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

December 30, 2023 · Bellanca 17-30A · N678MJ

Washington, MO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 30, 2023
Injury Outcomes
1 injury (1 serious injury)
Location
Washington, MO
Aircraft
Bellanca 17-30A (1979)
Tail Number
N678MJ
Operator
Piasa
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
CEN24LA077

The pilot reported that the engine start, run-up, and takeoff were without incident. However, shortly after takeoff, the engine completely lost power. In his efforts to avoid trees in the glide path, the airplane inadvertently entered an aerodynamic stall and spin. He was able to recover from the spin but unable to arrest the descent before impacting an open field. The airplane came to rest upright with damage to the fuselage, left wing, and empennage. The pilot reported that about three weeks before the accident a similar loss of engine power event occurred after takeoff. In that instance, he was able to land in the level grass area short of the runway without any damage to the airplane. A mechanic examined the airplane and noted that the diffuser was missing from the muffler. A postrecovery examination did not reveal any anomalies with the engine assembly. However, testing and disassembly of the fuel pump identified a piece of debris within the vapor ejector cavity. Further analysis determined that the material was a rubber fragment from a fuel line. The examination did not observe any indication that diffusers were installed in either the left or right mufflers. The fuel line fragment present in the pump likely traveled into a position in which it blocked the vapor return. This blockage then routed any fuel vapor into the fuel inlet line to the engine and resulted in an interruption of fuel flow due to vapor lock. The airplane maintenance records did not reveal a record of any recent work on the fuel pump or fuel lines. The investigation was unable to determine how the rubber fuel line fragment was introduced into the fuel system.

NTSB Probable Cause

Fuel starvation and a total loss of engine power due to an obstructed fuel vapor return path. Contributing to the accident was the pilot’s inadvertent aerodynamic stall/spin, which likely increased the severity of the ground impact.

Full Narrative

On December 30, 2023, about 1415 central standard time, a Bellanca 17-30A airplane, N678MJ, was substantially damaged when it was involved in an accident near Washington, Missouri. The pilot sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that the engine start and run-up were normal. Similarly, the takeoff was normal, and the pilot reduced to climb power shortly after lifting off. About 400 ft above ground level, as he began a left turn to crosswind, the pilot realized the engine had lost power. As the pilot tightened the turn to avoid trees, the airplane inadvertently entered an aerodynamic stall and a spin. He was able to recover from the spin but unable to arrest the descent before impacting an open field. The airplane came to rest upright with damage to the fuselage, left wing, and empennage. The pilot reported that about three weeks before the accident a similar loss of engine power event occurred after takeoff. In that instance, he was able to land in the level grass area short of the runway without any damage to the airplane. A mechanic examined the airplane and noted that the diffuser (flame cone) was missing from the muffler. A postrecovery examination did not reveal any anomalies with the core engine assembly. Testing of the throttle and control assembly similarly was unremarkable. However, testing of the fuel pump revealed flow rates that did not meet the manufacturer’s specification. Partial disassembly of the unit identified a piece of debris within the vapor ejector cavity. Analysis of the debris by the NTSB Materials Laboratory determined that the material was similar to nitrile rubber commonly used in the construction of fuel lines. The postrecovery examination noted that the engine was equipped with two mufflers, both of which appeared to be intact and securely installed. Neither muffler was equipped with a diffuser, nor were there brackets normally used to support a diffuser within a muffler housing. There was also no evidence of spot welds commonly used to secure the diffuser supports on the muffler housing. The airplane’s maintenance records did not reveal a record of any recent work on the fuel pump or fuel lines.

Flight

Event TypeAccident
Event Time14:15 CST
Nearest AirportWashington Regional (0nm NNW)
Runway33
Runway Length5002 ft
Runway Width75 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBellanca 17-30A
Tail NumberN678MJ
Aircraft CategoryAir
DamageSubstantial
OperatorPiasa
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-550-F · Reciprocating · 300
Seats4

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 79 · Third Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind220° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point48 F / 34 F
Altimeter29.90 inHg
Observation Time14:54
Weather SourceWFAC

Appendix: Source Data