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 21, 1995 · Cessna 310B · N661R

Monticello, NY

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 21, 1995
Injury Outcomes
No injuries (2 uninjured)
Location
Monticello, NY
Aircraft
Cessna 310B
Tail Number
N661R
Injuries
None
Aircraft Damage
Substantial
NTSB Number
NYC95LA201

During the landing roll, the right main gear collapsed, and the airplane veered off the runway into an embankment. Postaccident investigation revealed that the right main landing gear failed through the weld that held the socket-strut, strut-tube, and plate-reinforcement together. Metallurgical examination of the fracture revealed that the failure was due to fatigue.

NTSB Probable Cause

fatigue failure of the right main landing gear during the landing, which resulted in a gear collapse, loss of directional control, and subsequent collision with an embankment.

Full Narrative

On August 21, 1995, about 1550 eastern daylight time, a Cessna 310B, airplane, N661R, was substantially damaged when it collided with terrain during the landing, at the Monticello Airport, Monticello, New York. The private pilot and passenger were not injured. Visual meteorological conditions prevailed for the personal flight that departed from Sussex, New Jersey. There was no flight plan for the flight conducted under 14 CFR Part 91. In the NTSB form 6120.1/2, the pilot stated: ". . .At touchdown on runway 01, the right wheel fell off. . . .Upon leaving blacktop, airplane spun around and stopped beside runway. . . .Upon examination of wheel and strut, a weld broke causing wheel to fall off. . . ." The pilot reported that the airplane came to rest in a large embankment. Additionally, the right main landing gear assembly was examined by the National Transportation Safety Board Metallurgist Lab, Washington, District of Columbia. The metallurgist's factual report stated: "Examination of the fracture faces on the received pieces revealed features typical of fatigue cracking adjacent to the inner surface of the weld. The fatigue cracking initiated from multiple origins located at the inboard and outboard sides of the strut assembly. . . .Subsequent examination of the fracture faces revealed no evidence of corrosion pitting either at the fatigue crack origins or in any other areas of the fracture."

Flight

Event TypeAccident
Event Time15:50 EDT
Nearest AirportMonticello (0nm)
Runway1
Runway Length2845 ft
Runway Width31 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 310B
Tail NumberN661R
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsLycoming · IO-540-A1A5 · Reciprocating · 290
Seats6

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 40 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility15 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data