECK OF THE PILOT'S BLOOD REVEALED 266 MG PERCENT OF ETHYL ALCOHOL.

Full Narrative

THE HELICOPTER STRUCK POWER AND COMMUNICATION LINES AFTER TAKING OFF AT NIGHT. AFTER HITTING THE LINES, IT CRASHED INTO A RAILROAD GRADE AND BRIDGE. THE CRASH SITE WAS ABOUT ONE MILE FROM THE DEPARTURE POINT. AN INSPECTION OF THE ENGINE REVEALED NO PREIMPACT MALFUNCTION. IT WAS NOTED THAT THE CIRCUIT BREAKERS FOR THE FUEL BOOST PUMP AND THE MASTER CAUTION SYSTEMS WERE OPEN. A TOXICOLOGICAL CHECK OF THE PILOT'S BLOOD REVEALED 266 MG PERCENT OF ETHYL ALCOHOL.

Flight

Event TypeAccident
Event Time21:35 MST
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206B
Tail NumberN2272D
Aircraft CategoryHeli
DamageDestroyed
OperatorDoolittle Enterprises
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft
Seats2

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 53 · Third Class

Conditions

ConditionsVMC
LightDark Night
Wind260° @ 6 kt
Visibility15 sm
CeilingBroken clouds 20000 ft
Temperature / Dew Point11 C / 32 C
Altimeter30.00 inHg
Observation Time21:00

Appendix: Source Data