GAA18CA433
2018-07-22 · Colorado Springs, Colorado, United States · None · 1 aircraft · Status: Completed
Airport FLY
Current FAA registration · N99243
- Make / Model
- CESSNA 172P
- Year of manufacture
- 1985 · 33 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19850603
- ADS-B equipped
- Yes — Mode-S ADDD11
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot’s failure to maintain directional control during landing in gusting crosswind conditions.
Factual narrative
The student pilot reported that, during a check ride, during a short field landing in gusting crosswind conditions, the touchdown was normal, but the airplane quickly veered to the right. He added that, he and the designated pilot examiner applied left rudder to no avail. The airplane exited the runway to the right, the right main landing gear struck a taxiway sign, and the airplane came to rest in the grass adjacent to the taxiway. The airplane sustained substantial damage to the right horizontal stabilizer. The Federal Aviation Administration inspector conducted a postaccident examination. He reported that the rudder system appeared normal and functioned properly. He added that there were no pre-existing mechanical conditions that could have caused the accident. The automated weather observation station located on the airport reported that, about the time of the accident, the wind was from 50° at 11 knots, gusting to 21 knots. The airplane landed on runway 33. The airplane information manual stated that the maximum demonstrated crosswind is 15 knots. The student pilot reported that, during a check ride and a short-field landing in gusting crosswind conditions, the touchdown was normal, but the airplane quickly veered right. He added that he and the designated pilot examiner applied left rudder to no avail. The airplane exited the runway to the right, the right main landing gear struck a taxiway sign, and the airplane came to rest in the grass adjacent to the taxiway. The airplane sustained substantial damage to the right horizontal stabilizer. The Federal Aviation Administration inspector conducted a postaccident examination. He reported that the rudder system appeared normal and functioned properly. He added that there were no pre-existing mechanical conditions that could have caused the accident. The automated weather observation station located on the airport reported that, about the time of the accident, the wind was from 50° at 11 knots, gusting to 21 knots. The airplane landed on runway 33. 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-Student/instructed pilot - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation
- — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Effect on operation
- — Environmental issues-Physical environment-Object/animal/substance-Sign/marker-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA18CA433.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
- NTSB CAROL Agency ↗
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- Embry-Riddle Scholarly Commons 2023 · Conference paper Validation of Training Satisfaction Survey
The Training Satisfaction Survey (TSS) was developed as part of a larger project to examine the features of Virtual Reality software and supporting devices as a training program on visual illusions an…
- Semantic Scholar 2021 · Article (Data in Brief) Cockpit voice recorder transcript data: Capturing safety voice and safety listening during historic aviation accidents
Cockpit Voice Recorder (CVR) transcripts capture audio data within cockpit environments. This aids the investigation of causal factors contributing to aviation accidents by revealing communication and…
- Semantic Scholar 2021 · Article (Safety Science) Safety voice and safety listening during aviation accidents: Cockpit voice recordings reveal that speaking-up to power is not enough
Abstract Safety voice is theorised as an important factor for mitigating accidents, but behavioural research during actual hazards has been scant.