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

January 5, 2006 · Piper PA-32-300 · N190PH

Worthington, MN

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 5, 2006
Injury Outcomes
No injuries (1 uninjured)
Location
Worthington, MN
Aircraft
Piper PA-32-300
Tail Number
N190PH
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI06LA061

The airplane veered off the runway after touchdown following a precision instrument approach and landing on runway 29. Night visual meteorological conditions prevailed at the time of the accident. The pilot stated that the airport's automated weather observing system (AWOS) reported calm winds, but he felt that this was inaccurate so he checked reports from surrounding AWOSs, which reported winds from the northwest at 8-11 knots. The pilot stated that upon touchdown, the airplane moved "quickly" to the left and departed off the side of the runway and into snow, which folded the nose wheel landing gear. The maximum demonstrated cross wind for the airplane is 17 knots. Inspection of the airport's AWOS following the accident revealed that the AWOS was covered with ice, which inhibited operation of the wind speed and direction sensors. The Federal Aviation Administration had no record of a Notices to Airman being issued on the day of the accident pertaining to the airport AWOS.

NTSB Probable Cause

The missed approach not performed by the pilot and the directional control not maintained by the pilot during landing. Contributing factors were the crosswind, wind information not available due to inoperative meteorological equipment, and a Notices to Airman not issued by airport personnel indicating that the meteorological equipment was inoperative.

Full Narrative

On January 4, 2006, at 1930 central standard time, a Piper PA-32-300, N190PH, piloted by a private pilot, impacted terrain during landing when it veered off runway 29 at Worthington Municipal (OTG), Worthington, Minnesota. Night instrument meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 business flight was operating on an instrument rules flight plan. The pilot was uninjured. The flight originated from Scott City Municipal, Scott City, Kansas, at 1615 and was en route to OTG. The pilot stated that he departed from Scott City, Kansas, and was returning to OTG. The OTG Automated Weather Observing System (AWOS) reported a ceiling of 600 feet above ground level, 10 statute mile visibility, and calm winds. He stated that he "did not feel that this was accurate" so he checked Joe Foss Field (FSD), Sioux Falls, South Dakota, and Sheldon Municipal Airport (SHL), Sheldon, Iowa, AWOS reports. The pilot encountered instrument meteorological conditions 5-8 miles southwest of the airport and performed an instrument landing system approach to runway 29. He had the runway in sight at an altitude approximately 2,300 feet mean sea level. While on final approach, he "recognized" that there was a "significant crosswind". He applied right aileron and full left rudder but was unable to keep the airplane to the right side of the runway and touched down left of center. The airplane moved "quickly" to the left and departed off the side of the runway and into snow, which folded the nose wheel landing gear. OTG is served by runway 11-29 (5,506 feet by 100 feet, grooved asphalt) and runway 17-35 (4,201 feet by 100 feet, grooved asphalt) with a lighted wind sock located east of approach end of runway 35. OTG was equipped with a Qualimetics model 200 AWOS installed in the early 1990s. Later AWOS models were equipped with error checking correlating wind speed and direction, and may also incorporate a heater. The OTG AWOS recorded wind speed of 0 degrees and direction of 000 for the entire accident day. The Windom Municipal Airport, Windom, Minnesota, AWOS, located about 25.6 NM northeast of OTG, recorded at 1855 and 1955, wind 300 degrees at 6 knots. The Jackson Municipal Airport, Jackson, Minnesota, AWOS, located about 25.7 NM east of OTG, recorded at 1855 and 1955, wind 320 degrees at 7 knots and wind 310 degrees at 11 knots. The SHL AWOS, located about 29 nautical miles south of OTG, recorded at 1855 and 1955, wind 310 degrees at 10 knots and wind 330 at 11 knots, respectively. The FSD AWOS, located about 50.7 nautical miles east of OTG, recorded at 1856 and 1956, wind 320 degrees at 8 knots. Federal Aviation Administration (FAA) inspection of the OTG AWOS following the accident revealed that the AWOS was covered with ice, which inhibited operation of the wind speed and direction sensors. The FAA had no record of any Notices to Airman pertaining to the OTG AWOS on the day of the accident. The maximum demonstrated crosswind component for the Piper PA-32-300 is placarded as 17 knots.

Flight

Event TypeAccident
Event Time19:30 CST
Nearest AirportWorthington Municipal (0nm)
Runway29
Runway Length5506 ft
Runway Width100 ft
Flight Plan FiledIFR
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-32-300
Tail NumberN190PH
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsTextron Lycoming · IO-540 · Reciprocating · 300
Seats6

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 48 · Third Class · None

Conditions

ConditionsIMC
LightNight
WindCalm
Visibility9 sm
CeilingBroken clouds 800 ft
Temperature / Dew Point28 C / 25 C
Altimeter30.10 inHg
Observation Time00:55
Weather SourceWFAC

Appendix: Source Data