CEN11CA496
2011-07-20 · Battle Creek, Michigan, United States · None · 1 aircraft · Status: Completed
Airport BTL
Current FAA registration · N93TA
- Make / Model
- CIRRUS DESIGN SR20
- Year of manufacture
- 2006 · 5 years old at event
- Engine
- CONT MOTOR IO-360-ES (210 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20060710
- ADS-B equipped
- Yes — Mode-S ACE4FA
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's improper flare which resulted in a hard landing.
Factual narrative
The student pilot executed a go-around after the airplane's descent angle for the approach was too high. He then attempted another approach with a lower descent angle but at a somewhat faster approach speed with idle engine power. During the landing attempt, the airplane experienced a hard landing in a flat attitude and bounced twice before the pilot applied full engine power and retracted flaps from 100 percent to 50 percent. The airplane then veered off the left side of the runway and impacted terrain and a fence. The airplane sustained substantial damage to the empennage and wing. The student pilot executed a go-around after the airplane's pitch angle for the approach was too high. He then attempted another approach with a lower angle but at a somewhat faster approach speed with idle engine power. During the landing attempt, the airplane landed hard, bounced twice before the student pilot applied full engine power and retracted flaps from 100 percent to 50 percent in order to execute a go-around. The airplane then veered off the left side of the runway and impacted terrain and a fence. The airplane sustained substantial damage to the empennage and wing. The pilot student reported no mechanical anomalies that would have precluded normal operation. 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-Incorrect use/operation - C
Verbatim from NTSB's published report. Source file
NTSB_2011_CEN11CA496.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
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Related research
Matched on aircraft type or causal vocabulary (go-around). All research papers
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- Semantic Scholar 2022 · Article (Journal of Safety Research) Go-around accidents and general aviation safety.
INTRODUCTION Changes in General Aviation (GA) accident rates, specifically in the go-around phase, are examined by comparing the number of accidents, the proportion of fatal accidents, and the proport…
- Semantic Scholar 2021 · Article (Aerospace) Classification and Analysis of Go-Arounds in Commercial Aviation Using ADS-B Data
Go-arounds are a necessary aspect of commercial aviation and are conducted after a landing attempt has been aborted. It is necessary to conduct go-arounds in the safest possible manner, as go-arounds …
- NASA NTRS 2021 · Accepted Manuscript (Version with final changes) Go-Around Criteria Refinement for Transport Category Aircraft
Presently, airline pilots are trained to go around if, when lower than 500 ft above the ground, they are outside of a handful of parameters such as airspeed, position, and rate of descent.
- NASA NTRS 2019 · Conference Paper Validation of Proposed Go-Around Criteria Under Various Environmental Conditions
This paper evaluates the effects of environmental conditions on touchdown performance under varying approach states and validates proposed go-around criteria developed using data from a previously con…