CEN12LA543
2012-08-07 · Westcliffe, Colorado, United States · Serious · 1 aircraft · Status: Completed
Airport C08
Current FAA registration · N71AJ
- Make / Model
- GLASAIR GLASAIR III
- Year of manufacture
- 2010 · 2 years old at event
- Engine
- LYCOMING IO-540-K1A5 (300 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 20140723
- ADS-B equipped
- Yes — Mode-S A979BD
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of oil pressure due to the failure of an oil filter gasket, which resulted in a total loss of engine power.
Factual narrative
On August 7, 2012, about 0830 mountain daylight time a kit-built Glasair III airplane, N71AJ, was substantially damaged during a forced landing near Westcliffe, Colorado. The private pilot was seriously injured. The airplane was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91, as a personal flight. Visual meteorological conditions prevailed for the local flight, which operated without a flight plan. The local test flight originated from the Silver West Airport (C08), Westcliffe, Colorado, about 0810. According to the owner, the accident flight was the airplane's first flight of a 40-hour test flight program. The pilot departed C08 and climbed to 12,000 feet. The pilot noticed that the oil temperature began to increase and then noted a loss of oil pressure. The engine stopped producing power and the pilot performed a forced landing to a field. The airplane sustained substantial damage to its fuselage. An examination of the engine revealed that a gasket between the remote oil filter adapter and the "spin-on" filter mounting pad had failed which resulted in a loss of oil. The owner reported that the gasket was lubricated with a compound upon installation. It could not be determined if the compound degraded the gasket. After leveling off at 12,000 feet mean sea level for a test flight, the pilot noticed that the oil temperature began to increase, and then the engine lost oil pressure. The engine then lost total power, and the pilot performed a forced landing in a field. An examination of the engine revealed that a gasket between the remote oil filter adapter and the "spin-on" filter mounting pad had failed, which resulted in a loss of oil. The owner reported that he had lubricated the gasket with a compound upon installation. It could not be determined whether the compound had degraded the gasket. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft power plant-Engine (reciprocating)-Recip eng oil sys-Failure - C
Verbatim from NTSB's published report. Source file
NTSB_2012_CEN12LA543.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). 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…