LAX06CA282
2006-09-02 · Auburn, California, United States · Minor · 1 aircraft · Status: Completed
Airport AUN
Aircraft involved
Probable cause & findings
the pilot's failure to comply with weight and balance limitations and failure to attain an adequate airspeed, which resulted in a stall and loss of control.
Factual narrative
On September 2, 2006, about 0845 Pacific daylight time, a Piper PA-28-140, N4813T, collided with terrain during takeoff at Auburn Municipal Airport, Auburn, California. The pilot/owner was operating the airplane under the provisions of 14 CFR Part 91. The private pilot and two passengers sustained minor injuries; the airplane sustained substantial damage. The cross-country personal flight was originating with a planned destination of Santa Ynez, California. Visual meteorological conditions prevailed, and a visual flight rules (VFR) flight plan had been filed. The approximate global positioning system (GPS) coordinates of the primary wreckage were 38 degrees 57.28 minutes north latitude and 121 degrees 4.90 minutes west longitude. The pilot stated in a written report that he was departing from runway 7. At a speed of 65 miles per hour he rotated the nose of the airplane up for liftoff. He failed to obtain enough airspeed, which resulted in a departure stall. The pilot lost control of the airplane, collided with the ground, and went into a canal. The pilot and his passengers evacuated the airplane with minor injuries. The water in the canal was swift, and the airplane drifted downstream. The fuselage was completely submerged in the canal. The left wing was bent up sharply and sticking out of the water. The pilot stated that the airplane and engine had no mechanical failures or malfunctions. He also stated that he had not paid thorough attention to weight and balance considerations. According to the pilot the weight at the time of the accident was 2,300 pounds, which is 150 pounds above the airplane's certified maximum gross weight. Several witnesses stated they saw the airplane approaching the end of the runway with the wheels still on the ground. The airplane stalled and collided with terrain during takeoff, and went into a canal. The pilot reported that the weight of the airplane was 2,300 pounds, which is 150 pounds above the certified maximum gross weight of the airplane. He stated that he had not paid thorough attention to the weight and balance considerations. The airplane did not obtain enough airspeed at takeoff, which resulted in a departure stall, and the collision with terrain. The pilot stated that the airplane and engine had no mechanical failures or malfunctions. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_LAX06CA282.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, 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 …