CHI94LA261
1994-08-02 · ABERDEEN, South Dakota, United States · None · 1 aircraft · Status: Completed
Airport ABR
Current FAA registration · N35790
- Make / Model
- CESSNA 172I
- Year of manufacture
- 1968 · 26 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19680720
- ADS-B equipped
- Yes — Mode-S A4027A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain directional control during landing. A related factor is the dark night conditions.
Factual narrative
On August 2, 1994, at 0025 central daylight time, a Cessna 172, N35790, operated by a private pilot on a personal flight, sustained substantial damage during a hard landing at the Aberdeen Regional Airport, in Aberdeen, South Dakota. The private pilot and the one passenger reported no injuries. Visual meteorological conditions prevailed for the night flight, no flight plan was filed. The flight operated under 14 CFR Part 91, and originated from Rapid City, South Dakota approximately 2115. The pilot stated he experienced a loss of electrical power while en route to Aberdeen. When the airplane arrived in the vicinity of the Aberdeen Regional Airport, the pilot attempted to establish radio contact without success. He stated he circled the airport several times to obtain wind and runway information, then began an approach to land on Runway 17. The pilot stated it was a dark night. The pilot reported the approach looked good, but when the airplane touched down it suddenly veered to the right and departed the runway. The pilot stated he tried to regain directional control by adding "...full left aileron, full flare to lighten load on right..." The airplane struck a runway light, then veered back to the left. The nosewheel collapsed and the airplane came to rest on the runway. The pilot stated he thought a tire blew on landing, and the passenger reported she heard a "pop" at the time of touchdown. Postaccident investigation revealed although there was damage to the tire and valve stem, there was no evidence of tire blow out. The tire was reported to be in good condition, with slight wear. An FAA Inspector's statement is appended. Maintenance personnel reported when the master switch was activated during postaccident examination, the battery power was sufficient to retract the flaps. The alternator was removed from the airplane and bench tested, with no anomalies noted. THE PILOT STATED THE APPROACH TO LANDING LOOKED GOOD. WHEN THE AIRPLANE TOUCHED DOWN, IT SUDDENLY VEERED OFF THE RIGHT SIDE OF THE RUNWAY AND COLLIDED WITH A RUNWAY LIGHT. THE PILOT STATED HE APPLIED '...FULL LEFT AILERON AND FULL FLARE...' TO REGAIN DIRECTIONAL CONTROL. THE AIRPLANE VEERED BACK ONTO THE RUNWAY AND CAME TO REST IN THE MIDDLE OF THE RUNWAY WITH THE NOSEWHEEL COLLAPSED. THE PILOT STATED HE THOUGHT A TIRE HAD BLOWN. POSTACCIDENT INVESTIGATION REVEALED NO EVIDENCE OF A BLOW OUT OR ANY PREIMPACT MALFUNCTION. THE ACCIDENT OCCURRED AT 0025 LOCAL IN WHAT THE PILOT DESCRIBED AS DARK NIGHT LIGHT CONDITIONS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_CHI94LA261.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 or causal vocabulary (maintenance). 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.
- Semantic Scholar 2020 · Article (Collegiate Aviation Review International) From Classroom to Industry: Human Factors in Aviation Maintenance Decision-Making
The presence of human factors in aviation remains a critical area of research given the safety implications of human error.
- 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…
- 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