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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 ↗.

Related research

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