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

August 7, 2021 · Rotary RAF2000 STD · UNREG

Anahuac, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 7, 2021
Injury Outcomes
No injuries (2 uninjured)
Location
Anahuac, TX
Aircraft
Rotary RAF2000 STD (1999)
Tail Number
UNREG
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CEN21LA363

The pilot had just installed a new trim system in the gyroplane and intended to complete a maintenance test flight. During the test flight, the pilot tried to adjust the trim, but nothing happened. The pilot actuated the trim switch again, and the gyroplane pitched up violently. The pilot attempted to override the trim switch but was unable to do so, and the gyroplane rapidly descended from 50 ft to ground impact. The pilot reported after the accident that a trim limit switch was not installed and that the trim system maintenance was probably done incorrectly. Thus, given the available evidence for this investigation, the pilot’s incorrect trim system maintenance likely caused the malfunction during flight and led to the pilot’s loss of gyroplane control.

NTSB Probable Cause

The pilot’s incorrect trim system installation, which resulted in a loss of gyroplane control and impact with terrain.

Full Narrative

On August 7, 2021, about 1115 central daylight time, an unregistered Rotary Air Force RAF 2000 gyroplane sustained substantial damage when it was involved in an accident near Anahuac, Texas. The pilot was uninjured, and the passenger sustained minor injuries. The flight was operated as a Title 14 Code of Federal Regulations Part 91 test flight. The pilot reported that the test flight occurred after a new trim system was installed. The pilot stated that, during the test flight, he tried to adjust the trim, but nothing happened. He actuated the trim switch again, and the gyroplane responded with a “massive pitch up.” He attempted to override the trim switch but was unable to do so, and the gyroplane descended rapidly from 50 ft to ground impact. The figure below shows the gyroplane on its right side in a field. The fuselage, empennage, and rotor blades sustained substantial damage. Figure. Gyroplane wreckage in its resting location (source: Texas Department of Public Safety). The pilot stated that a trim limit switch was not installed, and that the trim system maintenance was “probably” done incorrectly, which is what caused the malfunction during flight. The maintenance logbooks were not made available during the investigation.

Flight

Event TypeAccident
Event Time11:15 CDT
Nearest AirportChambers County (0.5nm SSE)
Runway17
Runway Length1900 ft
Runway Width300 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRotary RAF2000 STD
Tail NumberUNREG
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsSubaru · EJ-22 · Reciprocating
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 76 · None · None
Crew 2Age 65 · Minor

Conditions

ConditionsVMC
LightDaylight
Wind210° @ 4 kt
Visibility10 sm
CeilingNone
Altimeter30.05 inHg
Observation Time11:10
Weather SourceWFAC

Appendix: Source Data