Pilot Debrief

PIPER PA-28-235 near Presidio, TX — 2021-12-30

Final reportCEN22LA091
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Date
2021-12-30
Location
Presidio, TX, USA
Airport
PRS
Aircraft
PIPER PA-28-235
Registration
N8591W
Category
Airplane
Highest injury
Serious
Fatalities
0
Phase of flight
Takeoff roll

Probable cause

The non-certificated pilot’s failure to perform a preflight weight and balance calculation and his decision to operate the airplane beyond the allowable center of gravity limitations, which resulted in a loss of control and impact with terrain.

NTSB narrative

The non-certificated pilot and 5 passengers intended to complete a personal flight. After takeoff, the airplane impacted the ground about 600 yards from the end of the runway. The airplane came to rest upright about 50 yards from the initial impact point. The pilot fled the scene and was not available during the investigation. The passengers were transported to medical facilities for treatment and did not provide any information for the investigation. Postaccident examination of the airplane revealed signs that the engine was producing power at the time of impact. There was no evidence of fuel in any of the fuel tanks or on the ground near the airplane, but one fuel tank was breached at the leading edge during the accident sequence. The examination did not reveal any preaccident mechanical malfunctions or anomalies that would have precluded normal operation. Local law enforcement stated that the total weight of the occupants was about 1,153 lbs. A fuel receipt showed that the airplane had been fueled with 42.23 gallons of fuel about 2 hours before the accident flight, at another airport about 142 nautical miles (nm) away. Due to the damage to the airplane, the investigation was unable to determine the amount of fuel onboard at the time of the accident. The estimated takeoff weight of the airplane was between 2,642 lbs and 2,775 lbs, and the maximum gross weight of the airplane was 2,900 lbs. The estimated center of gravity was between +93.89 and +93.94 inches aft of datum, which was aft of the allowable limit of +93.5 inches aft of datum. It is likely that the pilot did not complete a preflight weight and balance calculation, which would have determined that the center of gravity would have been aft of the allowable limits. The aft center of gravity would have reduced the longitudinal stability during the climb out.

Analysis

Primary failure mode
Fuel management
First missed decision gate
Pilot could have ensured adequate fuel before departure from Winkler County Airport.

NTSB coding

Evidence available

  • Photos
  • 4 docket documents
View NTSB final reportView NTSB docket

Docket documents4

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