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GAA17CA382

2017-06-28 · Alamogordo, New Mexico, United States · None · 1 aircraft · Status: Completed

Airport ALM

Current FAA registration · N2774D

Make / Model
CESSNA 170B
Year of manufacture
1952 · 65 years old at event
Engine
CONT MOTOR C145 SERIES (145 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19551111
ADS-B equipped
Yes — Mode-S A2C365

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot receiving instruction’s failure to maintain directional control during the landing roll and the flight instructor’s delayed remedial action, which resulted in a ground loop.

Factual narrative

The flight instructor in the tailwheel-equipped airplane reported that the pilot flying was receiving instruction for a tailwheel endorsement. He added that, during the 7th landing of the day, the pilot extended the downwind to allow for traffic that landed ahead of them. He further added that, during the wheel landing touchdown, as the tail was settling to the ground, a wind gust "turned the airplane's tail," which resulted in a ground loop on the runway. The left wing, engine mounts, and windscreen sustained substantial damage. The flight instructor and pilot receiving instruction reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. An automated weather observation station, at the accident airport, recorded wind from 240° at 6 knots. The flight instructor reported that the landing was on runway 22. The flight instructor in the tailwheel-equipped airplane reported that the pilot flying was receiving instruction for a tailwheel endorsement. He added that, during the seventh landing of the day, the pilot extended the downwind to allow for traffic that landed ahead of them. He further added that, during the wheel landing touchdown, as the tail was settling to the ground, a wind gust "turned the airplane's tail," which resulted in a ground loop on the runway. The left wing, engine mounts, and windscreen sustained substantial damage. The flight instructor and pilot receiving instruction reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. An automated weather observation station at the accident airport recorded wind from 240° at 6 knots. The flight instructor reported that the landing was on runway 22. 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
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Instructor/check pilot - C
  • C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C

Verbatim from NTSB's published report. Source file NTSB_2017_GAA17CA382.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

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