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

July 25, 1992 · Piper PA-38-112 · N9240T

Carrollton, TX

Overview

Report Status
Probable Cause
Event Type
Accident
Date
July 25, 1992
Injury Outcomes
1 injury (1 serious injury)
Location
Carrollton, TX
Aircraft
Piper PA-38-112
Tail Number
N9240T
Operator
Stramel Aviation
Injuries
Serious
Aircraft Damage
Destroyed
NTSB Number
FTW92LA188

THE PILOT WAS DESCENDING THE AIRPLANE INTO THE CONTROL ZONE AND HAD RECEIVED CLEARANCE TO ENTER A RIGHT BASE FOR RUNWAY 15 WHEN THE ENGINE QUIT AFTER HE APPLIED CARBURETOR HEAT. THE PILOT MADE A 180 DEGREE TURN AND DESCENDED OVER ONE OPEN GRASS FIELD AS HE ATTEMPTED TO GLIDE TO A DIRT FIELD. A FENCE AND A RAILROAD TRACK LAY BETWEEN THE FIELDS. THE AIRPLANE STRUCK THE FENCE, ROTATED APPROXIMATELY 180 DEGREES, AND DESCENDED OUT OF CONTROL TO IMPACT THE TERRAIN NEAR THE RAILROAD TRACKS. THE INVESTIGATION REVEALED THE MAIN VALVE FOR THE CARBURETOR HEAT BOX HAD FAILED AND WAS SUCKED INTO THE CARBURETOR INLET, BLOCKING AIR FLOW, AND RENDERED THE CARBURETOR INOPERATIVE. FURTHER INVESTIGATION REVEALED THAT PORTIONS OF THE VALVE ASSEMBLY HAD BEEN FAILING FOR AN UNSPECIFIED TIME PRIOR TO THE ACCIDENT AND ITS' RETAINING SCREWS HAD NOT BEEN SECURED PROPERLY.

NTSB Probable Cause

THE PILOT'S SELECTION OF UNSUITABLE TERRAIN. FACTORS WERE THE FAILED CARBURETOR DE-ICE SYSTEM VALVE RESULTING IN AN INOPERATIVE CARBURETOR AND THE INADEQUATE ANNUAL INSPECTION BY COMPANY MAINTENANCE PERSONNEL.

Full Narrative

THE PILOT WAS DESCENDING THE AIRPLANE INTO THE CONTROL ZONE AND HAD RECEIVED CLEARANCE TO ENTER A RIGHT BASE FOR RUNWAY 15 WHEN THE ENGINE QUIT AFTER HE APPLIED CARBURETOR HEAT. THE PILOT MADE A 180 DEGREE TURN AND DESCENDED OVER ONE OPEN GRASS FIELD AS HE ATTEMPTED TO GLIDE TO A DIRT FIELD. A FENCE AND A RAILROAD TRACK LAY BETWEEN THE FIELDS. THE AIRPLANE STRUCK THE FENCE, ROTATED APPROXIMATELY 180 DEGREES, AND DESCENDED OUT OF CONTROL TO IMPACT THE TERRAIN NEAR THE RAILROAD TRACKS. THE INVESTIGATION REVEALED THE MAIN VALVE FOR THE CARBURETOR HEAT BOX HAD FAILED AND WAS SUCKED INTO THE CARBURETOR INLET, BLOCKING AIR FLOW, AND RENDERED THE CARBURETOR INOPERATIVE. FURTHER INVESTIGATION REVEALED THAT PORTIONS OF THE VALVE ASSEMBLY HAD BEEN FAILING FOR AN UNSPECIFIED TIME PRIOR TO THE ACCIDENT AND ITS' RETAINING SCREWS HAD NOT BEEN SECURED PROPERLY.

Flight

Event TypeAccident
Event Time14:00 CDT
Nearest Airport0nm N
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-38-112
Tail NumberN9240T
Aircraft CategoryAir
DamageDestroyed
OperatorStramel Aviation
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-235-L2C · Reciprocating · 112
Seats2

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 31 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind250° @ 5 kt
Visibility20 sm
CeilingNone
Temperature / Dew Point64 F
Altimeter30.00 inHg
Observation Time20:37
Weather SourceWFAC

Appendix: Source Data