IAD03LA022
2002-12-04 · Leeds, Massachusetts, United States · Minor · 1 aircraft · Status: Completed
Airport BAF
Aircraft involved
Probable cause & findings
The flight instructor's failure to ensure adequate fuel onboard, which resulted in fuel exhaustion and a total loss of engine power.
Factual narrative
On December 4, 2002, about 1715 eastern standard time, a Cessna 172H, N2706L, was substantially damaged during a collision with trees and terrain following a loss of engine power and a forced landing near Leeds, Massachusetts. The certificated flight instructor and the certificated student pilot received minor injuries. Night visual meteorological conditions prevailed for the local instructional flight that departed Barnes Municipal Airport (BAF), Westfield, Massachusetts. No flight plan was filed for the flight conducted under 14 CFR Part 91. According to the flight instructor, the purpose of the flight was to perform a pre-solo evaluation of another instructor's student. The student performed the preflight inspection of the airplane by the checklist under the supervision of the flight instructor. The student pilot checked the fuel gauges and looked in the tanks, but did not "stick" the tanks and confirm the exact quantity. He estimated that each tank was about "three-quarters" full. The fuel samples drained from the wings and the fuel strainer were absent of water and debris. The student pilot performed the engine start, run-up procedures, and before-takeoff checks, and all indications were normal. He then flew out to the local training area and performed steep turns. The flight instructor noted some minor deficiencies in the student's technique, and demonstrated the use of pitch and power to smooth the maneuver. They then transitioned to minimum-controllable-airspeed maneuvers, then to power-off stalls. During a stall recovery, the flight instructor noticed a reduction in engine power. He adjusted the throttle, mixture, and carburetor heat controls but the engine stopped producing power, and the propeller stopped completely. During the subsequent descent, the flight instructor contacted air traffic control (ATC), declared an emergency, and selected a field for the forced landing area. The airplane struck trees prior to the field, descended to the ground, nosed over, and came to rest inverted. The airplane was examined at the site by a Federal Aviation Administration (FAA) team of inspectors. The inspector-in-charge said there was only a faint odor of fuel, and there was no evidence of fuel spillage at the scene. During recovery of the airplane, both wings were removed. The right fuel tank was intact and contained no fuel. An attachment screw for a wing tank access panel punctured the left tank during the accident sequence. There was no fuel in the tank, and no evidence of leakage through the hole. After recovery, the engine was rotated by hand, and continuity was established through the powertrain and valvetrain back to the accessory section. Both magnetos "snapped" during rotation. The fuel line to the carburetor was dry, and the carburetor contained no fuel. The flight instructor held a commercial pilot certificate with ratings for airplane single engine land, and instrument airplane. He held a flight instructor certificate with a rating for airplane single engine land. His most recent second-class medical certificate was issued May 14, 2002. The flight instructor reported approximately 1,200 hours of flight experience, 550 hours of which were in the Cessna 172. The student pilot was interviewed by telephone. His account of the events was consistent with that provided by the flight instructor. The student pilot was issued a third class medical certificate on August 7, 2002. He reported 14 hours of flight experience, all of which was in the Cessna 172. Both pilots reported there were no anomalies with the handling and performance of the airplane prior to the loss of engine power. The student pilot added that at one point during the flight he noticed the fuel gauges "bouncing between the one-half and three-quarters" position. He also noticed a faint odor of fuel, but didn't report it to the flight instructor. The engine was removed from the airplane, and taken to East Coast Aero Tech, where it was mounted on a donor airframe and tested. The engine ran without any problem. At 1653, the weather reported at Barnes Municipal Airport included clear skies with winds from 340 degrees at 6 knots. Official sunset was at 1621. The moon set at 1640, and was 28 degrees below the horizon at the time of the accident. The student pilot performed the preflight inspection, by the checklist, and under the supervision of the flight instructor, for the dual instructional flight. He checked the fuel gauges and looked in the tanks, but he did not "stick" the tanks and confirm the exact fuel quantity. He estimated that each tank was about "three-quarters" full. Fuel samples drained from the wings and the fuel strainer were absent of water and debris. The student pilot performed the engine start, run-up procedures, and before-takeoff checks, and all indications were normal. He then flew out to the local training area and performed steep turns. The flight instructor noted some minor deficiencies in the student's technique, and demonstrated the use of pitch and power to smooth the maneuver. They then transitioned to minimum-controllable-airspeed maneuvers, then to power-off stalls. During a stall recovery, the flight instructor noticed a reduction in engine power. He adjusted the throttle, mixture, and carburetor heat controls but the engine stopped producing power, and the propeller stopped completely. During the subsequent descent, the flight instructor contacted air traffic control, declared an emergency, and selected a field for the night forced landing. The airplane struck trees prior to the field, descended to the ground, nosed over, and came to rest inverted. There was only a faint odor of fuel and no evidence of fuel spillage at the scene. There was also no evidence of fuel in either fuel tank. Examination of the engine revealed no anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_IAD03LA022.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall, fuel exhaustion). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…