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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 ↗.

Related research

Matched on aircraft type or causal vocabulary (stall, runway excursion). All research papers