CEN12LA214
2012-03-29 · Midlothian, Texas, United States · None · 1 aircraft · Status: Completed
Airport KJWY
Current FAA registration · N480SP
- Make / Model
- CESSNA 172S
- Year of manufacture
- 1998 · 14 years old at event
- Engine
- LYCOMING I0360 SER (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19981028
- ADS-B equipped
- Yes — Mode-S A5EA37
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the landing roll.
Factual narrative
On March 29, 2012, at 1715 central daylight time, a Cessna 172S airplane, N480SP, was substantially damaged while landing at Mid-Way Regional Airport (KJWY), Midlothian, Texas. The private pilot was not injured. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 without a flight plan. Day visual meteorological conditions prevailed for the personal flight. The flight departed Sportsman's World Airport (TA65), Palo Pinto, Texas, about 1615 with KJWY as the intended destination. The pilot stated that there was a 5-10 knot left crosswind while landing on runway 18 (6,500 feet by 100 feet, asphalt). He reported that he had no difficulty maintaining runway centerline alignment during the final approach and touchdown. An uneventful touchdown was made on the runway centerline; however, during the landing roll, the airplane began to veer to the left. The pilot stated that despite his increased use of right rudder to regain directional control, the airplane departed off the left side of the runway and impacted a ditch. The nose landing gear collapsed when the airplane impacted the ditch. He further noted that he had not experienced any ground-handling difficulties during the 2 takeoffs and 1 landing completed earlier that day. A postaccident examination was completed by inspectors with the Federal Aviation Administration. The examination revealed substantial damage to the right wing primary structure and engine firewall. Although the nose wheel steering linkages had fractured when the nose gear collapsed, movement of the cockpit rudder pedals confirmed their proper operation. Additionally, no mechanical anomalies were found during a function test of the brake system. The postaccident examination did not reveal any preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. At 1715, the airport's automated surface observing system reported the following weather conditions: wind 120 degrees at 6 knots; visibility 10 miles; scattered clouds at 2,800 and 3,300 feet above ground level; temperature 25 degrees Celsius; dew point 17 degrees Celsius; altimeter setting 29.84 inches of mercury. The pilot stated that there was a 5 to 10 knot left crosswind while landing. He reported that he had no difficulty maintaining the runway centerline alignment during the final approach and touchdown. An uneventful touchdown was made on the runway centerline; however, during the landing roll, the airplane began to veer to the left. The pilot stated that despite his increased use of right rudder to regain directional control, the airplane departed the left side of the runway and impacted a ditch. The nose landing gear collapsed when the airplane impacted the ditch. The pilot further noted that he had not experienced any ground-handling difficulties during the two takeoffs and one landing completed earlier that day. A postaccident examination confirmed that the cockpit rudder pedals were operating properly. Additionally, no mechanical anomalies were revealed during a functional test of the brake system. A postaccident review of available wind data indicated that the accident airplane likely landed in a left quartering crosswind of about 5 knots with no appreciable gusts. In the absence of any significant crosswind or wind gust, and coupled with the lack of any preimpact mechanical malfunctions of the nose wheel steering or brake systems, the pilot should have been able to maintain directional control during the landing roll. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2012_CEN12LA214.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. All research papers
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In most post-WWII cross country air racing events, the “handicap” method of determining race scoring is utilized. A typical example is the Women’s Air Race Classic transcontinental annual competition.…
- Embry-Riddle Scholarly Commons 2015 · Conference paper Approach Stability from FDM Data
The Embry-Riddle Aeronautical University Prescott Campus maintains a fleet of twenty four aircraft, which includes sixteen Cessna 172S NavIII and four Diamond DA42NG equipped with flight data monitori…