ERA23LA229
2023-05-11 · South Bethlehem, New York, United States · Serious · 1 aircraft · Status: Completed
Airport 4B0
Current FAA registration · N1596E
- Make / Model
- CESSNA 172N
- Engine
- LYCOMING O-360 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20021217
- ADS-B equipped
- Yes — Mode-S A0EECD
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s improper decision to attempt an intersection takeoff in a tailwind when the full runway in the opposite, headwind direction was available.
Factual narrative
On May 11, 2023, about 1420 eastern daylight time, a Cessna 172N, N1596E, was substantially damaged when it was involved in an accident near South Bethlehem, New York. The private pilot and one passenger suffered serious injuries, while a second passenger incurred minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that his injuries included a vertebrae fracture and concussion, and he could not recall the accident sequence. A pilot-rated witness reported that the airplane was attempting to take off from runway 19 at South Albany Airport (4B0), South Bethlehem, New York. Runway 19 was 2,853 ft-long, 60 ft-wide, and consisted of asphalt. About 15 minutes before the accident takeoff, another Cessna 172 performed a tailwind takeoff on runway 19 uneventfully; however, that airplane started its takeoff roll at the beginning of the runway. The accident airplane took off beginning at a runway intersection, with about 2,293 ft of runway remaining, in an approximate 9-kt tailwind, gusting to 13 or 14 kts. The accident airplane subsequently impacted a field near the departure end of runway 19 and came to rest upright. Examination of the wreckage by a Federal Aviation Administration inspector revealed substantial damage to the left wing and fuselage. The inspector observed the flaps in the retracted position and did not note evidence of any preimpact mechanical malfunctions. Following the wreckage recovery to a storage facility, recovery company personnel were able to rotate the propeller by hand, confirm powertrain continuity to the rear accessory section, and attain thumb compression on all cylinders. Review of weight and balance data for the airplane revealed that it had a useful load of 820 lbs. The reported occupant weights totaled about 740 lbs., leaving 80 lbs for fuel and baggage. The amount of fuel onboard and weight of the baggage was unknown. Review of performance data from a make and model pilot operating handbook revealed that, at maximum gross weight and in the reported wind and temperature conditions, the airplane required about 2,300 ft of runway to take off and clear a 50-ft obstacle. There were no performance data for any tailwind greater than 10 knots or any weight above the maximum gross weight. Due to his injuries, the pilot did not recall the accident. A pilot-rated witness reported seeing the airplane make an intersection takeoff from a 2,853-ft-long runway with a tailwind (9 kts, gusting to 13 or 14 kts). The intersection used resulted in only 2,293 ft of runway available. The accident airplane subsequently impacted a field near the departure end of the runway and came to rest upright. Postaccident examination of the wreckage did not reveal evidence of any preimpact mechanical malfunctions. Review of weight and balance data for the airplane revealed that it was loaded to within 80 pounds of its maximum gross weight before accounting for baggage and fuel (the quantities of which could not be determined). Review of performance data revealed that at maximum gross weight, in the reported wind and temperature conditions, the airplane required about 2,300 ft of runway to take off to clear a 50-ft obstacle. There were no performance data for tailwind conditions greater than 10 knots or any weight above the maximum gross weight. Based on the takeoff performance data, the pilot was likely attempting to operate the airplane in excess of its performance capabilities, which resulted in a subsequent collision with terrain when it was unable to climb. Instead of departing with a tailwind, and from an intersection with a reduced amount of runway remaining, had the pilot instead elected to depart in the opposite direction utilizing the full runway length, it is possible that the accident could have been avoided. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
- — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Decision related to condition
- — Aircraft-Aircraft oper/perf/capability-Aircraft capability-Takeoff distance-Capability exceeded
Verbatim from NTSB's published report. Source file
NTSB_2023_ERA23LA229.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. 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.