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Atlas / NTSB / DEN07CA023

NTSB CAROL · Event

Event DEN07CA023

2006-11-13 Santa Fe, New Mexico, United States Airport · SAF None 1 aircraft Status: Completed

Registry · N87VF

FAA Aircraft Registry record.

Make / Model

AMERICAN CHAMPION AIRCRAFT 7GCBC

Year of manufacture

2007

Engine

SUPERIOR O-360 SERIES (180 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

20070630

ADS-B equipped

Yes — Mode-S ABF5DE

Registrant of record

AGRI FLITE INC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the pilot's failure to maintain directional control during the landing roll, and his failure to maintain airspeed which resulted in a stall and hard landing.

Factual narrative

On November 13, 2006, at 0938 mountain standard time, an American Champion 7GCBC, N87VF, piloted by a commercial pilot, was substantially damaged when it landed hard during an attempted an aborted landing at Santa Fe Municipal Airport (SAF), Santa Fe, New Mexico. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The pilot and passenger on board the airplane were not injured. The local flight originated from Santa Fe approximately 0700. The pilot said he made a normal wheel landing and allowed the tail to settle. When the tail wheel touched the runway, the airplane veered sharply to the left. The pilot applied full right rudder but the airplane did not respond. The airplane departed the left side of the runway and the pilot applied full power in an attempt to abort the landing. The airplane lifted off briefly, then "settled back on the runway, impacted, and spun around." The FAA inspector who went to the scene said his investigation revealed that during the landing abort, the airplane lifted off, stalled, and landed hard. Post-accident inspection revealed the left wing spar was bent, and a rib was broken, the left elevator and rudder were bent, the empennage was twisted, and the left main landing gear was torn off. Flight control continuity was established, and no system anomalies were found. The pilot made a normal wheel landing and allowed the tail to settle. When the tail wheel touched the runway, the airplane veered sharply to the left. The pilot applied full right rudder but the airplane did not respond. The airplane departed the left side of the runway and the pilot applied full power in an attempt to abort the landing. The airplane lifted off, stalled, and landed hard. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2006_DEN07CA023.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 (stall). 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 ↗