NTSB CAROL · Event
Event FTW97LA371
Registry · N260MT
FAA Aircraft Registry record.
Make / Model
SIAI-MARCHETTI F.260
Year of manufacture
1972 · 25 years old at event
Engine
LYCOMING O-540-E4A5 (260 hp)
Seats / Engines
3 seats · 1 engine
Last airworthiness date
20121219
ADS-B equipped
Yes — Mode-S A28022
Registrant of record
CARLOMAGNO KENT GENE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
improper planning/decision by the pilot, which led to fuel exhaustion, loss of engine power, and a forced landing. A related factor was the lack of suitable terrain for the forced landing.
Factual narrative
On September 30, 1997, at 1530 mountain daylight time, a Siai-Marchetti F.260 airplane, N260MT, owned and operated by the pilot, was substantially damaged during a forced landing following a loss of engine power near Santa Rosa, New Mexico. Visual meteorological conditions prevailed, and a VFR flight plan was filed for the Title 14 CFR Part 91 personal cross country flight. The commercial pilot, sole occupant of the airplane, sustained minor injuries. The flight originated from Palm Springs, California, about 3 hours 45 minutes prior to the accident. The pilot reported on the enclosed Pilot/Operator Aircraft Accident Report that he fueled the airplane prior to departing Palm Springs, California, and planned to stop at Santa Rosa, New Mexico, for fuel. Approximately 20 minutes prior to the Santa Rosa Municipal Airport, at the beginning of initial descent, the airplane's engine lost power. He initiated a forced landing to a dirt road, which was located approximately 1/2 mile south of Interstate 40. During descent the he "attempted a restart w/opposite wing tank selected;" however, the engine did not start. The pilot further reported that his "last fuel check indicated 1/8 - 1/4 fuel in both wing tanks, wing tip tanks empty." Examination of the accident site by two FAA inspectors revealed that during the landing roll, the aircraft's nose landing gear impacted a ditch separating its wheel. The aircraft continued across the dirt road, crossed another ditch and nosed over to the inverted position. Examination of the aircraft by the FAA inspectors revealed that the vertical stabilizer's aft spar was fractured. The right wing's spar was buckled and cracked two feet from the wing tip. The left and right wing tip tanks were damaged, and the fuselage was wrinkled. The nose landing gear was separated at the fork, and the right main landing gear was collapsed. Examination of the aircraft's fuel system revealed that the fuel selector was found in the left tip tank position. The main fuel tanks and the wing tip tanks were "void of fuel," and "there were not any fuel stains on the aircraft or the ground." The carburetor fuel bowl had approximately 0.5 ounce of fuel, and residual fuel was found in the fuel line to the gascolator and the gascolator. Approximately 20 minutes before reaching a planned fuel stop at Santa Rosa, NM, the engine lost power. The pilot initiated a forced landing to a dirt road. During the descent, he 'attempted a restart w/opposite wing tank selected;' however, the engine did not start. The pilot reported that his 'last fuel check indicated 1/8 - 1/4 fuel in both wing tanks, wing tip tanks empty.' During the landing roll, the nose landing gear impacted a ditch separating its wheel. The aircraft continued across the dirt road, crossed another ditch, and nosed over. Examination of the aircraft's fuel system revealed that the fuel selector was in the left tip tank position. The main fuel tanks and the wing tip tanks were 'void of fuel,' and 'there were not any fuel stains on the aircraft or the ground.' Only residual fuel was found in the fuel line to the gascolator and in the gascolator, and the carburetor fuel bowl had approximately 0.5 ounce of fuel. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_FTW97LA371.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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