NTSB CAROL · Event
Event ANC96LA074
Registry · N3795L
FAA Aircraft Registry record.
Make / Model
CESSNA 172G
Engine
CONT MOTOR 0-300 SER (145 hp)
Seats / Engines
4 seats · 1 engine
ADS-B equipped
Yes — Mode-S A4584C
Registrant of record
CISNEROS ADRIAN
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's premature flare and the flight instructor's failure to perform remedial action prior to the hard landing.
Factual narrative
On May 1, 1996, approximately 1800 Alaska daylight time, a wheel equipped Cessna 172 airplane, N3795L, registered to and operated by Smith Aero Services of Fairbanks, Alaska, experienced a hard landing causing damage to the firewall while performing touch and go landings at Fairbanks International Airport, Fairbanks, Alaska. The instructional flight, operating under 14 CFR Part 91, departed Fairbanks for a local flight. No flight plan was filed and visual meteorological conditions prevailed. The certificated flight instructor and the student were not injured and the airplane received substantial damage. During a telephone conversation with the flight instructor on May 24, 1996, she stated that during one of the landings the student flared higher than normal and the airplane struck the ground in a three point attitude. She felt that the landing was not unusually hard so they continued to perform touch and go landings. After the flight, the student, who had ten hours of total flight time, performed the walk around inspection and did not see any damage. The flight instructor did not perform the walk around inspection with the student. Approximately three days later, another instructor noticed that the control yoke would not move through its entire forward range of travel. Later examination showed that the firewall was bent and the surrounding structure was impeding the control yoke's movement. The flight instructor believes that they did not cause the damage because during the remainder of their flight they did not encounter restrictions during the control yoke's movements. However, the company records show that the airplane had not flown since their flight. The operator was sent an NTSB Form 6120.1/2 on May 28, 1996 and June 11,1996. The flight instructor stated she did not feel this was an accident and she did not complete and return the NTSB Form 6120.1/2. The flight instructor and student were practicing soft field landings. The instructor stated that the student flared the airplane too high during a landing, The airplane landed hard on all three wheels simultaneously. After the flight's termination, the student performed the post flight walk around inspection. The instructor did not perform the walk around with the student. The next flight instructor, during the taxi/run up, found that the flight controls would not move through their entire range of travel. Subsequent examination of the airplane showed that the firewall was bent and restricted the forward motion of the control yoke. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_ANC96LA074.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 (icing). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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.
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
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