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

August 19, 1993 · Piper PA-28-180 · N9533J

Showlow, AZ

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 19, 1993
Injury Outcomes
No injuries (2 uninjured)
Location
Showlow, AZ
Aircraft
Piper PA-28-180
Tail Number
N9533J
Operator
Dale Cornett
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX93LA330

THE ENGINE LOST TOTAL POWER WHILE AT CRUISE FLIGHT. THE FLIGHT INSTRUCTOR WAS UNSUCCESSFUL IN HIS ATTEMPT TO RESTART THE ENGINE. THE AIRPLANE'S NOSE WHEEL COLLAPSED AFTER IT COLLIDED WITH A BUSH DURING THE LANDING ROLL IN THE HIGH DESERT TERRAIN. INSPECTION OF THE ENGINE REVEALED THAT THE BALLJOINT ASSEMBLY THAT ATTACHES THE MIXTURE CONTROL CABLE TO THE MIXTURE ARM ON THE CARBURETOR HAD SEPARATED. AN ANNUAL INSPECTION WAS CONDUCTED 10 FLIGHT HOURS PRIOR TO THE ACCIDENT.

NTSB Probable Cause

A total loss of engine power due to a separation of the mixture control balljoint assembly at the carburetor mixture arm and subsequent forced landing.

Full Narrative

On August 19, 1993, about 0630 hours mountain standard time, a Piper PA-28-180, N9533J, crashed during a forced landing about 24 miles northeast of Showlow, Arizona. The airplane was being operated as a visual flight rules (VFR) cross country instructional flight to Tucumcari, New Mexico, when the accident occurred. The airplane, co-owned and operated by the pilot, received substantial damage. The certificated commercial pilot/certified flight instructor (first pilot) and a non-certified student pilot (second pilot) were not injured. Visual meteorological conditions prevailed. A VFR flight plan was filed. The flight originated at Payson, Arizona, at 0510 hours. The first pilot reported that while in cruise flight at 11,500 feet mean sea level the engine suddenly began to run rough and then quit. The pilot adjusted the mixture control in an attempt to restart the engine; however, movement of the control did not produce any results. The second pilot, who was initially flying the airplane, selected a clear area of high desert terrain for a forced landing. Just before touchdown, the first pilot took the controls and completed the landing. During the landing roll, the airplane collided with large bushes and high vegetation and received damage to the nose, landing gear, and wings. Mr. John Eller, Airworthiness Inspector, Federal Aviation Administration, Scottsdale Flight Standards District Office, examined the mixture control cable. He reported that the balljoint assembly that attaches the control cable to the mixture control arm on the carburetor had separated. The assembly, part number 31747.00, was not recovered. The airplane and engine had accumulated a total time in service of 2,545.60 flight hours. Examination of the maintenance records revealed that the most recent annual inspection was accomplished on August 6, 1993, 10 flight hours before the accident. The engine had accrued 420.5 hours of operation since being overhauled.

Flight

Event TypeAccident
Event Time06:30 MST
Nearest Airport0nm
Runway0
Flight Plan FiledVFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-180
Tail NumberN9533J
Aircraft CategoryAir
DamageSubstantial
OperatorDale Cornett
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-A3A · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 63 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind240°
Visibility30 sm
CeilingNone
Temperature / Dew Point70 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data