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

June 29, 2001 · Piper PA-18-150 · N6881B

Palmer, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 29, 2001
Injury Outcomes
2 injuries (2 serious injuries)
Location
Palmer, AK
Aircraft
Piper PA-18-150
Tail Number
N6881B
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
ANC01LA078

The certificated private pilot, with one passenger aboard, was departing from an 800-feet long airstrip. A witness to the accident reported that just after takeoff the accident airplane's engine began to run rough and lose power. The witness said that it appeared that the pilot was trying to turn the airplane around in an attempt to return to the airstrip, and subsequently struck the surface of an open field next to the airstrip. An FAA airworthiness inspector from the local FSDO traveled to the accident scene and examined the airplane. He reported that the airplane came to rest upright with the left wing still attached to the fuselage, but the right wing was torn from the airplane during the impact. Both wing fuel tanks remained intact and were not breached, and the fuel selector valve was selected to the right fuel tank. The right fuel tank was empty, but the left tank was approximately 2/3 full. The FAA inspector interviewed a neighbor that lives close to the accident airstrip who responded to the accident site just after the accident. The neighbor stated that in the process of assisting rescue personnel, he moved the right wing away from the fuselage. In the process of moving the severed wing, he noted that the right wing fuel tank was empty, with no visible signs of postaccident spillage. While at the accident site, an Alaska State Trooper removed the right wing fuel cap and verified that the right wing fuel tank was empty.

NTSB Probable Cause

Fuel starvation due to the pilot's selection of an empty fuel tank during takeoff.

Full Narrative

On June 29, 2001, about 1350 Alaska daylight time, a wheel-equipped Piper PA-18-150 airplane, N6881B, sustained substantial damage during a forced landing at a private airstrip located about 2 miles north of Palmer, Alaska. The airplane was being operated as a visual flight rules (VFR) personal flight under Title 14, CFR Part 91, when the accident occurred. The certificated private pilot, and the one passenger aboard, sustained serious injuries. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated at the accident airstrip about 1349. A witness to the accident reported to the Alaska State Troopers that just after the accident airplane departed from the 800-feet long airstrip, the engine began to run rough and lose power. The witness said that it appeared that the pilot was trying to turn the airplane around in an attempt to return to the airstrip, and subsequently struck the surface of an open field next to the airstrip. The airplane sustained substantial damage to the wings, fuselage, and empennage. A Federal Aviation Administration (FAA) airworthiness inspector from the Anchorage Flight Standards District Office, traveled to the accident scene on June 29, and examined the airplane. He reported that the airplane came to rest upright with the left wing still attached to the fuselage, but the right wing was torn from the airplane during the impact. The FAA inspector noted that both wing fuel tanks remained intact and were not breached. He added that the left fuel tank appeared to be about 2/3 full, and the right tank was empty. The fuel selector valve was selected to the right fuel tank. The FAA inspector interviewed a neighbor that lives close to the accident airstrip who responded to the accident site, just after the accident. The neighbor stated that in conjunction with responding fire rescue personnel and Alaska State Troopers, he was one of first to reach the accident site. He reported that during the rescue attempts of the pilot and passenger, Fire Department personnel asked him to move the right wing away from the fuselage. In the process of moving the severed wing, he noted that the right wing fuel tank was empty, with no visible signs of postaccident spillage. While at the accident site an Alaska State Trooper removed the right wing fuel cap, and verified that the right wing fuel tank was empty. The pilot did not to submit a Pilot/Operator report (NTSB form 6120.1/2).

Flight

Event TypeAccident
Event Time13:50 AKDT
Nearest Airport0nm
Runway18
Runway Length800 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-18-150
Tail NumberN6881B
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-320 · Reciprocating · 150
Seats2

People & Injuries

Injury Summary2 injuries (2 serious injuries)
Fatal0
Serious2
Minor0
Uninjured0
Total2
Crew 1Age 45 · Third Class · Serious

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility50 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Weather SourceWIT

Appendix: Source Data