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WPR10CA238

2010-05-12 · Corvallis, Oregon, United States · None · 1 aircraft · Status: Completed

Airport CVO

Current FAA registration · N66083

Make / Model
CESSNA 172S
Year of manufacture
2005 · 5 years old at event
Engine
LYCOMING IO-360-L2A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20050926
ADS-B equipped
Yes — Mode-S A8B7C5

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's improper use of the flight and engine controls, resulting in a bounced landing.

Factual narrative

The private pilot receiving instruction reported that during the proficiency training flight, he was seated in the right front seat position while the flight instructor was in the left seat. Following a normal approach for landing, he felt the airplane begin to sink about three to five feet above the runway and attempted to compensate with flight control inputs. The pilot stated that the "automatic (almost subconscious) reaction was to push in the throttle with his right hand and pull back on the yoke with his left hand slightly," which, due to his right seated position, resulted in his right hand pushing the nose down and his left hand pulling back on the throttle thus reducing power. Subsequently, the airplane struck the ground and bounced back into the air. The pilot initiated a go-around followed by the flight instructor taking control of the airplane and landing uneventfully. Post accident examination of the airplane by the pilot and an airframe and power plant mechanic revealed that the engine firewall was structurally damaged. The pilot reported that there were no mechanical anomalies that would have precluded normal operation of the airplane at the time of the accident. The private pilot receiving instruction reported that during the proficiency training flight, he was seated in the right front seat position while the flight instructor was in the left seat. Following a normal approach for landing, he felt the airplane begin to sink about three to five feet above the runway and attempted to compensate with flight control inputs. The pilot stated that the "automatic (almost subconscious) reaction was to push in the throttle with his right hand and pull back on the yoke with his left hand slightly," which, due to his right seated position, resulted in his right hand pushing the nose down and his left hand pulling back on the throttle thus reducing power. Subsequently, the airplane struck the ground and bounced back into the air. The pilot initiated a go-around followed by the flight instructor taking control of the airplane and landing uneventfully. Post accident examination of the airplane by the pilot and an airframe and power plant mechanic revealed that the engine firewall was structurally damaged. The pilot reported that there were no mechanical anomalies that would have precluded normal operation of the airplane at the time of the accident. 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-Landing flare-Incorrect use/operation - C
  • C Personnel issues-Action/decision-Action-Incorrect action selection-Pilot - C
  • C Aircraft-Aircraft systems-Flight control system-(general)-Incorrect use/operation - C
  • C Aircraft-Aircraft power plant-Engine controls-Power lever-Incorrect use/operation - C

Verbatim from NTSB's published report. Source file NTSB_2010_WPR10CA238.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