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Accidents · NTSB DFW05FA082 · Final report

Cessna 172F accident near Hot Springs, Arkansas, March 8, 2005

On March 8, 2005 at about 11:45 pm local time, a Cessna 172F, registered N8382U, was substantially damaged in an accident near Hot Springs, Arkansas (Hot Springs Memorial Airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A loss of engine power due to the pilot's failure to refuel resulting in fuel starvation. Contributing factors were the lack of suitable terrain for the forced landing, and a shoulder harness restraint system was not installed.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
March 8, 2005 · about 11:45 pm local time
Place
Hot Springs, Arkansas · Hot Springs Memorial Airport · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Cessna 172F · all 172Fs on the register
Registration
N8382U · no longer on the register · serial 17252282
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

After a cross-country flight, the single-engine airplane, piloted by a 40,000-hour pilot, impacted heavily wooded terrain about 1/4 miles short of the approach end of a municipal airport runway. Earlier in the day, the airplane had departed from a private airstrip with approximately 15 gallons of fuel on board. A person, who was in the vicinity of the accident site, witnessed an airplane flying toward the airport about 100 feet agl, and that the "engine was not running." He watched the airplane fly over a tree line and disappear, but he did not hear any kind of impact noise. No radio transmissions were heard from the accident airplane. There was a report by a friend of the pilot that the radio in the airplane was inoperative. Examination of the airframe and engine at the accident site did not reveal any mechanical pre-impact anomalies. The fuel tanks in both wings were not breached. The airplane was leveled, and approximately 1.5 gallons of clear automotive gasoline was drained from the airplane's fuel tanks. There did not appear to be an odor of fuel present when the investigation team first examined the wreckage. The wing-mounted, vented fuel caps were found secured. When the fuel level transmitter from each fuel tank was removed, the float arms for each moved smoothly, and were not restricted. Power was applied to the aircraft and each transmitter float moved through their full range of motion, and valid indications were observed on both fuel level gauges. The fuel selector handle was found in the "Both" position. The fuel screen was removed and found to be clean and clear of debris. According to manufacturer's documentation, the total fuel capacity of the airplane was 39 gallons (both tanks), of which, 3.0 gallons are not usable (1.5 gallons per tank). The total fuel found on-board at the accident site was approximately 1.5 gallons. Total flight time, from when the pilot last refueled the airplane with 15 gallons, could not be determined. Examination of the wrecakge showed that the basic shape and volume of the cabin was not altered during the crash. The pilot's seat was found intact with the exception of the forward inboard roller assembly, which remained attached to the seat rail within the cabin. The pilot's lap belt was found intact. Shoulder harnesses were not installed, and by FAA regulations, they were not required to be installed in the 1965 year model airplane. The pilot sustained head and chest injuries during the impact.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

Pilot

  • Certificate: airline transport pilot, flight instructor, commercial pilot, flight engineer
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: glider; instructor: helicopter; instructor: instrument airplane; instrument: airplane; instrument: helicopter; rotorcraft: glider; rotorcraft: helicopter
  • Flight time: 40,500 hours in all
  • Last flight review: May 5, 2004
  • Medical certificate: None (expired)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 159.3 hours
  • Last inspection: annual inspection, December 16, 2003
  • Maximum gross weight: 2,300 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Continental O-300-D (piston); 0 hours total

The flight

  • Departed from: NONE Sherrill AR at 10:30 pm
  • Destination: HOT
  • Flight plan: none
  • Runway 23, 6,595 ft by 150 ft

Weather at the time

  • Light: daylight
  • Wind: from 350° at 5 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 55°F (13°C), dew point 23°F (-5°C)
  • Altimeter: 29.97 inHg
  • Observation at 10:53 pm from HOT

Injuries

FatalSeriousMinorNone
Crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.