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

September 3, 2004 · Hardin Lancair 320 · N320MC

Chewelah, WA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 3, 2004
Injury Outcomes
2 injuries (2 minor injuries)
Location
Chewelah, WA
Aircraft
Hardin Lancair 320
Tail Number
N320MC
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
SEA04LA179

Both the pilot and pilot rated passenger reported that this was the first flight after the engine had been rebuilt. The flight was planned to circle the airport environment to "break-in" the engine. The engine had been operating at 75% power for the 30 minutes and readings for engine performance and fuel consumption were recorded. The pilots then decided to land at the airport they had been circling. Both pilots reported that just after the landing gear was lowered, they both smelled a heavy odor of fuel. About two minutes later, the engine began to sputter and subsequently quit. Unable to accomplish a successful landing at the airport, the pilot elected to perform a forced landing to an open field. The aircraft's left wingtip contacted the surface first and the aircraft cartwheeled before coming to rest. Post-accident inspection of the wreckage found a small amount of fuel in one wing, however, due to the severity of the break-up of the structure and compromise of the fuel system, the source of the fuel leak could not be determined.

NTSB Probable Cause

Fuel exhaustion as a result of a fuel leak from an undetermined location resulting in a loss of engine power during approach for landing and subsequent forced landing. Soft terrain was a factor.

Full Narrative

On September 3, 2004, at 1230 Pacific daylight time, an experimental Hardin Lancair 320, N320MC, registered to and flown by the pilot as a 14 CFR Part 91 personal flight, experienced a loss of engine power followed by an emergency off airport landing to an open field near Chewelah, Washington. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The aircraft was substantially damaged and the private pilot owner and commercial pilot rated passenger received minor injuries. The flight had been operating in the local area for about 30 minutes prior to the accident. During a telephone interview, both the pilot and pilot rated passenger reported that this was the first flight after the engine had been rebuilt. The flight was planned to circle the airport environment to "break-in" the engine. The engine had been operating at 75 % power for the 30 minutes and readings for engine performance and fuel consumption were recorded. The pilots then decided to land at the airport they had been circling. Both pilots reported that just after the landing gear was lowered, they both smelled a heavy odor of fuel. About two minutes later, the engine began to sputter and subsequently quit. Unable to accomplish a successful landing at the airport, the pilot elected to perform a forced landing to an open field. The aircraft's left wingtip contacted the surface first and the aircraft cartwheeled before coming to rest. Post-accident inspection of the wreckage by a Federal Aviation Administration Inspector from the Spokane, Washington, Flight Standards District Office, reported that the right side wing tank contained a quart of fuel and there was some fuel present in the main strainer. No "header tank" had been installed nor were there check valves in the vent system. During the crash sequence, the propeller shaft broke inside the crankcase and the crankshaft could not be rotated. Due to the severity of the break-up of the structure and compromise of the fuel system, the source of the fuel leak could not be determined. The pilot reported that approximately 36 gallons of fuel was on board at the time of departure.

Flight

Event TypeAccident
Event Time12:30 PDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHardin Lancair 320
Tail NumberN320MC
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-360-B1A · Reciprocating · 180
Seats2

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 71 · Third Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind140° @ 4 kt
Visibility10 sm
CeilingOvercast 6000 ft
Temperature / Dew Point61 F / 43 C
Altimeter30.04 inHg
Observation Time19:53
Weather SourceWFAC

Appendix: Source Data