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

June 25, 2001 · Hughes 269A · N8724F

Paso Robles, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 25, 2001
Injury Outcomes
1 injury (1 serious injury), 1 uninjured
Location
Paso Robles, CA
Aircraft
Hughes 269A
Tail Number
N8724F
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
LAX01LA219

The single engine helicopter impacted the ground hard during an autorotational landing following a simulated loss of engine power. The flight instructor was simulating the loss of engine power to his student and noticed the rotor rpm was low when the helicopter was approximately 400 feet above the ground. The instructor ensured the collective was lowered all the way and placed the cyclic forward, but was unable to recover the rotor rpm. He flared the helicopter, but it landed hard resulting in the main rotor blades severing the tail boom.

NTSB Probable Cause

the pilot's failure to maintain rotor rpm during a practice autorotational landing, which resulted in a hard landing.

Full Narrative

On June 24, 2001, approximately 1930 Pacific daylight time, a Hughes 269A single engine helicopter, N8724F, was substantially damaged during a hard landing following an autorotational landing at the Paso Robles Municipal Airport, Paso Robles, California. The flight instructor sustained serious injuries and the student was not injured. The helicopter was registered to and operated by Del Rio Aviation, Paso Robles, under the provision of 14 CRR Part 91 as an instructional flight. Visual meteorological conditions prevailed for the flight, and a flight plan had not been filed. The local instructional flight originated about 1845. According to the instructor pilot, he was demonstrating a simulated loss of engine power and ensuing autorotational landing to the student. He reduced the throttle and lowered the collective. He then pointed out an area to land to the student. As he looked back into the cockpit (approximately 400 feet agl), he noticed the rotor rpm had decreased "drastically" and was dropping even lower. The instructor then ensured the collective was lowered all the way and put the cyclic forward; however, he was unable to regain the lost rotor rpm in time. The instructor then flared the helicopter, but it impacted the ground hard. The main rotor blades severed the tail boom and the helicopter rolled over. The flight instructor indicated he was not sure how the rotor rpm got so low, but commented there were no problems with the engine or the freewheeling unit. The instructor pilot reported having accumulated approximately 2,000 total hours in helicopters, of which about 300 hours were flown in the accident helicopter make and model.

Flight

Event TypeAccident
Event Time19:30 PDT
Nearest AirportPaso Robles Municipal (0nm)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 269A
Tail NumberN8724F
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HO-360 · Reciprocating · 180
Seats4

People & Injuries

Injury Summary1 injury (1 serious injury), 1 uninjured
Fatal0
Serious1
Minor0
Uninjured1
Total2
Crew 1Age 61 · Second Class · Serious

Conditions

ConditionsVMC
LightDaylight
Wind300° @ 11 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point68 F / 43 C
Altimeter29.98 inHg
Observation Time02:53
Weather SourceWFAC

Appendix: Source Data