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

May 3, 2016 · Cessna 180 · N6479X

Naknek, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 3, 2016
Injury Outcomes
No injuries (1 uninjured)
Location
Naknek, AK
Aircraft
Cessna 180 (1961)
Tail Number
N6479X
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC16LA024

The commercial pilot stated that, during the landing rollout in the tailwheel-equipped airplane, the left wheel axle fractured and separated from the airplane with the wheel attached. The left landing gear leg then dug into the runway surface, the airplane made a sudden left turn, and the left wing and left horizontal stabilizer struck the runway. An examination of the fractured left axle revealed features consistent with a bending overstress fracture. High magnification optical examination of the fracture also revealed several small fatigue cracks within the crack origin area. Although several fatigue initiation sites were present along the fracture origin area, none of them were large enough to have led to the failure or to have significantly lowered the ultimate strength of the axle enough for a bending overstress failure to occur under normal loading conditions. Therefore, it is likely the landing gear axle failed as a result of bending overstress due to a hard landing.

NTSB Probable Cause

The overstress fracture and subsequent separation of the left main landing gear axle due to a hard landing, which resulted in the pilot’s inability to maintain directional control of the airplane.

Full Narrative

On May 3, 2016, about 1230 Alaska daylight time, a tailwheel-equipped Cessna 180 airplane, N6479X, sustained substantial damage following a separation of the left main wheel and axle from the landing gear strut during the landing rollout at the Naknek airport, Naknek, Alaska. The commercial pilot and sole occupant were not injured. The airplane was registered to Skol-Alaska, LLC and operated by the pilot under the provisions of 14 Code of Federal Regulations (CFR) Part 91 as a personal flight. Visual meteorological conditions prevailed at the time of the accident and a Federal Aviation Administration (FAA) visual flight rules (VFR) flight plan had been filed and activated. During an interview with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on May 3, 2016, the pilot stated that during the landing roll out, the left wheel axle fractured and separated from the airplane with the wheel attached. As the left landing gear leg dug into the runway surface, the airplane made a sudden left turn, and the left wing and left horizontal stabilizer struck the runway. The airplane sustained substantial damage to the left wing and left horizontal stabilizer. The fractured wheel axle was sent to the NTSB Materials Laboratory in Washington, D.C. for further examination. The fracture surface showed several areas of post-fracture damage. The undamaged portions of the fracture surface were optically, matte grey and highly textured consistent with a bending overstress fracture. Radial lines visible on the fracture indicated a wide area initiation at the outer diameter surface near the inboard end of the axle. High magnification optical examination of the fracture also revealed several small fatigue cracks within the crack origin area. A Materials Laboratory Factual Report is located in the public docket for this accident. The closest weather reporting facility is King Salmon Airport, King Salmon, Alaska, about 12 miles east of the accident site. At 1154, an aviation routine weather report (METAR) from the King Salmon Airport was reporting in part: wind from 080 degrees at 4 knots; sky condition, scattered at 2,700 feet AGL, broken at 5,000 feet AGL, broken at 7,500 feet AGL, broken at 20,000 AGL; visibility, 10 statute miles; temperature 52° F; dewpoint 36° F; barometric pressure 29.70 inHG.

Flight

Event TypeAccident
Event Time12:30 AKDT
Nearest AirportNAKNEK (0nm E)
Runway08
Runway Length1950 ft
Runway Width50 ft
Flight Plan FiledVFR
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 180
Tail NumberN6479X
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsCont Motor · O-470 SERIES · Reciprocating · 225
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 51 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind80° @ 4 kt
Visibility10 sm
CeilingBroken clouds 5000 ft
Temperature / Dew Point52 / 36 C
Altimeter29.70 inHg
Observation Time19:54
Weather SourceWFAC

Appendix: Source Data