The U.S. aircraft register, updated daily · Carbon Free Flight by 2050
Accidents · NTSB ERA13FA055 · Final report

Piper PA-32-300 accident near Jackson, Mississippi, November 13, 2012

On November 13, 2012 at about 11:15 pm local time, a Piper PA-32-300, registered N717RL, was substantially damaged in an accident during initial climb near Jackson, Mississippi (Hawkins Field). It was a personal flight under general aviation rules (Part 91). 3 people were killed. The weather was visual conditions (good weather).

Preview. This page is not yet listed for search engines.

The NTSB's probable cause their words, unchanged

The pilot's inadequate preflight inspection, which resulted in his failure to note the water in the fuel tank due to condensation, which subsequently shut down the engine in flight. Contributing to the accident was the pilot's self-induced pressure to expedite the departure.

Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.

What the record shows

Date
November 13, 2012 · about 11:15 pm local time
Place
Jackson, Mississippi · Hawkins Field · map
Type
Accident
Injuries
3 people were killed.
Weather
visual conditions (good weather)
Aircraft
Piper PA-32-300 · all PA-32-300s on the register
Registration
N717RL · registry record · serial 32-7340050
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

Before the accident flight, the airplane had sat in its hangar for the previous 2 months with its fuel tanks half full under varying temperature conditions. The pilot had planned on flying to a safety seminar that began at 1630, so he had the airplane pulled out of its hangar, and its main fuel tanks were topped off from a fuel truck. After his arrival at the airport shortly before 1700, the pilot performed a preflight inspection. The manager of the hangar facility described the pilot's preflight inspection as "real quick." A lineman observed the pilot in a position to reach the fuel strainer valve, but he did not see the pilot sumping the main fuel tanks. When the lineman drove by the airplane, he saw a puddle about 1 foot in diameter on the tarmac beneath the fuel strainer, but he did not note anything under either main fuel tank drain. The lineman also noted that the airplane had an underinflated tire, but, due to other duties, he could not warn the pilot before he taxied the airplane away. About 2 minutes after takeoff, the pilot reported an "engine problem" to air traffic control and turned the airplane back toward the airport. The airplane subsequently descended at a steep angle, consistent with a stall, into a house located in a populated area. The airplane impacted the roof, came to rest upside down, and was subsequently mostly consumed in a postcrash fire. Postaccident examination of the airplane revealed evidence indicating that the airplane was not under power at the time of the accident; the fuel-injected engine was charred and the propeller did not exhibit torsional bending or leading edge damage that would have been present if it had been under power. No preexisting mechanical anomalies were found that would have precluded normal engine operation. However, when the fuel flow divider was opened, water was found in it, which likely resulted in the loss of engine power. Water typically enters fuel tanks via three sources: leakage, normally through a fuel cap; contaminated fuel sources; and fuel tank condensation. The fuel cap was likely not the source of water since the airplane was stored in a hangar. Contaminated fuel from the fuel truck was also not the likely source of water since the truck was reportedly sumped daily. Further, on the day of the accident, five airplanes received fuel from the same truck before the accident airplane with no reports of any performance anomalies, and a clean fuel sample was taken from the truck about 20 minutes after the accident. It is more likely that condensation occurred in the half-filled fuel tanks during the previous 2 months that the airplane was sitting in the hangar under varying temperature conditions. Regardless, the pilot had an opportunity to eliminate the condensation during the preflight inspection. However, as noted previously, not enough evidence existed to determine whether the pilot actually drained each main tank to ensure that all of the water was removed. It is likely that the pilot either did not sufficiently drain the main fuel tanks or that he was relying on draining the main fuel tanks through the fuel strainer and fuel lines and did not sufficiently drain them all. Given witness statements indicating that the pilot was in a hurry and his oversight of the underinflated tire, it is likely that the pilot's preflight inspection was inadequate, which resulted in his failure to notice the fuel tank condensation.

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. Collision with terrain or object (not controlled flight into terrain) during emergency descent
  2. Fuel contamination during initial climb defining event

The NTSB's findings

  • cause Personnel issues › Action/decision › Action › Incomplete action › Pilot
  • factor Personnel issues › Psychological › Personality/attitude › Motivation/respond to pressure › Pilot
  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › (general) › Failure
  • cause Personnel issues › Task performance › Inspection › Preflight inspection › Pilot
  • cause Aircraft › Fluids/misc hardware › Fluids › Fuel › Fluid condition

Pilot

  • Certificate: airline transport pilot
  • Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instructor: instrument airplane; instructor: instrument helicopter; instrument: airplane; rotorcraft: balloon; rotorcraft: glider; rotorcraft: helicopter
  • Flight time: 17,775 hours in all; 334 in this make and model; 44 in the last 90 days; 10 in the last 30 days; 984 on instruments
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 4,413 hours
  • Last inspection: annual inspection, March 2, 2012; 28 hours since
  • Seats: 7
  • Landing gear: fixed
  • Engine: Lycoming TI0-540 SER (piston); 0 hours total
  • Fire on the ground
  • Operator: Superior Pallet CO

The flight

  • Departed from: HKS Jackson MS at 11:13 pm
  • Destination: JVW Raymond MS
  • Flight plan: none
  • Runway 16, 5,387 ft by 150 ft

Weather at the time

  • Light: daylight
  • Wind: from 010° at 3 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 52°F (11°C), dew point 28°F (-2°C)
  • Altimeter: 30.32 inHg
  • Observation at 11:15 pm from HKS, 1 miles away

Injuries

FatalSeriousMinorNone
Flig1
Passengers2

About this page

Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The docket at the NTSB holds the report as a PDF and the investigation's photographs and documents. This site never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number ERA13FA055.