CHI96LA262
1996-07-30 · CAMP LAKE, Wisconsin, United States · Minor · 1 aircraft · Status: Completed
Airport 49C
Current FAA registration · N3445K
- Make / Model
- PIPER J3C-65
- Year of manufacture
- 1946 · 50 years old at event
- Engine
- CONT MOTOR A&C65 SERIES (65 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19770120
- ADS-B equipped
- Yes — Mode-S A3CF3B
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
seizure of the number 2 piston. Inadequate maintenance was a related factor.
Factual narrative
On July 30, 1996, at 1921 central daylight time, a Piper PA-J3C, N3445K, was substantially damaged. The pilot was attempting to return to the airport for landing after he experienced engine failure after takeoff. The airplane hit a tree and remained lodged in its branches. The private pilot reported minor injuries. The 14 CFR Part 91 flight had departed the Camp Lake Airport, Camp Lake, Wisconsin, on a local flight. Visual meteorological conditions prevailed and no flight plan had been filed. The pilot reported that the number two cylinder had just been replaced on the engine. The engine had not been run since it had been repaired. He reported that he preflighted the aircraft and then did an engine run-up. He reported that he was on the ground for 20 minutes with the engine running. He then departed for a test flight around the airport. He reported that during the climb the engine began to "slow down," so he started a turn back to the airport. While he was in the turn the engine quit. He reported that due to lack of altitude he was unable to land in any clear fields, and he did a forced landing in some trees. The engine was examined and it was determined that the number two piston had seized in the cylinder. The number two cylinder's bore was a standard cylinder with .007 inch over standard. The number two piston, p/n 4557P15, a .015 inch oversized piston, was galled as a result of the engine seizure. An Airworthiness Inspector from the Federal Aviation Administration reported that measurements and tolerances of the piston could not be determined due to the galling of the piston. He reported that the cylinder and piston used for repair were used parts. The inspector reported that the mechanic who had installed the parts reported that adequate clearances existed. The pilot reported that the number two cylinder and piston had just been replaced on the engine. He preflighted the aircraft, then did a twenty minute engine run-up. He then departed for a test flight around the airport. During the climb, the engine began to 'slow down,' so the pilot started a turn back to the airport. While he was in the turn, the engine seized. The pilot reported that due to lack of altitude, he was unable to reach a clear area, and he was forced to land in trees. Examination of the engine revealed that the number two piston had seized in the cylinder. The number 2 cylinder's bore was reported to be 0.007 inch over standard, and the piston was 0.015 inch oversize. The piston was galled as a result of the engine seizure. The cylinder and piston, which were used for repair, were used parts. The mechanic who had installed the parts reported that adequate clearances had existed. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_CHI96LA262.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (stall, engine failure, maintenance). All research papers
- 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 2026 · Article (Reliability Engineering & System Safety) Understanding human error in military aviation maintenance: The role of Performance shaping factors, cognitive workload and error orientation
- 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.
- Semantic Scholar 2024 · Article (Defence Science Journal) Modelling of Human Factors in Aviation Maintenance Using HFACS ME Human Factors Analysis and Classification System Maintenance Extension and Bayesian Network
Aircraft maintenance is a complex task involving a skilled human workforce, spare parts, and various other resources. Human factors are an inherent element of the human workforce.