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

January 27, 1989 · Piper PA-23-160 · N4391P

Carson City, NV

Overview

Report Status
Probable Cause
Event Type
Accident
Date
January 27, 1989
Injury Outcomes
1 injury (1 fatality)
Location
Carson City, NV
Aircraft
Piper PA-23-160
Tail Number
N4391P
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
SEA89FA040

WHILE ON CROSSWIND LEG AFTER T/O, THE PILOT ANNOUNCED HE HAD LOST AN ENGINE AND WAS RETURNING TO LAND. DURING A LEFT TURN BACK TOWARD THE ARPT, THE ACFT ROLLED INVERTED TO THE LEFT AND DESCENDED IN A NOSE DOWN ATTITUDE UNTIL IMPACT. EXAM REVEALED AN EXTRA NEEDLE VALVE LOOSE IN THE LEFT ENG CARBURETOR FLOAT BOWL. ANOTHER NEEDLE VALVE AND SEAT ASSEMBLY WAS CORRECTLY INSTALLED IN THE CARBURETOR. NUMEROUS SMOOTH BRIGHT SPOTS OF WEAR WERE FOUND ON THE BOTTOM SURFACE OF THE GRAINY TEXTURED INTERIOR OF THE FLOAT BOWL. THE AREA AROUND THE FUEL MIXTURE METERING ASSEMBLY PORT WAS POLISHED AND THE NEEDLE VALVE COULD BE INSERTED IN THE PORT. MAINTENANCE RECORDS REVEALED NEW ENGINES HAD BEEN INSTALLED ON 10/30/79. ALTHOUGH RECORDS AND WITNESSES INDICATED POWER PROBLEMS WITH THE LEFT ENGINE, NO RECORDS INDICATED THE CARBURETOR FLOAT BOWL HAD EVER BEEN REMOVED AFTER THE ENGINE HAD INITIALLY BEEN INSTALLED ON THE AIRCRAFT.

NTSB Probable Cause

LOSS OF POWER ON THE LEFT ENGINE DUE TO A FOREIGN OBJECT WHICH OBSTRUCTED THE FUEL FLOW, AND THE PILOT'S FAILURE TO MAINTAIN AIRSPEED ABOVE VMC DURING HIS ATTEMPTED RETURN TO THE AIRFIELD. CONTRIBUTING TO THE ACCIDENT WAS THE LACK OF RECENT FLIGHT TIME BY THE PILOT.

Full Narrative

WHILE ON CROSSWIND LEG AFTER T/O, THE PILOT ANNOUNCED HE HAD LOST AN ENGINE AND WAS RETURNING TO LAND. DURING A LEFT TURN BACK TOWARD THE ARPT, THE ACFT ROLLED INVERTED TO THE LEFT AND DESCENDED IN A NOSE DOWN ATTITUDE UNTIL IMPACT. EXAM REVEALED AN EXTRA NEEDLE VALVE LOOSE IN THE LEFT ENG CARBURETOR FLOAT BOWL. ANOTHER NEEDLE VALVE AND SEAT ASSEMBLY WAS CORRECTLY INSTALLED IN THE CARBURETOR. NUMEROUS SMOOTH BRIGHT SPOTS OF WEAR WERE FOUND ON THE BOTTOM SURFACE OF THE GRAINY TEXTURED INTERIOR OF THE FLOAT BOWL. THE AREA AROUND THE FUEL MIXTURE METERING ASSEMBLY PORT WAS POLISHED AND THE NEEDLE VALVE COULD BE INSERTED IN THE PORT. MAINTENANCE RECORDS REVEALED NEW ENGINES HAD BEEN INSTALLED ON 10/30/79. ALTHOUGH RECORDS AND WITNESSES INDICATED POWER PROBLEMS WITH THE LEFT ENGINE, NO RECORDS INDICATED THE CARBURETOR FLOAT BOWL HAD EVER BEEN REMOVED AFTER THE ENGINE HAD INITIALLY BEEN INSTALLED ON THE AIRCRAFT.

Flight

Event TypeAccident
Event Time12:52 PST
Nearest AirportCarson City (1nm SW)
Runway27
Runway Length5900 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-23-160
Tail NumberN4391P
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsLycoming · O-360-A1D · Reciprocating · 180
Seats4

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 65 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility20 sm
CeilingNone
Temperature / Dew Point37 C / 19 C
Altimeter30.00 inHg
Observation Time20:59
Weather SourceWFAC

Appendix: Source Data