NTSB CAROL · Event
Event NYC96LA136
Registry · N4776E
FAA Aircraft Registry record.
Make / Model
CESSNA 172N
Year of manufacture
1978 · 18 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19790126
ADS-B equipped
Yes — Mode-S A5DE4A
Registrant of record
ALPHA ONE AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
failure of the pilot to identify the inoperative airspeed indication and abort the takeoff, while there was sufficient runway remaining; excessive speed during the approach/landing; and the pilot's failure to perform a go-around after not attaining a proper touchdown point during the landing. A factor relating to the accident was: the blocked pitot tube, which resulted in an inoperative airspeed indicator.
Factual narrative
On June 28, 1996, about 1150 eastern daylight time, a Cessna 172N, N4776E, was substantially damaged when it overran the runway during the landing at the Blue Knob Valley Airport, Newry, Pennsylvania. The private pilot and passenger were not injured. Visual meteorological conditions prevailed for the local flight. No flight plan was filed for the personal flight conducted under 14 CFR Part 91. The pilot stated, in the NTSB form 6120.1/2: "My son and I arrived at the airport and I preflighted the airplane. We taxied to the run-up area for runway 29. I "ran-up" the engine, checked the gauges and set the flight instruments and radio. We cleared for take off and during the take-off roll, I noticed the airspeed was not working properly. It bounced a few times and then quit. By this time I was too far down the runway to abort the takeoff. I took off and we flew locally for 1.2 hours. We flew back to the airport to land. I was concerned about coming in too slow and stalling out. I use 10 [degrees] flaps for a final but was too high and fast to touch down. I made a go around and used 20 [degrees] flaps for final. I touched down about 1/3 to 1/2 down the runway, applied full brakes but was still going too fast and ran off the end of the runway." Examination of the wreckage by a Federal Aviation Administration Inspector revealed sediment clogged the pitot tube. According to the Airport Facility Directory, runway 29 was a 3,415 foot long, 92 foot wide, dirt runway with no obstructions. The weather at a nearby airport was reported as ceiling 3,500 broken; visibility 12 miles; temperature 80 degrees F; dewpoint 60 degrees F; altimeter 30.20" Hg; wind from 330 degrees at 7 knots. According to the Cessna 172 Pilot Operating Handbook, for the above conditions, the takeoff and landing distances were approximately 1,300 and 900 feet respectively. During the takeoff roll, the pilot observed that the airspeed indicator was inoperative. However, he said that by the time he realized the problem, the airplane was too far down the runway to abort the takeoff. He continued the takeoff and flew about 1.2 hours before returning to landing. The airplane was high and fast during the first approach to land, and the pilot decided to go-around. After the second approach, the airplane touched down about half way down the 3,415 foot long runway. The pilot stated that he applied full brakes; however, the airplane was too fast and continued off the departure end of the runway. Subsequently, it encountered rough terrain and was damaged. Examination of the airplane revealed that the pitot tube was blocked with a sediment. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_NYC96LA136.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 (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.
- 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
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
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