NTSB CAROL · Event
Event FTW97LA158
Aircraft involved
Probable cause & findings
the pilot's improper plannning/decision, which resulted in loss of engine power (both engines) due to fuel exhaustion. Darkness was a related factor.
Factual narrative
On April 12, 1997, at 0454 mountain standard time, a Piper PA-31-350, Mexican registration XASBM, was substantially damaged during a forced landing following a loss of engine power (both engines) at El Paso International Airport, El Paso, Texas. The international on-demand air cargo flight, operating under Title 14 CFR Part 129, was repositioning to El Paso after a cargo delivery to Mexico. The two occupants, the pilot-in-command and one pilot rated passenger, were not injured. Visual meteorological conditions prevailed, and an instrument flight plan was filed. The flight originated at 0130 from Monterey, Mexico. According to El Paso tower personnel, at 0440, the pilot of XASBM reported in on tower frequency to commence an approach to the airport. At 0446, tower issued a clearance to the pilot to descend to 7,000 feet. Approximately 0449, the pilot advised tower that the airport was in sight, and then was cleared for a visual approach and landing to runway 26L. At 0451, the pilot advised tower the aircraft's engines were "starving for fuel, mayday." He relayed to tower that he thought that he could make runway 26L, but subsequently requested the taxiway and stated that he had "two dead engines." Approximately 0454, tower personnel observed the aircraft touch down on taxiway "L", proceed to skid off the taxiway, and come to rest south of the taxiway, near the intersection of taxiway "L" and taxiway "V". In a written statement, the pilot reported that he fueled the aircraft to a total of 150 gallons prior to departure from Monterey, Mexico. He stated that he flew the aircraft at an altitude of 16,000 feet and operated the engines at "best economy" for the 3 hour flight from Monterey to El Paso. He further stated that the landing gear did not fully extend prior to ground contact, resulting in structural damage to the wings and fuselage. According to the engine manufacturer's operator manual, the following fuel consumption chart outlines approximate fuel burn rates at several different power settings: OPERATION RPM HP GALLONS PER HOUR / PER ENGINE Normal Rated 2,500 350 38.5 Performance 2,400 260 22.0 Cruise(75%rated) Economy 2,200 210 15.0 Cruise(60%rated) After approximately 3 hours and 10 minutes of uneventful flight, the pilot of the twin engine airplane declared an emergency, citing that both engines were starving for fuel. At that time, the airplane was about 5 miles south of the destination airport. Unable to safety reach a runway, the pilot elected to land on taxiway 'L.' However, the landing gear did not fully extend before touch down, and the airplane was subsequently damaged. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_FTW97LA158.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (fuel exhaustion). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- AOPA Air Safety Institute 2023 · Safety advisor
Safety Advisor: Fuel Awareness
AOPA Air Safety Institute safety advisor on preventing fuel-exhaustion and fuel-starvation accidents in general aviation. Covers pre-flight fuel planning, reserve requirements (14 CFR 91.151, 91.167),…
- NASA NTRS 2019 · Abstract
U.S. Civil Rotorcraft Accidents, 1963 through 1997
The U.S. National Transportation Safety Board (NTSB) has recorded 8,436 rotorcraft accidents during the period mid - 1963 through the end of 1997.
- NASA NTRS 2019 · Contractor Report (CR)
A study of carburetor/induction system icing in general aviation accidents
An assessment of the frequency and severity of carburetor/induction icing in general-aviation accidents was performed. The available literature and accident data from the National Transportation Safet…
- NASA NTRS 2018 · Other
Parachuting to Safety
NASA's Langley Research Center awarded Ballistic Recovery Systems, Inc., three Small Business Innovation Research (SBIR) contracts to research and develop a new, low cost, lightweight recovery system …
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