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Atlas / NTSB / FTW95LA121

NTSB CAROL · Event

Event FTW95LA121

1995-02-23 SANTA FE, New Mexico, United States Airport · SAF None 1 aircraft Status: Completed

Registry · N737TC

FAA Aircraft Registry record.

Make / Model

CESSNA 172N

Year of manufacture

1977 · 18 years old at event

Engine

LYCOMING 0-320 SERIES (180 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19771118

ADS-B equipped

Yes — Mode-S A9E6B8

Registrant of record

FLYBOYS NEVADA LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

THE PILOT'S DELAYED LANDING FLARE AND THE IMPROPER BOUNCED LANDING RECOVERY.

Factual narrative

On February 23, 1995, at 1030 mountain standard time, a Cessna 172N, N737TC, was substantially damaged during landing at Santa Fe, New Mexico. The solo student pilot was not injured. Visual meteorological conditions prevailed for the local supervised solo instructional flight. The pilot reported that, while making a planned touch and go landing on runway 20 at the Santa Fe Municipal Airport, she "bounced the landing" and "the plane began to oscillate." Full power was added to go around and the pilot believes that it was at this point the propeller struck the ground. Having accomplished the go-around, the pilot noticed that the yoke was "not responsive" and landed the airplane without further incident. Post-landing inspection by a Federal Aviation Administration inspector revealed deformation of the firewall and the tunnel structure behind the firewall, a bent propeller and nose gear, and damage to the stringers near the main gear box. DURING A TOUCH AND GO LANDING, THE AIRCRAFT BEGAN TO BOUNCE AND OSCILLATE FOLLOWING TOUCHDOWN. THE SOLO STUDENT PILOT APPLIED FULL POWER TO GO AROUND AT WHICH POINT THE PROPELLER STRUCK THE RUNWAY. HAVING ACCOMPLISHED THE GO-AROUND, THE PILOT NOTICED THAT THE YOKE WAS 'NOT RESPONSIVE' AND LANDED THE AIRPLANE WITHOUT FURTHER INCIDENT. POST-LANDING INSPECTION REVEALED DEFORMATION OF THE FIREWALL AND THE TUNNEL STRUCTURE BEHIND THE FIREWALL, A BENT PROPELLER AND NOSE GEAR, AND DAMAGE TO THE STRINGERS NEAR THE MAIN GEAR BOX. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1995_FTW95LA121.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 (go-around). 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 ↗