NTSB CAROL · Event
Event NYC04LA169
Registry · N262MC
FAA Aircraft Registry record.
Make / Model
CESSNA 421C
Engine
CONT MOTOR GTSIO-520-L (375 hp)
Seats / Engines
8 seats · 2 engines
Last airworthiness date
20081004
ADS-B equipped
Yes — Mode-S A28781
Registrant of record
AEROSPACE TRUST MANAGEMENT LLC TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's failure to maintain airspeed and his failure to follow the go-around procedure which resulted in a stall.
Factual narrative
On July 17, 2004, about 1315 eastern daylight time, a Cessna 172N, N262MC, was substantially damaged during a go-around at Vansant Airport (9N1), Erwinna, Pennsylvania. The certificated student pilot was seriously injured. Visual meteorological conditions prevailed for the flight that departed Doylestown Airport (DYL), Doylestown, Pennsylvania. No flight plan was filed for the solo instructional flight conducted under 14 CFR Part 91. According to the student pilot's written statement, he originally departed Trenton Mercer Airport (TTN), Trenton, New Jersey. The student pilot flew to Doylestown Airport, and performed three landings. He then flew to Vansant Airport, to practice low approaches and go-arounds. The student pilot did not have a logbook endorsement for Vansant Airport, and did not plan on actually landing there. The student pilot thought he was making approaches to runway 25, a 3,058-foot-long, 120-foot-wide, turf runway. However, he was actually making approaches to runway 7; opposite the flow of traffic. During the third approach, while the airplane was on a short final for runway 7, the student pilot observed another airplane on final approach for runway 25. Fearing a collision, the student pilot banked the airplane left and initiated a climb. During the maneuver, he forgot to increase throttle and partially retract the flaps. The airplane subsequently stalled and descended straight down. The airplane impacted a grass area to the left of runway 7, and came to rest upright. Review a Cessna 172N Information Manual revealed: "BALKED LANDING 1. Throttle -- FULL OPEN. 2. Carburetor Heat -- COLD. 3. Wing Flaps -- 20 degrees (immediately). 4. Climb Speed -- 55 KIAS 5. Wing Flaps -- 10 degrees (until obstacles are cleared). RETRACT (after reaching a safe altitude and 60 KIAS)." The student pilot reported a total flight experience of approximately 161 hours; of which, all were in the same make and model as the accident airplane, and about 42 hours were as solo flight. The reported wind at an airport about 14 miles west of the accident site, at 1320, was from 260 degrees at 5 knots. The student pilot thought he was practicing approaches and go-arounds to runway 25, a 3,058-foot-long, 120-foot-wide, turf runway. However, he was actually making approaches to runway 7; opposite the flow of traffic. During the third approach, while the airplane was on short final for runway 7, the student pilot observed another airplane final approach for runway 25. Fearing a collision, the student pilot banked the airplane left and initiated a climb. During the maneuver, he forgot to increase throttle and partially retract the flaps. The airplane subsequently stalled, descended straight down, and impacted a grass area to the left of the runway. Review of the airplane information manual revealed that a go-around required full engine power and a flap setting of 20 degrees. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_NYC04LA169.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing, stall, 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.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP)
NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
- NASA NTRS 2019 · Other
[Tail Plane Icing]
The Aviation Safety Program initiated by NASA in 1997 has put greater emphasis in safety related research activities. Ice-contaminated-tailplane stall (ICTS) has been identified by the NASA Lewis Icin…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Airport Policing in Pakistan: Structure, Training, and Issue
Airports are strategically and economically important installations of any country. Airports are the gateway of any country and any incidents at these gateways may harm the very aspects of a country i…
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