GAA18CA313
2018-05-30 · Payson, Arizona, United States · None · 1 aircraft · Status: Completed
Airport PAN
Current FAA registration · N780JA
- Make / Model
- CESSNA 172S
- Year of manufacture
- 2007 · 11 years old at event
- Engine
- LYCOMING IO-360-L2A (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20070423
- ADS-B equipped
- Yes — Mode-S AA914F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain yaw control during a short-field takeoff in high-density altitude conditions.
Factual narrative
The pilot reported that, during a short field takeoff, around 100 ft above ground, he saw the primary flight display (PFD) airspeed indicator show 0. He added, the engine appeared to be functioning normal, but he decided to level the airplane and attempt to land on the remaining runway. The airplane then began to turn left and he added right rudder. Subsequently, the airplane touched down on an adjacent taxiway left of the runway and the nose landing gear collapsed. The airplane sustained substantial damage to the left horizontal stabilizer. Postaccident examination videos were provided by a Federal Aviation Administration inspector. The videos showed both the PFD and backup airspeed indicators moving in sync with air applied to the pitot tube. The automated weather observation system at the accident airport reported that, about the time of the accident, the wind was from 190° at 10 knots, gusting to 18 knots, and the calculated density altitude was 7883 ft. The pilot was departing on runway 24. The pilot reported that, during a short-field takeoff, around 100 ft above the ground, he saw the primary flight display (PFD) airspeed indicator showing 0. He added that the engine appeared to be functioning normally, but he decided to level the airplane and attempt to land on the remaining runway. The airplane then began to turn left, and he added right rudder. Subsequently, the airplane touched down on an adjacent taxiway left of the runway, and the nose landing gear collapsed. The airplane sustained substantial damage to the left horizontal stabilizer. Postaccident examination videos were provided by a Federal Aviation Administration inspector. The videos showed both the PFD and backup airspeed indicators moving in sync with air applied to the pitot tube. The automated weather observation system at the airport reported that, about the time of the accident, the wind was from 190° at 10 knots, gusting to 18 knots, and the calculated density altitude was 7,883 ft. The pilot was departing from runway 24. 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-Yaw control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-High density altitude-Effect on equipment
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA18CA313.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 ↗
- NTSB Docket 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.