SEA03LA067
2003-04-19 · Orofino, Idaho, United States · None · 1 aircraft · Status: Completed
Airport S68
Current FAA registration · N6268W
- 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
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 ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (stall, loss of control). All research papers
- 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…
- 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.
- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
In Urban Air Mobility (UAM), maintaining a minimum separation between aircraft is a safety requirement, which becomes challenging amidst congested air traffic and off-nominal conditions, such as Loss …