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Accidents · NTSB ERA13LA407 · Final report

Piper PA-32R-300 accident near Guntersville, Alabama, September 8, 2013

On September 8, 2013 at about 9:56 pm local time, a Piper PA-32R-300, registered N8362C, was substantially damaged in an accident during enroute (cruise) near Guntersville, Alabama (Guntersville Municipal airport). It was a personal flight under general aviation rules (Part 91). 2 people had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The improper installation of the engine magneto by unknown maintenance personnel, which resulted in the magneto separating from the engine and a subsequent total loss of engine power. Contributing to the accident was the pilot's delay in proceeding directly to the nearest airport and his failure to prevent the automatic extension of the landing gear following the total loss of engine power, which resulted in a landing undershoot.

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

What the record shows

Date
September 8, 2013 · about 9:56 pm local time
Place
Guntersville, Alabama · Guntersville Municipal · map
Type
Accident
Injuries
2 people had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Piper PA-32R-300 · all PA-32R-300s on the register
Registration
N8362C · no longer on the register · serial 32R-7680099
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot reported that, about 3 to 4 nautical miles east-northeast of the nearest airport, the engine suddenly quit. GPS data indicate that the airplane was about 4,300 ft about that time. The pilot's attempts to restore power were unsuccessful. The pilot stated that he turned the airplane right toward the airport, and that, as he neared it, he announced his intention to land. While on approach, about 1/2 to 3/4 mile from the intended runway and with the flaps retracted, he allowed the airplane to slow to the point that the landing gear autoextend system caused the landing gear to extend, which he had not planned to do. He continued toward the runway, and the airplane touched down in water about 100 yards from the approach end of the intended runway. The pilot stated that, if the landing gear had not extended automatically, he believed that he could have reached land. Although the pilot reported that he turned toward the airport after the power loss, GPS data indicated that he actually flew west of the extended runway centerline and then maneuvered toward the airport. Based on data from the best glide chart in the Pilot's Operating Handbook, if the pilot had proceeded on a more direct course to the airport after the engine power loss or had not allowed the landing gear to automatically extend while on short final, the airplane likely would have been able to reach the intended runway. Postrecovery examination of the engine revealed that the single-drive dual magneto was separated from the accessory case because the lower attachment hardware had lost its clamping force and that the upper flange of the magneto had fractured due to fatigue cracking. Examination also revealed that the magneto was not installed in accordance with an engine manufacturer's service instruction—an incorrect gasket, washer, and clamp were used—all of which contributed to the separation of the magneto. Although compliance with service instructions is not mandatory for Part 91 operators, if the instructions had been complied with the last time the magneto was serviced, it is likely that it would not have separated despite the fact that the airplane had not undergone an annual inspection in over 2 1/2 years and, therefore, was unairworthy at the time of the accident.

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

What happened, in order

  1. Aircraft maintenance event during prior to flight
  2. Loss of engine power (total) during enroute (cruise) defining event
  3. Off-field or emergency landing during emergency descent
  4. Ditching during landing (flare/touchdown)

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Ignition system › Magneto/distributor › Incorrect service/maintenance
  • cause Personnel issues › Task performance › Maintenance › Installation › Maintenance personnel
  • factor Personnel issues › Action/decision › Action › Delayed action › Pilot
  • factor Aircraft › Aircraft systems › Landing gear system › Gear extension and retract sys › Incorrect use/operation
  • factor Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Descent/approach/glide path › Not attained/maintained
  • Personnel issues › Task performance › Inspection › Scheduled/routine inspection › Pilot

Pilot

  • Certificate: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 595 hours in all; 230 in this make and model
  • Last flight review: February 1, 2011
  • Medical certificate: Class 3
  • Seat: left
  • Injury: minor injuries

The aircraft

  • Airframe total time: 5,156 hours
  • Last inspection: annual inspection, February 18, 2011; 20 hours since
  • Maximum gross weight: 3,600 lb
  • Seats: 6
  • Landing gear: retractable
  • Engine: Lycoming TIO-540-K1A5D (piston); 0 hours total

The flight

  • Departed from: GAD Gadsden AL at 9:09 pm
  • Destination: GAD Gadsden AL
  • Flight plan: none
  • Runway 21, 3,368 ft by 95 ft

Weather at the time

  • Light: daylight
  • Wind: from 290° at 3 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 88°F (31°C), dew point 64°F (18°C)
  • Altimeter: 29.97 inHg
  • Observation at 9:55 pm from 8A0, 10 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

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

15 documents, released by the NTSB on May 12, 2015. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

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.