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Atlas / NTSB / WPR14LA205

NTSB CAROL · Event

Event WPR14LA205

2014-05-13 Nampa, Idaho, United States Airport · MAN None 1 aircraft Status: Completed

Registry · N5281D

FAA Aircraft Registry record.

Make / Model

CESSNA 180A

Year of manufacture

1958 · 56 years old at event

Engine

CONT MOTOR O-470 SERIES (230 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19580118

ADS-B equipped

Yes — Mode-S A6A925

Registrant of record

ROCKY POINTE LOGISTICS LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s failure to maintain directional control during the landing roll, which resulted in a ground loop.

Factual narrative

On May 13, 2014, about 1430 mountain daylight time, a Cessna 180A, N5281D, sustained substantial damage to the left wing during a ground loop at the Nampa Municipal Airport (MAN), Nampa, Idaho. The private pilot and one passenger were not injured. The airplane was owned and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated from MAN at about 1415. The pilot reported that after an uneventful approach to the runway, he landed the tailwheel equipped airplane in a tail low, three-point landing. About 30 feet into the landing roll the airplane suddenly turned sharply to the right and ground looped. Subsequently, the landing gear collapsed and the left wing impacted the ground. Postaccident examination of the tailwheel by a Federal Aviation Administration inspector revealed the tailwheel was heavily worn; however, it castered freely, and no anomalies were noted. The pilot reported that, after an uneventful approach to the runway, he conducted a tail-low, three-point landing in the tailwheel-equipped airplane. About 30 ft into the landing roll, the airplane suddenly turned sharply right and ground looped. Subsequently, the landing gear collapsed, and the left wing impacted the ground. Postaccident examination of the tailwheel revealed that, although it was heavily worn, it castered freely. No evidence of a mechanical malfunction or failure of the tailwheel was found that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or 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-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2014_WPR14LA205.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.