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CEN12CA510

2012-08-01 · Oshkosh, Wisconsin, United States · None · 1 aircraft · Status: Completed

Airport OSH

Current FAA registration · N462TR

Make / Model
CESSNA 172S
Year of manufacture
2003 · 9 years old at event
Engine
LYCOMING IO-360-L2A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20031030
ADS-B equipped
Yes — Mode-S A5A2C2

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The flight instructor’s loss of directional control during landing, which resulted in a collision with a runway light.

Factual narrative

The airplane was on final approach to land after the completion of a local night instructional flight. The flight instructor was to demonstrate the proper pitch attitude and sight picture needed for a landing at night. On short final, just before touchdown, the airplane drifted off of the runway center line to the left. Upon touchdown the airplane was still moving toward the left side of the runway. The instructor pilot stated that with the low energy state of the airplane there was not enough room to perform a go around safely. The airplane then exited the runway as flight control inputs were applied to correct back to centerline. Upon exiting the runway, the airplane impacted a runway light on the lower portion of the right wing strut attach point, resulting in structural damage to the strut. The instructor pilot reported that the accident could have been prevented if positive control was maintained during the landing phase of the flight. The airplane was on final approach to land after the completion of a local night instructional flight. The flight instructor was to demonstrate the proper pitch attitude and sight picture needed for a landing at night. On short final, just before touchdown, the airplane drifted off of the runway centerline to the left. Upon touchdown the airplane was still moving toward the left side of the runway. The instructor stated that with the low energy state of the airplane there was not enough room to perform a go-around safely. The airplane then exited the runway as he applied flight control inputs to correct back to the centerline. Upon exiting the runway, the airplane impacted a runway light on the lower portion of the right wing strut attach point, resulting in structural damage to the strut. The instructor reported that the accident could have been prevented if positive control was maintained during the landing phase of the flight. 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-Directional control-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • — Environmental issues-Physical environment-Object/animal/substance-Runway/taxi/approach light-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2012_CEN12CA510.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 (go-around). All research papers