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ERA11CA236

2011-04-10 · Millville, New Jersey, United States · None · 1 aircraft · Status: Completed

Airport MIV

Current FAA registration · N6338F

Make / Model
CESSNA 172N
Year of manufacture
1979 · 32 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19790830
ADS-B equipped
Yes — Mode-S A84C57

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s improper recovery from a bounced landing which resulted in a loss of aircraft control during the go-around.

Factual narrative

The pilot-in-command, along with two other pilot-rated passengers, was practicing a no flap landing. The pilot in command began to flare the airplane about half-way down the runway, bounced, and then pitched the airplane up. The airplane drifted to the left, while the tail tie-down contacted the runway. The pilot-rated passenger in the right front seat took control of the airplane, lowered the pitch, and added full power in an attempt to go around. As the airplane climbed, it continued to the left, and the left horizontal stabilizer impacted an airport sign, separating the left elevator from the airplane. The pilot-rated passenger in the right seat continued the climb and returned to land uneventfully. The left horizontal stabilizer, left elevator, and rudder were substantially damaged during the accident sequence. The pilot-in-command reported there were no mechanical anomalies with the airplane. The pilot was on a flight with two other pilot-rated passengers, practicing a no flap landing. He flared the airplane about half-way down the runway, it bounced, and then pitched up, drifted to the left, and the tail tie-down contacted the runway. The pilot relinquished the controls, and the pilot-rated passenger in the right front seat took control of the airplane. He lowered the pitch, and added full power to perform a go around. During the go-around, as the airplane climbed, it continued to the left, and the left horizontal stabilizer impacted an airport sign, separating the left elevator from the airplane. The pilot-rated passenger continued the climb and landed uneventfully. The left horizontal stabilizer, left elevator, and rudder were substantially damaged during the accident sequence. The pilot reported there were no mechanical anomalies with the airplane. 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
  • F Personnel issues-Psychological-Personality/attitude-Motivation/respond to pressure-Pilot - F
  • C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2011_ERA11CA236.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 (icing, go-around). All research papers