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Atlas / NTSB / CEN21LA082

NTSB CAROL · Event

Event CEN21LA082

2020-12-08 Spearfish, South Dakota, United States Airport · SPF None 1 aircraft Status: Completed

Registry · N2554M

FAA Aircraft Registry record.

Make / Model

PIPER PA-12

Year of manufacture

1946 · 74 years old at event

Engine

LYCOMING 0-235 SERIES (115 hp)

Seats / Engines

3 seats · 1 engine

Last airworthiness date

19570806

ADS-B equipped

Yes — Mode-S A26D01

Registrant of record

LENSEGRAV LESLIE C

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

A total loss of engine power during initial climb for undetermined reasons.

Factual narrative

On December 8, 2020, about 1030 mountain standard time, a Piper PA-12, N2554M, was involved in an accident near Spearfish, South Dakota. The private pilot and a passenger were uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 maintenance test/check flight. After completing an annual inspection, maintenance personnel performed post-inspection engine run-ups, then turned the fuel selector to the OFF position. The pilot arrived at the maintenance facility with a passenger to perform a post-maintenance test/check flight. The pilot stated that the left fuel tank was ½ full and the right fuel tank was ¾ full, and that he positioned the fuel selector to the right fuel tank. Following an engine run-up, he initiated takeoff, and the airplane climbed to about 70 ft above the runway. The airplane lost engine power for a few seconds, regained power for a few more seconds, and then lost total power. The pilot lowered the airplane’s nose to increase airspeed, and the airplane continued to descend. He tried to flare the airplane, but the airplane landed hard on the runway, resulting in substantial damage to the fuselage tubular structure. A postacccident engine run revealed no mechanical anomalies that would have precluded normal operation. Before departing on the first flight after completion of the annual inspection, the pilot selected the right wing fuel tank, which was the fuller tank, performed an engine runup, and then initiated takeoff. The pilot said that the airplane climbed to about 70 ft above the runway, lost engine power for a few seconds, regained power briefly, then lost total power. The airplane landed hard on the runway, resulting in substantial damage to the fuselage. A postacccident engine run revealed no mechanical anomalies that would have precluded normal airplane operation. Based on the available evidence, the reason for the loss of engine power could not be determined. 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).

  • Aircraft-Aircraft power plant-Engine (reciprocating)-(general)-Unknown/Not determined

Verbatim from NTSB's published report. Source file NTSB_2020_CEN21LA082.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗