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GAA17CA341

2017-06-14 · Galena, Idaho, United States · None · 1 aircraft · Status: Completed

Airport U87

Current FAA registration · N9912Q

Make / Model
CESSNA 172M
Year of manufacture
1975 · 42 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19750911
ADS-B equipped
Yes — Mode-S ADD907

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's exceedance of the airplane’s critical angle of attack, which resulted in a power-on stall and subsequent loss of airplane control.

Factual narrative

The pilot in the airplane reported that he attempted to perform a crosswind, soft-field take off from a dry turf airstrip. The pilot configured the airplane with full throttle application, flaps 10°, and a nose high attitude until the stall warning horn sounded. He then relaxed pressure on the yoke until the stall warning horn subsided. Shortly after rotation the airplane entered a power-on stall and the pilot lost directional control of the airplane. The airplane impacted a barbed wire fence and sustained substantial damage to the right wing strut. Per the National Transportation Safety Board Pilot Aircraft Accident Report, the pilot reported that the accident could have been prevented, if he had received instruction from a Federal Aviation Administration Certificated Flight Instructor that was specific to the accident airplane, specifically for a soft-field takeoff because each individual aircraft has nuances that can affect the operation. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot reported that he was attempting to perform a crosswind, soft-field takeoff from a dry, turf airstrip. He set the flaps to 10°, and the airplane was in a nose-high attitude until the stall warning horn sounded. He then relaxed pressure on the yoke until the stall warning horn stopped. Shortly after liftoff, the airplane entered a power-on stall, and the pilot lost airplane control, and the airplane then began to descend to the runway. The airplane subsequently departed the runway and impacted a barbed wire fence. The airplane sustained substantial damage to the right wing strut. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane 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-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • — Environmental issues-Physical environment-Object/animal/substance-Fence/fence post-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2017_GAA17CA341.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 (stall). All research papers