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

July 1, 1999 · Mcdonnell Douglas 500-E · N686F

Oklahoma City, OK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 1, 1999
Injury Outcomes
1 injury (1 minor injury), 2 uninjured
Location
Oklahoma City, OK
Aircraft
Mcdonnell Douglas 500-E
Tail Number
N686F
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
FTW99TA183

During a night practice autorotation, after reapplying power, the pilot flared the helicopter too low, and the tailboom contacted the ground. Tail rotor control was lost, and the helicopter came to rest on its right side.

NTSB Probable Cause

During a practice autorotation, the pilot flared the helicopter too low, which resulted in the tailboom contacting the ground. A factor was the dark night light conditions.

Full Narrative

On June 30, 1999, at 2330 central daylight time, a McDonnell Douglas 500-E helicopter, N686F, owned and operated by the Oklahoma City Police Department, was substantially damaged during a night practice autorotational landing at the Downtown Airpark Airport, Oklahoma City, Oklahoma. The commercial pilot and observer were not injured, and the passenger received minor injuries. Dark night visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 public use flight. The local flight departed the Downtown Airpark Airport, about 40 minutes prior to the accident. The pilot reported that after completing patrol duties, the flight returned to the airport. He proceeded to practice some quick stop maneuvers, slope landings, and a hovering autorotation. The pilot further reported that he then entered the traffic pattern and "once [on] downwind ... entered a 180 degree autorotation" for the area east of runway 16 on the north end of the field. During the approach, and "after reapplying power, the flare was executed at too low of an altitude, and the tail boom made contact with the ground." The pilot added that "tail rotor use was lost," and the helicopter came to rest on its right side. The operator reported that an examination of the helicopter revealed that the tailboom was partially separated about three feet aft of its fuselage attaching point. The main drive shaft was damaged, the tail rotor drive shaft was separated at its aft flex coupling, and the right skid was separated.

Flight

Event TypeAccident
Event Time23:30 CDT
Nearest AirportDowntown Airpark (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftMcdonnell Douglas 500-E
Tail NumberN686F
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250C-20B · Turboshaft · 420
Seats4

People & Injuries

Injury Summary1 injury (1 minor injury), 2 uninjured
Fatal0
Serious0
Minor1
Uninjured2
Total3
Crew 1Age 29 · Second Class

Conditions

ConditionsVMC
LightDark Night
Wind120° @ 9 kt
Visibility10 sm
CeilingNone
Altimeter29.00 inHg
Observation Time03:56
Weather SourceWFAC

Appendix: Source Data