NTSB CAROL · Event
Event ANC19LA005
Registry · N3227M
FAA Aircraft Registry record.
Make / Model
PIPER PA-12
Year of manufacture
1947 · 71 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
3 seats · 1 engine
Last airworthiness date
19620928
ADS-B equipped
Yes — Mode-S A37917
Registrant of record
PARKER SHON T
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power shortly after takeoff for reasons that could not be determined based on the available information, which resulted in an emergency landing and collision with trees.
Factual narrative
On November 1, 2018, about 1630 Alaska daylight time, a Piper PA-12 airplane, N3227M, sustained substantial damage during a forced landing, following a total loss of engine power about 8 miles northwest of Willow Airport (PAUO) near Willow, Alaska. The airplane was registered to and operated by the pilot as a 14 Code of Federal Regulations (CFR) Part 91 visual flight rules flight when the accident occurred. The commercial pilot sustained serious injuries. Visual meteorological conditions prevailed and no flight plan had been filed for the local area flight. The flight had departed a private airstrip located about 1 mile east of the accident location at about 1629. According to the pilot, during the initial climb, the engine popped three times "like a backfire", and then lost all power. He switched from operating on the left fuel tank to the right fuel tank and applied the carburetor heat, but the engine failed to respond. Subsequently, during the forced landing into trees, the airplane sustained substantial damage to the wings and fuselage. A friend of the pilot stated that this was the first flight following engine maintenance, where he, an airframe and powerplant mechanic, and the pilot had been troubleshooting for excessive magneto drops and a cold cylinder. He added that, they had just reinstalled the fine wire spark plugs after cleaning them. The National Transportation Safety Board (NTSB) investigator-in-charge, along with another NTSB investigator conducted a post-accident examination of the airplane following recovery. The spark plugs and rocker arm covers were removed from the engine and all spark plugs exhibited normal operational signatures with no defects or anomalies noted. The crankshaft was rotated by hand and thumb compression and suction were obtained on all four cylinders, and continuity was established throughout the engine and valvetrain. The wiring from the ignition switch to the magnetos was frayed and separated. It could not be determined if the separation happened before the accident or as a result of the accident. Both magnetos were removed from the engine and tested at Alaskan Aircraft Engines in Anchorage, Alaska. Both magnetos produced spark at all terminals as designed. Neither distributor was fractured, however the impulse coupler inside the left magneto was fractured but that did not preclude the magneto from sparking. The ignition harness was removed from the airplane and sent to Continental Motors for testing. The ignition switch was connected to a magneto synchronizer box (Model E50). The key was rotated through the OFF, L, R, and BOTH positions of the ignition switch with normal function observed. According to the pilot, during the initial climb on the personal flight, the engine backfired and then lost total power. He was unable to restore power, and during the subsequent off-airport forced landing, the airplane collided with a stand of trees, which resulted in substantial damage to the wings and fuselage. A mechanic/friend of the pilot stated that this was the first flight after engine maintenance, during which he and the pilot had been troubleshooting for excessive magneto drops and a cold cylinder. He added that they had just reinstalled the fine wire spark plugs after cleaning them. A postaccident examination of the airplane revealed that all spark plugs exhibited normal operational signatures with no defects or anomalies noted. Both magnetos produced spark at all terminals as designed. The impulse coupler inside the left magneto was fractured, but that did not preclude the magneto from sparking. Additionally, the wiring harness from the ignition switch to the magnetos was frayed and separated. However, it could not be determined if the separation occurred as a result of the accident. Thus, the reason(s) for the loss of engine power could not be determined. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
- — Environmental issues-Physical environment-Object/animal/substance-Tree(s)-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2018_ANC19LA005.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, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2023 · Conference paper
The Value of Strong Partnerships to Build a Successful Aviation Maintenance Career Pathway Program for Transitioning Military Service Members
The aerospace industry is competing with other industries for a qualified workforce, and many of those competing industries are investing heavily in creating workforce development pipelines.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- 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 …
- Semantic Scholar 2025 · Article (Applied Sciences)
Decision-Making Framework for Aviation Safety in Predictive Maintenance Strategies
The implementation of predictive maintenance (PM) in aviation presents unique challenges due to strict safety requirements, complex operational environments, and regulatory constraints.
- Embry-Riddle Scholarly Commons 2024 · Journal article (JAAER)
Low-Resource Automatic Speech Recognition Domain Adaptation – A Case-Study in Aviation Maintenance
With timeliness and efficiency being critical in the aviation maintenance industry, the need has been growing for smart technological solutions that optimize and streamline the different underlying ta…
- Embry-Riddle Scholarly Commons 2024 · Journal article (JAAER)
A New Trajectory in UAV Safety: Leveraging Reinforcement Learning for Distance Maintenance Under Wind Variations
In the field of aviation, safety is a critical cornerstone, and the operation of Unmanned Aerial Vehicle (UAV) systems is deeply connected with this principle.
Browse the full corpus — academia portal ↗