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

September 5, 2013 · Piper J3L-65 · N38262

Nondalton, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 5, 2013
Injury Outcomes
No injuries (2 uninjured)
Location
Nondalton, AK
Aircraft
Piper J3L-65 (1941)
Tail Number
N38262
Operator
Patrick Paul Williams
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC13LA102

The pilot reported that, while the airplane was in level cruise flight, he heard a loud "pop," followed by a total loss of engine power. He subsequently made a forced landing to an open, tundra-covered site. During the forced landing, the airplane nosed over, which resulted in substantial damage to the wings, fuselage, and empennage. A postaccident examination of the engine revealed a fractured exhaust valve stem on the No. 4 cylinder, which subsequently pulverized the electrodes on both sparks plugs and severely damaged the piston.

NTSB Probable Cause

The fracture and subsequent failure of the No. 4 cylinder exhaust valve during cruise flight, which resulted in a total loss of engine power.

Full Narrative

On September 5, 2013, about 1300 Alaska daylight time, a wheel-equipped Piper J3L-65 airplane, N38262, sustained substantial damage during a forced landing, following a loss of engine power, near Nondalton, Alaska. The airplane was being operated by the pilot as a visual flight rules (VFR) personal cross-country flight under the provisions of Title 14, CFR Part 91, when the accident occurred. The private pilot and one passenger were not injured. Visual meteorological conditions prevailed, and no flight plan had been filed. The flight departed about 1150, from the Keyes Point Airstrip, a private remote fly-in community about 18 miles southwest of Port Alsworth, Alaska. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on September 11, the pilot stated that the purpose of the flight was to scout for moose to hunt. He said that while in level cruise flight, he heard a loud "pop," which was followed by a total loss of engine power, and he made a forced landing to an open, tundra-covered site. During the forced landing, the airplane nosed over, sustaining substantial damage to the wings, fuselage, and empennage. When the flight failed to arrive back at the Keyes Point Airstrip on the evening of September 5, a concerned family member of the passenger reported the airplane overdue. The flight was officially reported overdue to the Federal Aviation Administration (FAA) at 1238, on September 6. Search personnel from the Civil Air Patrol, Alaska State Troopers, Alaska Air National Guard, along with several volunteers, were dispatched to conduct an extensive search effort. No emergency transmitter locator (ELT) signal was received by search personnel. The accident airplane was equipped with an older generation 121.5 MHz ELT instead of a digital, 406 MHz ELT that instantly transmits a distress signal to search and rescue satellites, thereby alerting rescue personnel within minutes of the location of the crash. As of February 1, 2009, analog, 121.5 MHz ELT's stopped being monitored by search and rescue satellites, and the installation of the 406 MHz has been voluntary. Both types of ELT's can be turned on manually, or automatically, by impact forces. On September 7, about 2151, the airplane's overturned wreckage was located by an Alaska State Trooper search airplane about 10 miles north-northwest of Nondalton, but the two occupants were not found at the accident site. On September 8, about 1200, the two uninjured occupants were located about 3 miles northwest of Nondalton. The airplane was equipped with a Continental Motors C-85 series engine. The airplane owner's insurance company sold the airplane wreckage on an "as is, where is" basis. According to the new owner, a postaccident inspection of the airplane's engine revealed a fractured exhaust valve stem on the number four cylinder, which subsequently pulverized the electrodes on both sparks plugs, and severely damaged the piston. Once the number 4 cylinder was replaced, the engine was started, and it continued to operate without further mechanical anomalies. The fractured valve stem was not made available to the NTSB for examination. After repeated requests, the accident pilot did not submit the required 6120.1 Pilot/Operator Aircraft Accident/Incident Report.

Flight

Event TypeAccident
Event Time13:00 AKDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper J3L-65
Tail NumberN38262
Aircraft CategoryAir
DamageSubstantial
OperatorPatrick Paul Williams
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental Motors · C-85 Series · Reciprocating · 85
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 53 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point55 / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data