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 19, 2009 · Bellanca 17-31ATC · N14797

Roosevelt, UT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 19, 2009
Injury Outcomes
No injuries (1 uninjured)
Location
Roosevelt, UT
Aircraft
Bellanca 17-31ATC
Tail Number
N14797
Operator
Gregory G Page Dds
Injuries
None
Aircraft Damage
Substantial
NTSB Number
WPR09LA297

During the landing roll, the bolt holding the left main landing gear hydraulic extension and retraction actuator to the gear support structure failed, which allowed the left main landing gear leg to retract. Further inspection determined that over time the bolt hole on the support structure had elongated to about twice its original size. This condition would have been very difficult to detect on a preflight inspection; however, it should have been detected during previous annual inspections.

NTSB Probable Cause

The retraction of the left main landing gear due to the failure of the extension and retraction actuator arm attach bolt. Contributing to the accident was the failure of maintenance personnel to discover the extensive elongation of the actuator attach fitting bolt hole during past annual inspections.

Full Narrative

On June 18, 2009, about 2115 mountain daylight time, a Bellanca 17-31ATC, N14797, experienced a collapse of the left main landing gear during the landing roll at Roosevelt Municipal Airport, Roosevelt, Utah. The commercial pilot, who was the sole occupant, was not injured, but the airplane, which is owned and operated by the pilot, sustained substantial damage. The local 14 Code of Federal Regulations Part 91 personal pleasure flight, which departed Roosevelt Municipal Airport about 15 minutes earlier, was being operated in visual meteorological conditions. No flight plan had been filed. According to the pilot, this was a brief local flight to check the operation of the turbocharger, which had just come out of maintenance. After the flight around the local area, the pilot returned to the airport for a full stop landing. Reportedly, he made a normal flare and touchdown, and the first 1,000 feet of the landing roll was uneventful. The left main landing gear green DOWN light went out, and the red landing gear TRANSITION warning light came on, and the left main gear retracted. After the gear retracted, the airplane exited the left side of the runway, and collided with rough terrain. This sequence resulted in damage to the left wing, and bending of the fuselage structure. A post- accident inspection of the left landing gear extension and retraction system by a Federal Aviation Administration (FAA) Airworthiness Inspector determined that the bolt connecting the hydraulic gear actuator rod to the gear leg support had failed. Further inspection revealed that over a period of time the bolt hole in the gear leg support had worn to a point where it had become elongated to about twice its original size (see photo in the public docket for this accident). According to the FAA inspector, the elongation of the hole, and the looseness it would have created, should have been detected during at least the last couple of annual inspections.

Flight

Event TypeAccident
Event Time21:15 MDT
Nearest AirportRoosevelt Municipal (0nm)
Runway07
Runway Length6500 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBellanca 17-31ATC
Tail NumberN14797
Aircraft CategoryAir
DamageSubstantial
OperatorGregory G Page Dds
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · TIO-540 SER · Reciprocating · 310
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 55 · Third Class · None

Conditions

ConditionsVMC
LightDusk
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data