NTSB CAROL · Event
Event SEA03LA067
Registry · N6268W
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-140
Year of manufacture
1964 · 39 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19640826
ADS-B equipped
Yes — Mode-S A8300C
Registrant of record
TERESHCHENKOV NIKITA
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's misjudgment of speed and distance resulting in a loss of airspeed, stall and undershoot of runway.
Factual narrative
On April 19, 2003, approximately 1100 Pacific daylight time, a Piper PA-28-140 single-engine airplane, N6268W, was substantially damaged during an undershoot and loss of control on landing at the Orofino Municipal Airport, Orofino, Idaho. The airplane was registered to a private individual and operated by the pilot. The student pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 CFR Part 91 instructional flight. The cross-country flight originated from the Lewiston-Nez Perce County Airport, Lewiston, Idaho, at 1000. According to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the pilot reported that after setting up on a one-mile final for runway 27 (2,500' X 50'), "I realized I was a little low and slow on the glideslope and slowly started adding power." The pilot further stated that on a 1/4 mile final coming in over the river which borders the runway on the east, the aircraft lost lift and impacted the grassy approach area 50 feet short of the runway. The pilot also reported that the landing marks indicated the main gear touched down first, then the nose gear began collapsing on contact. The aircraft veered left across the end of the runway and onto a grassy area where it skidded for 100 yards before coming to rest in an upright position. An FAA inspector, who responded to the accident site, reported substantial damage to the firewall as a result of the nose gear collapsing rearward, a small dent in the leading edge of the right wing, and damage to both propeller blades, the result of a propeller strike. The pilot set up for landing on runway 27 (2,500' X 50'). When he was approximately on a one-mile final he realized he was a little low and slow, and slowly started adding power. As the airplane came in over the river which borders the runway on the east, about a 1/4 mile final, it experienced a loss of lift and subsequently impacted terrain 50 feet short of the runway. The aircraft veered onto a grassy area where it skidded for 100 yards before coming to rest in an upright position. Both propeller blades were damaged, the nose gear collapsed rearward, the leading edge of the right wing was dented as a result of impacting a runway edge light, and there was substantial damage to the firewall. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_SEA03LA067.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, loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
Browse the full corpus — academia portal ↗