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Accidents · NTSB FTW00LA202 · Final report

Piper PA-28-235 accident near Sugar Land, Texas, June 8, 2000

On June 8, 2000 at about 10:20 pm local time, a Piper PA-28-235, registered N9407W, was substantially damaged in an accident near Sugar Land, Texas (Sugar Land Municipal airport). It was a personal flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).

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The NTSB's probable cause their words, unchanged

The pilot's improper fuel tank selection, which resulted in fuel starvation. A factor was the lack of suitable terrain for the forced landing.

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

What the record shows

Date
June 8, 2000 · about 10:20 pm local time
Place
Sugar Land, Texas · Sugar Land Municipal · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Piper PA-28-235 · all PA-28-235s on the register
Registration
N9407W · registry record · serial 28-11114
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

After departure, the airplane was climbing through 1,500 feet, when the engine 'spooled down.' The pilot stated that he pushed the engine controls forward and turned on the auxiliary fuel pump; however, he did not detect a change in engine power. The pilot elected to make a forced landing in a field approximately 2 miles from the departure airport. During the landing roll, the left main landing gear impacted an ant hill and separated. The FAA inspector found the fuel selector in the off position. He added that he found the left auxiliary fuel tank 'completely empty,' the left and right main fuel tanks full, and the right auxiliary fuel tank containing 3.5 gallons of fuel. The airplane was taken to an aircraft maintenance facility where mechanics test ran the engine on the airplane. The mechanics reported that the engine would not start and run with the left auxiliary fuel tank selected; however, the engine started and ran for approximately 15 minutes on each of the remaining fuel tanks. The FAA inspector stated that the pilot indicated that he thought he had taken off with the left main fuel tank selected.

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: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 767 hours in all; 9 in this make and model; 10 in the last 90 days
  • Medical certificate: Class 3 (valid medical--w/ waivers/lim.)
  • Seat: left

The aircraft

  • Airframe total time: 3,492 hours
  • Last inspection: annual inspection, April 1, 2000
  • Maximum gross weight: 2,950 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming O-540-B4B5 (piston); 0 hours total

The flight

  • Departed from: SGR at 10:10 pm
  • Destination: IWS Houston TX
  • Flight plan: none
  • Runway 0

Weather at the time

  • Light: daylight
  • Wind: from 110° at 5 knots
  • Visibility: 6 statute miles
  • Sky: broken clouds at 5,000 ft; not recorded
  • Temperature: 79°F (26°C), dew point 0°F (-18°C)
  • Altimeter: 29.00 inHg
  • Observation at 10:20 pm from SGR, 3 miles away

Injuries

FatalSeriousMinorNone
Crew1

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 FTW00LA202.