NTSB CAROL · Event
Event SEA96LA055
Registry · N96879
FAA Aircraft Registry record.
Make / Model
CESSNA 172P
Year of manufacture
1984 · 12 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19831216
ADS-B equipped
Yes — Mode-S AD7D4D
Registrant of record
GC AVIATION SERVICES-1 LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
failure of the pilot to maintain directional control during the landing, which resulted in a ground swerve. A factor relating to the accident was: the rock pile to the left of the runway.
Factual narrative
On February 15, 1996, approximately 1300 mountain standard time, a Cessna 172P, N96879, registered to and operated by Minuteman Aviation of Missoula, Montana, received substantial damage after it departed the runway following a loss of control on landing roll at Lemhi County Airport, Salmon, Idaho. The student pilot, who was on a 14 CFR 91 solo cross-country instructional flight from Missoula, was not injured. Visual meteorological conditions existed and a visual flight rules (VFR) flight plan had been filed. The pilot was landing on runway 17 at Salmon (5,150 by 60 feet, elevation 4,045 feet above sea level.) Winds at the time were calm. The pilot stated: "...I was on a decent approach, full flaps in, on centerline. As I was flaring in ground effect, I noted a slight left yaw. As I tried to correct for this, the right main touched down and I instantly started to jitter. I further tried to correct the problem. The airplane started a pronounced skid off the runway and I attempted an immediate go around, at which time the aircraft somehow flipped on its back side...." The FAA on-scene investigator reported that the airplane came to rest in an inverted position, with its nose pointed west, in an irrigation canal approximately 90 feet to the left of runway 17. Post-accident investigation revealed sidewise flat spots on both main tires. The right main wheel would not turn until the right main brake line was disconnected and fluid released. The right main brake torque plate was bent. Photographs taken at the accident scene showed the bottom of the forward part of the right main wheel fairing partially separated from the remainder of the fairing. The nosewheel was broken off at the fork and was located behind the airplane (with respect to its direction of travel) in a rock pile. The portion of the nose gear strut which remained attached to the aircraft was bent aft and cocked to the right. The left main wheel turned freely and no damage to the left main wheel or wheel fairing was visible in the photographs. The rudder and pedal position were slightly left of center in the photographs; the right rudder pedal was jammed into the firewall, which was shown buckled in this area. The control yokes were rotated about 50 degrees to the left. A control cable continuity check revealed no abnormalities. There was a skid mark on the runway approximately 90 feet long, starting at approximately the midpoint of the runway and arcing from the approximate runway centerline to the left edge of the runway. The aircraft was lying about 120 to 130 feet down the length of the runway from the end of the skid mark. The 1984 Cessna 172P pilot's operating handbook specifies a flaps-down landing airspeed of 60 to 70 knots indicated airspeed (KIAS) for a normal landing. Based on an airspeed of 60 KIAS, a density altitude of 4,000 feet, and no wind, the time for the airplane to travel 90 feet (the approximate length of the skid mark) was calculated to be 0.84 seconds. The straight-line distance from the end of the skid mark (at the left edge of the runway) to the aircraft wreckage was calculated to be approximately 158 feet, based on 90 feet laterally from the runway and 130 feet down the runway. The time for the aircraft to travel 158 feet at 60 KIAS, 4,000 feet density altitude and no wind was calculated to be 1.47 seconds. The angle off the runway centerline from the beginning point of the skid mark to the end point of the skid mark, based on a distance of 30 feet from the runway centerline to the runway edge and an approximate distance of 90 feet from the beginning of the mark to the end of the mark, was calculated to be 19.5 degrees. The student pilot was landing on runway 17 in calm winds. He stated that he 'was on a decent approach, full flaps in, on centerline.' The pilot stated that in the flare, he 'noted a slight left yaw.' The airplane touched down with this left yaw and, according to the pilot, 'started a pronounced skid off the runway.' The pilot stated that although he attempted corrective action, the airplane departed the left edge of the 60-foot wide runway, struck a rock pile with its nosewheel, and nosed over. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_SEA96LA055.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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