Colorado Aviation Accidents & Incidents

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Boulder, Colorado

May 28, 2014 · NTSB CEN14LA261 · PIPER PA-25-235 (N8808L)
Minor/None
Note: This analysis may be based on NTSB preliminary reports, which represent an initial, incomplete investigation. Facts can change as the investigation progresses, and preliminary findings should not be assumed to be accurate or final. For older events, a final NTSB report may have been issued β€” always consult the NTSB Aviation Query for the authoritative record.

NTSB Narrative

On May 28, 2014, about 1500 mountain daylight time, a Piper model PA-25-235 airplane, N8808L, was substantially damaged during a forced landing near Boulder, Colorado. The commercial pilot sustained minor injuries. The airplane was registered to and operated by the Soaring Society of Boulder under the provisions of 14 Code of Federal Regulations Part 91 without a flight plan. Day visual meteorological conditions prevailed for the local glider aero-tow flight that departed Boulder Municipal Airport (BDU), Boulder, Colorado, about 1430.The pilot reported that the purpose of the accident flight was to aero-tow a glider to 10,200 feet mean sea level (msl) before returning to the departure airport. He stated that the aero-tow and glider release were uneventful. However, as the airplane was returning to BDU, the engine began to run intermittently as the airplane crossed over the foothills southwest of the airport. The engine eventually lost total power around 10,000 feet msl. The pilot reported that he did not attempt to restart the engine following the loss of engine power. He initially thought that the airplane had sufficient altitude to safely glide to the airport, but it ultimately descended to altitude that required an off-airport landing. He decided to land on a nearby soccer field; however, as he approached the field he realized that there were power lines situated alongside the road that bordered the soccer field. The airplane landing gear collided with a chain-link fence as he maneuvered the airplane below the power lines. After the landing gear became entangled with the fence, the airplane collided with the road before it came to rest in a drainage ditch. The right wing sustained substantial damage during the collision with the fence and terrain.

The airplane's single fuel tank held 38 gallons, of which 2 gallons were considered unusable. The pilot reported that, before his first flight of the day, the fuel level was about 1-inch from the top of the filler neck and that the fuel quantity sight gauge indicated that the tank was near capacity. The airplane operator reported that a 1-inch void at the top of the tank equated to about 3.5 gallons of unused tank capacity. Therefore, before the pilot's first flight of the day, the total useable fuel was about 32.5 gallons.

The recording tachometer indicated 3,607.7 hours before the pilot's first flight of the day and 3,609.9 hours following the accident, equating to 2.2 tachometer hours having been accumulated since the last refueling. The calculated average fuel consumption rate was about 14.8 gallons per tachometer hour since the last refueling.

The airplane operator reported that, according to historical fueling and flight data, obtained from January-March 2014, the airplane's average fuel consumption rate was about 10.2 gallons per tachometer hour. Additionally, the previous pilot had flown 13 aero-tows with an average fuel consumption rate of 10.3 gallons per tachometer hour. The previous p

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NTSB Findings

  • Aircraft-Fluids/misc hardware-Fluids-Fuel-Related operating info - C
  • Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid level - C
  • Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot - C
  • Personnel issues-Action/decision-Info processing/decision-Identification/recognition-Pilot - C

Details

NTSB ReportCEN14LA261
AircraftPIPER PA-25-235
RegistrationN8808L
DamageSUBS
FAR Part091
Location40.0403, -105.2483
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