NTSB CAROL · Event
Event DCA95MA006
Registry · N918AE
FAA Aircraft Registry record.
Make / Model
EMBRAER EMB-145LR
Year of manufacture
2005
Engine
ROLLS-ROYC AE3007 SER
Seats / Engines
55 seats · 2 engines
Last airworthiness date
20050331
ADS-B equipped
Yes — Mode-S ACB468
Registrant of record
AMERICAN AIRLINES INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
1) the captain's improper assumption that an engine had failed, and 2) the captain's subsequent failure to follow approved procedures for engine failure, single-engine approach and go-around, and stall recovery. Contributing to the cause of the accident was the failure of AMR Eagle/Flagship management to identify, document, monitor, and remedy deficiencies in pilot performance and training. (NTSB Report AAR-95/07)
Factual narrative
The crew of American Eagle Flight 3379 was completing the return leg of a scheduled out-and-back trip sequence between Raleigh Durham, North Carolina and Greensboro, North Carolina. The flight was cleared for runway 5 left ILS approach. The crew switched radio frequencies to Raleigh Durham tower, and the local air traffic controller cleared the flight to land at 1832:20 eastern standard time. The aircraft crashed approximately four miles southwest of the runway threshold in a wooded area. The pilot, co-pilot and thirteen passengers were fatally injured, while the other five passengers were seriously injured. A post crash fire was extinguished by the Morrisville Fire Department and other agencies in Wake County. The weather report from Raleigh Durham weather facility at the time of the accident reported the ceiling at 500 feet overcast, 2 miles visibility in light rain and fog, wind 010 degrees at 8 knots, temperature 38 degrees (F), dew point 36 degrees (F), and altimeter 30.31 inches. ADDITIONAL PARTIES INCLUDE: capt Joe Oyler, Allied Pilots Assoc, 2214 Paddock Way, Grand Prairie, TX, 75050; Gary Parham, NATCA, 108 Quail Run Circle, Stockbridge, GA 30281; Tom Knopp, McCauley Propeller, 3535 McCauley Drive, Vandalia, OH 45377 The airplane crashed about 4 miles southwest of the runway 5L threshold during an ILS approach. The captain had associated the illumination of the left engine IGN light, illuminated as a result of a momentary negative torque condition when the propeller speed levers were advanced tp 100% and the power levers were at flight idle, with an engine failure. There was no evidence of an engine failure. The captain failed to follow established procedures for engine failure identification, single engine appoach, single engine go-around, and stall recovery. AMR Eagle training did not adequately address the recognition of engine failure at low power, the aerodynamic effects of asymmetric thrust from a 'windmilling' propeller, and high thrust on the other engine. AMR Eagle and Flagship Airlines crew training records do not provide sufficient detail for management to track performance. Flagship Airlines management was deficient in its knowledge of the types of crew records available, and in the content and use of such records. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_DCA95MA006.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 (stall, engine failure, go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
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