NYC95LA217
1995-09-02 · QUAKERTOWN, Pennsylvania, United States · None · 1 aircraft · Status: Completed
Airport UKT
Aircraft involved
Probable cause & findings
the pilot's failure to maintain directional control, and the pilot's improper use of the wing flaps, which resulted in an inadvertent stall, and contact with trees. A factor was the crosswind.
Factual narrative
On September 2, 1995, at 1000 eastern daylight time, a Cessna 172, N7154T, struck trees during a go-around, at Quakertown Airport, Quakertown, Pennsylvania. The student pilot was not injured, and the airplane received substantial damage. Visual meteorological conditions prevailed, and no flight plan had been filed for the local, solo training flight, which was conducted under 14 CFR Part 91, and departed at 0900. In the NTSB Accident Report, the pilot stated: ...[I] was about to land for the fifth time. I was coming in on final on 29 and was over the runway waiting for the plane to flare. The winds were gusting at about 8 to 10 knots from the north. I got caught in an updraft. I felt I was too high to land so I decided to go around. I pushed the throttle full forward and began to do so. The correction I made for the wind was not enough to keep me over the runway. Another gust blew me to the left where there is a row of trees separated by about 60 feet of grass. I pulled [retracted] the flaps to try to gain some altitude. Instead of one [notch of] flap, two [notches] came out and made the situation worse blowing me further to the left. I was over the tree tops by then. I pulled up to keep the plane out of the trees and stalled. The plane lost all lift and dove to the ground.... The wing flaps were manually extended by depressing a thumb lock on the end of a bar located between the seats, and pulling up. The degree of movement on the lever controled the amount of flap extension. There were 5 detents which correspond to up, 10 degrees, 20 degrees, 30 degrees, and 40 degrees of flap extension. In a telephone interview, the pilot reported she had extended the flaps to 40 degrees when she initiated the go-around. She attempted to retract the flaps to 30 degrees, however, they were inadvertently retracted to 20 degrees. According to the Airport Facility Directory, runway 29 was 3,201 feet long, 50 feet wide, and had an asphalt surface. THE STUDENT PILOT WAS CONDUCTING TAKEOFF AND LANDING PRACTICE. ON HER FIFTH APPROACH, SHE ENCOUNTERED AN UPDRAFT, AND ADDED POWER TO MAKE A GO-AROUND. THERE WAS A CROSSWIND FROM THE RIGHT WHICH DRIFTED THE AIRPLANE LEFT, OFF THE SIDE OF THE RUNWAY TOWARD TREES. THE WING FLAPS WERE EXTENDED 40 DEGREES, AND WHEN SHE ATTEMPTED TO RETRACT THE FLAPS 10 DEGREES SHE INADVERTENTLY RETRACTED THEM 20 DEGREES. THE AIRPLANE CONTINUED TO DRIFT LEFT, OVER THE TOPS OF TREES AND WHEN SHE PULLED BACK ON THE YOKE TO STAY OUT OF THE TREES, THE AIRPLANE STALLED AND CRASHED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_NYC95LA217.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (stall, go-around). All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
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- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
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