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

November 29, 1986 · Hiller UH-12B · N48209

Capac, MI

Overview

Report Status
Preliminary report
Event Type
Accident
Date
November 29, 1986
Injury Outcomes
No injuries (1 uninjured)
Location
Capac, MI
Aircraft
Hiller UH-12B
Tail Number
N48209
Operator
Mark W Smith
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI87LA045

TEN MINUTES AFTER TAKEOFF AND JUST PRIOR TO LETDOWN FROM 350 FEET AGL A MAIN ROTOR BLADE DRAG STRUT FAILED DUE TO PROGRESSIVE FATIGUE THROUGH A THREADED PORTION OF THE STRUT. ONLY PARTIAL CONTROL OF THE HELICOPTER WAS POSSIBLE AFTER THE FAILURE. THE PILOT LOST CONTROL OF THE AIRCRAFT AT ONE POINT, BUT REGAINED CONTROL IN TIME TO PERFORM A HARD, SLIDING LANDING IN A FIELD. SUBSTANTIAL DAMAGE OCCURRED. THE ENTIRE SEQUENCE OF EVENTS TOOK PLACE IN 10-15 SECONDS. THE PLT HAD A PRIVATE CERT FOR FIXED WING AND A STUDENT CERT FOR ROTORCRAFT.

Full Narrative

TEN MINUTES AFTER TAKEOFF AND JUST PRIOR TO LETDOWN FROM 350 FEET AGL A MAIN ROTOR BLADE DRAG STRUT FAILED DUE TO PROGRESSIVE FATIGUE THROUGH A THREADED PORTION OF THE STRUT. ONLY PARTIAL CONTROL OF THE HELICOPTER WAS POSSIBLE AFTER THE FAILURE. THE PILOT LOST CONTROL OF THE AIRCRAFT AT ONE POINT, BUT REGAINED CONTROL IN TIME TO PERFORM A HARD, SLIDING LANDING IN A FIELD. SUBSTANTIAL DAMAGE OCCURRED. THE ENTIRE SEQUENCE OF EVENTS TOOK PLACE IN 10-15 SECONDS. THE PLT HAD A PRIVATE CERT FOR FIXED WING AND A STUDENT CERT FOR ROTORCRAFT.

Flight

Event TypeAccident
Event Time17:08 EST
Nearest Airport0nm N
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHiller UH-12B
Tail NumberN48209
Aircraft CategoryHeli
DamageSubstantial
OperatorMark W Smith
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · 6V3355D · Reciprocating · 210
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 28 · Second Class

Conditions

ConditionsVMC
LightDusk
WindCalm
Visibility7 sm
CeilingNone
Temperature / Dew Point43 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data