Skip to content

GAA16CA523

2016-09-16 · Tooele, Utah, United States · None · 1 aircraft · Status: Completed

Airport TVY

Current FAA registration · N461SP

Make / Model
CESSNA 172S
Year of manufacture
2000 · 16 years old at event
Engine
LYCOMING I0360 SER A&C (200 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20000118
ADS-B equipped
Yes — Mode-S A59EF0

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's improper landing flare, which resulted in a hard, bounced landing.

Factual narrative

The student pilot reported that the airplane landed hard and bounced and that she then pulled the yoke to the farthest aft position. She further reported that the airplane porpoised and that she applied the brakes; however, she "could not press the right brake fully". Subsequently ,the airplane veered to the left side of the runway. A postaccident examination by a local mechanic revealed substantial damage to the yoke, which was broken at the lower attach point. Further, the rudder bearing cap on the pilot side inboard was damaged, the rudder springs were damaged and disconnected at the tunnel, and the floorboards and firewall were buckled and creased. The student pilot reported that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The student pilot reported that the airplane landed hard and bounced and that she then pulled the yoke to the farthest aft position. She further reported that the airplane porpoised and that she applied the brakes; however, she "could not press the right brake fully". Subsequently, the airplane veered to the left side of the runway. A postaccident examination by a local mechanic revealed substantial damage to the yoke, which was broken at the lower attach point. Further, the rudder bearing cap on the pilot side inboard was damaged, the rudder springs were damaged and disconnected at the tunnel, and the floorboards and firewall were buckled and creased. The student pilot reported that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained - C

Verbatim from NTSB's published report. Source file NTSB_2016_GAA16CA523.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type. All research papers