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 18, 1983 · Piper PA-22-160 · N2801Z

Brighton, CO

Overview

Report Status
Preliminary report
Event Type
Accident
Date
June 18, 1983
Injury Outcomes
No injuries (2 uninjured)
Location
Brighton, CO
Aircraft
Piper PA-22-160
Tail Number
N2801Z
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DEN83LA144

AFTER ENTERING THE LANDING PATTERN, THE PLT NOTED BINDING OF THE AILERON CONTROL SYSTEM. REPORTEDLY THE AILERON CONTROLS SEEMED TO LOCK, SO HE USED THE RUDDERS FOR DIRECTIONAL CONTROL & LANDED IN A PLOWED FIELD. DURING THE LANDING, THE ACFT NOSED OVER. AN EXAM REVEALED THAT THE PIPER AUTO CONTROL SYS (WING LEVELER) HAD BECOME ENGAGED. WITH THE WING LEVELER ENGAGED, AN EXTRAORDINARY AMOUNT OF CONTROL FORCE WAS REQUIRED TO OVERCOME A GEAR SYS. THE PLT BELIEVED THAT THE WING LEVELER CONTROL, PN 751-519, VIBRATED INTO THE ENGAGED POSITION.

Full Narrative

AFTER ENTERING THE LANDING PATTERN, THE PLT NOTED BINDING OF THE AILERON CONTROL SYSTEM. REPORTEDLY THE AILERON CONTROLS SEEMED TO LOCK, SO HE USED THE RUDDERS FOR DIRECTIONAL CONTROL & LANDED IN A PLOWED FIELD. DURING THE LANDING, THE ACFT NOSED OVER. AN EXAM REVEALED THAT THE PIPER AUTO CONTROL SYS (WING LEVELER) HAD BECOME ENGAGED. WITH THE WING LEVELER ENGAGED, AN EXTRAORDINARY AMOUNT OF CONTROL FORCE WAS REQUIRED TO OVERCOME A GEAR SYS. THE PLT BELIEVED THAT THE WING LEVELER CONTROL, PN 751-519, VIBRATED INTO THE ENGAGED POSITION.

Flight

Event TypeAccident
Event Time09:00 MDT
Nearest AirportBrighton Van-Aire (1nm NNE)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-22-160
Tail NumberN2801Z
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-B2B · Reciprocating · 160
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 59 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind40° @ 5 kt, gusting 5 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point64 F / 0 C
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data