GAA16CA340
2016-05-31 · Lumberton, New Jersey, United States · None · 1 aircraft · Status: Completed
Airport VAY
Current FAA registration · N7095G
- Make / Model
- CESSNA 172K
- Year of manufacture
- 1969 · 47 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19691211
- ADS-B equipped
- Yes — Mode-S A9790B
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's hard landing, resulting in a runway excursion and substantial damage to the firewall.
Factual narrative
The pilot reported that during landing, the main landing gear touched down first, followed by the nose landing gear. He reported that the nose landing gear tire deflated upon contact with the runway surface. During a telephone conversation with the National Transportation Safety Board investigator, the pilot stated that the main landing gear touched down at airspeed of about 40 knots, and the airplane rolled to the right side of the runway and came to rest about 5 feet from the edge of the runway. The Airframe and Powerplant mechanic that recovered the airplane reported that the nose landing gear wheel was broken in half and damage was sustained to the upper and lower firewall on both the pilot and copilot sides. According to the manufacturer's pilot operating handbook: The stall airspeed for this airplane with flaps down, power off is 49 knots. The pilot reported that there were no mechanical failures or anomalies with any portion of the airplane prior to touch down that would have prevented normal flight operations. The pilot reported that during landing, the main landing gear touched down first, followed by the nose landing gear. He reported that the nose landing gear tire deflated upon contact with the runway surface. During a telephone conversation with the National Transportation Safety Board investigator, the pilot stated that the main landing gear touched down at airspeed of about 40 knots, and the airplane rolled to the right side of the runway and came to rest about 5 feet from the edge of the runway. The Airframe and Powerplant mechanic that recovered the airplane reported that the nose landing gear wheel was broken in half and damage was sustained to the upper and lower firewall on both the pilot and copilot sides. According to the manufacturer's pilot operating handbook: The stall airspeed for this airplane with flaps down, power off is 49 knots. The pilot reported that there were no mechanical failures or anomalies with any portion of the airplane prior to touch down that would have prevented normal flight operations. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Aircraft-Aircraft systems-Landing gear system-Wheel/ski/float-Capability exceeded
Verbatim from NTSB's published report. Source file
NTSB_2016_GAA16CA340.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall, runway excursion). 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.
- 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 …
- SKYbrary (Eurocontrol) 2024 · SKYbrary article Runway Excursion — SKYbrary Knowledge Base
SKYbrary runway excursion review — RE-OE (overruns) + RE-LO (lateral). Risk drivers: long landing, high approach speed, contaminated surface, tailwind, mis-set autobrakes.
- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.