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 16, 1998 · Hughes 269A · N271JB

Hanceville, AL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 16, 1998
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Hanceville, AL
Aircraft
Hughes 269A
Tail Number
N271JB
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
ATL99LA035

The flight instructor reported that the student pilot was flying the helicopter for the dark night takeoff. According to the flight instructor, shortly after climbing through 100 feet, the engine lost power. The flight instructor initiated an autorotation. During the touchdown phase of the autorotation, the helicopter collided with the ground. During the subsequent landing gyrations, the flight instructor stated that, a main rotor blade severed the tail boom, and the helicopter also rolled over. No mechanical problems with the helicopter were discovered during the subsequent post-impact examination. The engine assembly was removed from the airframe and installed in an engine test cell. During the functional test run the engine operated smoothly through all power ranges.

NTSB Probable Cause

The loss of engine power for undetermined reasons. Factors were a dark night and terrain condition.

Full Narrative

On December 15, 1998, at 2010 Central Standard Time, a Hughes 269A, helicopter, N271JB, registered to Wallace State Commercial College, collided with the ground during an attempted takeoff from a heli-pad in Hanceville, Alabama. The instructional flight was operated by Wallace State College under the provisions of Title 14 CFR Part 91 with no flight plan filed. According to the flight instructor, the helicopter sustained substantial structural damage. The flight instructor was not injured, but the student pilot received minor injuries. The accident occurred during the initial takeoff from Hanceville, Alabama. The flight instructor reported that the student pilot was flying the helicopter for a required dark night takeoff. According to the flight instructor, shortly after climbing through 100 feet, the engine lost power. The flight instructor initiated an autorotation (see the attached NTSB Form 6120.1/2 with pilot's statement). During the touchdown phase of the autorotation, the helicopter collided with the ground. During the subsequent landing gyrations, the flight instructor stated that, a main rotor blade severed the tail boom, and the helicopter also rolled over. The helicopter rested in a ditch. No mechanical problems with the helicopter were discovered during the subsequent post-impact examination. The engine assembly was removed from the airframe and installed in an engine test cell. During the functional test run the engine operated smoothly through all power ranges (see attached engine test run).

Flight

Event TypeAccident
Event Time20:10 CST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 269A
Tail NumberN271JB
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFord · HIO-360-B1A · Reciprocating
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 50 · Second Class

Conditions

ConditionsVMC
LightDark Night
Wind330° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point45 C / 30 C
Altimeter30.00 inHg
Observation Time01:53
Weather SourceWFAC

Appendix: Source Data