NTSB CAROL · Event
Event CHI96LA004
Registry · N6469P
FAA Aircraft Registry record.
Make / Model
CESSNA 152
Year of manufacture
1981 · 14 years old at event
Engine
LYCOMING 0-235 SERIES (115 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19810326
ADS-B equipped
Yes — Mode-S A87F26
Registrant of record
SUNRISE AVIATION INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's inadequate recovery from a bounced landing. A factor associated with the accident was the quartering tailwind condition and the pilot's selection of the wrong runway on which to land.
Factual narrative
On October 9, 1995, at 1840 eastern daylight time (edt), a Cessna 152II, N6469P, experienced a nose gear collapse following a loss of control while landing at the Big Beaver Airport, Troy, Michigan. The private pilot and passenger were not injured. The airplane was substantially damaged. The 14 CFR Part 91 personal flight was operating in visual meteorological conditions without a flight plan. The local flight originated from the Big Beaver Airport at 1800 edt. The pilot stated he listened to the Pontiac ATIS and called the Big Beaver Unicom for airport advisories prior to making an approach to runway 09. Pontiac ATIS was reporting winds from 220 degrees at 10 knots. He stated that while on final approach with full flaps, he last noticed an airspeed of 60 knots prior to flaring for touchdown. He reported he set up for a slight right crosswind landing, touching down on the right main gear first. The airplane became airborne again and, according to the pilot, he added power to "stabilize" the airplane. The airplane then touched down on both main gear and once again the airplane bounced. When the airplane touched down a third time, the pilot stated, he heard a "sharp crack" then the nose dropped to the runway. The airplane was inspected by a Federal Aviation Administration Inspector who reported that nose gear had collapsed, the firewall was buckled and wrinkles were present in the bulkhead behind the firewall. The landing was being made on runway 09. Winds reported 15 miles from the accident site were from 200 degrees at 10 knots. The pilot stated he made a crosswind landing and twice the airplane touched down and became airborne. On the third touchdown, the nose gear collapsed. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_CHI96LA004.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 (loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation)
ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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