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 28, 1988 · Cessna 305A · N5166G

Gregory, MI

Overview

Report Status
Probable Cause
Event Type
Accident
Date
August 28, 1988
Injury Outcomes
No injuries (1 uninjured)
Location
Gregory, MI
Aircraft
Cessna 305A
Tail Number
N5166G
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI88DEC07

AS THE AIRCRAFT CLIMBED THROUGH AN ALTITUDE OF ABOUT 100 FEET ABOVE THE GROUND WITH A GLIDER IN TOW, THE ENGINE BEGAN TO RUN ROUGH, AND THEN FAILED COMPLETELY. THE PILOT EXECUTED A FORCED LANDING IN A GRASSY, ROLLING FIELD, STRIKING A FENCE AND SMALL TREE BEFORE IMPACTING THE GROUND.THE GLIDER RELEASED AND LANDED WITHOUT INCIDENT. POST-ACCIDENT EXAMINATION OF THE POWERPLANT, IT'S SYSTEMS AND ACCESSORIES REVEALED NO EVIDENCE OF PRE-IMPACT MECHANICAL MALFUNCTION/DIFFICULTY. THE ENGINE PERFORMED SATISFACTORILY DURING A SUBSEQUENT RUN-UP. INVESTIGATORS DRAINED 7.5 GALLONS OF 80/87 OCTANE AVIATION FUEL FROM EACH OF TWO FUEL TANKS; THE AIRCRAFT HAS A 'NO TAKEOFF' VALUE OF 6.75 GALLONS OR LESS. THIS VALUE WAS ESTABLISHED BECAUSE OF THE POSITIONING OF THE FUEL TANK OUTLETS AND THE RESULTANT POSSIBILITY OF FUEL FLOW INTERRUPTION IN VARIOUS FLIGHT ATTITUDES.

NTSB Probable Cause

FAILURE (AT FIRST PARTIAL, THEN TOTAL) OF THE AIRCRAFT'S POWERPLANT AT AN ALTITUDE OF ABOUT 100 FEET ABOVE THE GROUND DURING THE INITIAL CLIMBOUT WITH A GLIDER IN TOW; A FORCED LANDING ENSUED, DURING WHICH THE AIRCRAFT STRUCK A FENCE, A SMALL TREE, AND IMPACTED THE GROUND. THE GLIDER RELEASED AND LANDED WITHOUT INCIDENT.

Full Narrative

AS THE AIRCRAFT CLIMBED THROUGH AN ALTITUDE OF ABOUT 100 FEET ABOVE THE GROUND WITH A GLIDER IN TOW, THE ENGINE BEGAN TO RUN ROUGH, AND THEN FAILED COMPLETELY. THE PILOT EXECUTED A FORCED LANDING IN A GRASSY, ROLLING FIELD, STRIKING A FENCE AND SMALL TREE BEFORE IMPACTING THE GROUND.THE GLIDER RELEASED AND LANDED WITHOUT INCIDENT. POST-ACCIDENT EXAMINATION OF THE POWERPLANT, IT'S SYSTEMS AND ACCESSORIES REVEALED NO EVIDENCE OF PRE-IMPACT MECHANICAL MALFUNCTION/DIFFICULTY. THE ENGINE PERFORMED SATISFACTORILY DURING A SUBSEQUENT RUN-UP. INVESTIGATORS DRAINED 7.5 GALLONS OF 80/87 OCTANE AVIATION FUEL FROM EACH OF TWO FUEL TANKS; THE AIRCRAFT HAS A 'NO TAKEOFF' VALUE OF 6.75 GALLONS OR LESS. THIS VALUE WAS ESTABLISHED BECAUSE OF THE POSITIONING OF THE FUEL TANK OUTLETS AND THE RESULTANT POSSIBILITY OF FUEL FLOW INTERRUPTION IN VARIOUS FLIGHT ATTITUDES.

Flight

Event TypeAccident
Event Time13:00 EDT
Nearest AirportRICHMOND (0nm N)
Runway18
Runway Length2500 ft
Runway Width100 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 305A
Tail NumberN5166G
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · O-470-11B · Reciprocating · 190
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 68 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind290° @ 5 kt, gusting 10 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F / 52
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data