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 8, 2023 · Piper PA-24-260 · N503JA

Fullerton, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 8, 2023
Injury Outcomes
1 injury (1 minor injury)
Location
Fullerton, CA
Aircraft
Piper PA-24-260 (1965)
Tail Number
N503JA
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
WPR23LA317

Shortly after takeoff the airplane began to shake violently with the control yoke moving rapidly forward and aft from stop to stop. The pilot was able to perform an on-airport emergency landing after shutting down the engine, but sustained hand injuries due to the extreme control forces and oscillations. The airplane sustained substantial damage to the stabilator structure in a manner consistent with it exhibiting aerodynamic flutter. Postaccident examination revealed that the stabilator tab actuator was disconnected from the control tab, and the bolt, nut, and washer that connected them were missing. The disconnection of the actuator allowed the tab surface to uncouple, which resulted in flutter and structural damage to the stabilator. Circumferential scoring around the bolt hole within the tabs indicated that the bolt was likely loose for an undetermined period before failure. The nut had likely not been replaced since the airplane was manufactured almost 60 years before the accident, so its locking properties would have been significantly diminished.

NTSB Probable Cause

The separation of the stabilator actuator from the stabilator tab, which resulted in pitch control surface flutter and structural damage.

Full Narrative

On August 8, 2023, about 1500 Pacific daylight time, a Piper PA-24-260, N503JA, was substantially damaged when it was involved in an accident near Fullerton, California. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot stated that, shortly after takeoff, the airplane began to shake violently with the control yoke moving rapidly forward and aft from stop to stop. The vibrations were so extreme that he assumed the engine had suffered a catastrophic failure, such as a detached engine cylinder. He shut down the engine and turned the airplane back to the airport for landing. The pilot stated he was able to land, but sustained hand injuries due to the extreme control forces and oscillations. The airplane sustained substantial damage to the stabilator structure and postaccident examination revealed that the stabilator tab actuator was disconnected from the control tab, and the bolt, nut, and washer that connected them were missing (figure 1). Figure 1 - Stabilator tab disconnected from the actuator. The tabs sustained extensive scratch and peening damage to both their inner and forward surfaces consistent with high frequency oscillations. The paint around the end of the tab actuator arm had chipped away, revealing similar peening damage to its steel surface. Neither the bolt nor the nut that connected the tabs to the actuator were located, and there was circumferential scoring to the tabs around the bolt hole bore. Neither bolt hole appeared to be elongated. Likewise, the bushing within the actuator did not appear to be out of round. According to the airplane’s illustrated parts catalog, the actuator retaining nut was supposed to be a self-locking type, with no provisions for a cotter pin. The mechanic who had performed an annual inspection 5.5 flight hours before the accident stated that he did not remove or replace either the bolt or the nut, and that he performed a functional check of the pitch trim system with no anomalies noted. Examination of the maintenance logbooks did not reveal any evidence that the nut had been replaced since the airplane was manufactured in 1965.

Flight

Event TypeAccident
Event Time15:00 PDT
Nearest AirportFullerton Muni (0nm E)
Runway24
Runway Length3121 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-24-260
Tail NumberN503JA
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540-D4A5 · Reciprocating · 260
Seats4

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 41 · Second Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind190° @ 7 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point63 F
Altimeter29.96 inHg
Observation Time15:53
Weather SourceWFAC

Appendix: Source Data