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

October 17, 1983 · Bellanca 7GCBC · N9109L

Capitan, NM

Overview

Report Status
Preliminary report
Event Type
Accident
Date
October 17, 1983
Injury Outcomes
No injuries (2 uninjured)
Location
Capitan, NM
Aircraft
Bellanca 7GCBC
Tail Number
N9109L
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW84LA043

THE PLT REPORTED THAT THE ACFT BOUNCED ON LANDING, RESULTING IN THE COLLAPSE OF THE MAIN GEAR & DAMAGE TO THE PROP & LEFT WING. AN EXAM REVEALED THAT THE U-BOLT WHICH ATTACHES THE LEFT MAIN GEAR STRUT TO THE FUSELAGE HAD FAILED DUE TO TENSILE OVERLOAD. SEVERAL PREEXISTING CRACKS WERE FOUND IN THE RADIUS OF THE U-BOLT. THERE WAS EVIDENCE THAT THE FAILURE OCCURRED AT A CRACK & THAT THE U-BOLT HAD BEEN LOOSE FOR A PERIOD OF TIME PRIOR TO THE ACCIDENT.

Full Narrative

THE PLT REPORTED THAT THE ACFT BOUNCED ON LANDING, RESULTING IN THE COLLAPSE OF THE MAIN GEAR & DAMAGE TO THE PROP & LEFT WING. AN EXAM REVEALED THAT THE U-BOLT WHICH ATTACHES THE LEFT MAIN GEAR STRUT TO THE FUSELAGE HAD FAILED DUE TO TENSILE OVERLOAD. SEVERAL PREEXISTING CRACKS WERE FOUND IN THE RADIUS OF THE U-BOLT. THERE WAS EVIDENCE THAT THE FAILURE OCCURRED AT A CRACK & THAT THE U-BOLT HAD BEEN LOOSE FOR A PERIOD OF TIME PRIOR TO THE ACCIDENT.

Flight

Event TypeAccident
Event Time12:30 MDT
Nearest Airport0nm N
Runway18
Runway Length2300 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBellanca 7GCBC
Tail NumberN9109L
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-A2B · Reciprocating · 150
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 72 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind225° @ 10 kt
Visibility10 sm
CeilingBroken clouds 12000 ft
Temperature / Dew Point61 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data