ERA22LA029
2021-10-23 · Westhampton Beach, New York, United States · None · 1 aircraft · Status: Completed
Airport FOK
Current FAA registration · N1188L
- Make / Model
- CESSNA 172S
- Year of manufacture
- 2006 · 15 years old at event
- Engine
- LYCOMING IO-360-L2A (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20061128
- ADS-B equipped
- Yes — Mode-S A04D66
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A total loss of engine power during cruise flight for reasons that could not be determined based on the available evidence.
Factual narrative
On October 23, 2021, about 1334 eastern daylight time, a Cessna 172S, N1188L, was substantially damaged when it was involved in an accident near Francis S Gabreski Airport (FOK), Westhampton Beach, New York. The private pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot, who was conducting a cross-country flight, reported that he heard a “pop” when the airplane was at an altitude of 3,000 ft mean sea level. Afterward, the engine lost all power, but the propeller continued to windmill. The pilot diverted to FOK, which was about 5 miles west of the airplane’s position. He also attempted to restart the engine but was unsuccessful. During the glide to FOK, the airplane impacted trees before reaching runway 24 and came to rest upright against the airport perimeter fence. Postaccident examination of the wreckage revealed substantial damage to the right wing and fuselage. Examination of the engine found that the top spark plugs, once removed, had electrodes that were intact and light gray in color. When the propeller was rotated by hand, crankshaft, camshaft, and valve train continuity were confirmed to the rear accessory section of the engine. Thumb compression was attained on all cylinders, and borescope examination of each cylinder revealed no anomalies. Both magnetos produced spark at all leads when rotated by hand. Additionally, about 35 gallons of fuel were drained after the accident, and fuel remained throughout the fuel system. The examination revealed no preimpact mechanical malfunctions that would have precluded normal engine operation. During a cross-country flight, the engine lost all power when the airplane was at an altitude of 3,000 ft mean sea level; however, the propeller continued to windmill. The pilot diverted toward an airport located about 5 miles west of the airplane’s position. He also attempted to restart the engine but was unsuccessful. During the glide to the diversion airport, the airplane impacted trees just before the intended landing runway and came to rest upright against the airport perimeter fence. Postaccident examination of the engine and its accessories revealed no preimpact mechanical malfunctions that would have precluded normal operation. Additionally, about 35 gallons of fuel were drained after the accident, and fuel remained throughout the fuel system. As a result, the cause of the loss of engine power could not be determined based on the available evidence for this investigation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Not determined-Not determined-(general)-(general)-Unknown/Not determined
Verbatim from NTSB's published report. Source file
NTSB_2021_ERA22LA029.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. All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- Embry-Riddle Scholarly Commons 2023 · Conference paper Validation of Training Satisfaction Survey
The Training Satisfaction Survey (TSS) was developed as part of a larger project to examine the features of Virtual Reality software and supporting devices as a training program on visual illusions an…
- Semantic Scholar 2021 · Article (Data in Brief) Cockpit voice recorder transcript data: Capturing safety voice and safety listening during historic aviation accidents
Cockpit Voice Recorder (CVR) transcripts capture audio data within cockpit environments. This aids the investigation of causal factors contributing to aviation accidents by revealing communication and…
- Semantic Scholar 2021 · Article (Safety Science) Safety voice and safety listening during aviation accidents: Cockpit voice recordings reveal that speaking-up to power is not enough
Abstract Safety voice is theorised as an important factor for mitigating accidents, but behavioural research during actual hazards has been scant.