CEN25LA045
2024-11-18 · Crowley, Louisiana, United States · None · 1 aircraft · Status: Completed
Airport LS09
Current FAA registration · N738PG
- Make / Model
- CESSNA R182
- Year of manufacture
- 1979 · 45 years old at event
- Engine
- LYCOMING 0-540 SERIES (250 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19790309
- ADS-B equipped
- Yes — Mode-S A9EA0F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s un-stabilized landing approach and high airspeed during the approach, that resulted in touchdown with insufficient runway remaining to stop the airplane.
Factual narrative
The pilot reported that he was returning from a pipeline patrol flight and was landing to the south on the north-south oriented grass runway which was wet from recent rain. He said that upon touchdown the airplane “yanked” to the left and began sliding on the wet grass. He could not stop the airplane because of the reduced braking action due to the wet runway. The airplane impacted a hangar located at the south end of the runway and the right wing sustained substantial damage. The operator reported that he had witnessed the accident. He noted that the weather conditions were getting worse and were approaching instrument meteorological conditions. He saw the airplane approach from the north to land to the south on the north-south oriented runway. Initially the airplane was lined up on a field to the east of the runway and he then saw the airplane attempt to turn and line up with the runway. He noted that the airplane appeared lower and faster than normal. After the airplane turned toward the runway, it touched down about halfway down the 2,500 ft. runway and was about 45° from runway alignment. The airplane then started to skid sideways on the wet grass. The airplane tires then regained grip and the airplane darted to the side and impacted the hangar at the south end of the runway. The operator stated that the pilot did not report any problem with the rudder trim system either before or after the accident. Well after the accident, the pilot stated that the rudder trim on the airplane was not operating correctly, and the skid-slip ball was not centered during the flight. He said the rudder trim wheel had no tension. He reported no other mechanical issues with the airplane. The pilot’s report of the rudder trim system issues was not provided until after the airplane was no longer available for examination of the rudder trim system. Regardless, the rudder trim should not have inhibited the pilot from maintaining directional control of the airplane while landing on the wet runway. The reported weather conditions at a nearby airport included a broken ceiling of 700 ft. above ground level (agl), an overcast ceiling at 1,300 ft. agl, and 7 miles visibility. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Descent/approach/glide path-Not attained/maintained
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Environmental issues-Physical environment-Runway/land/takeoff/taxi surface-Wet surface-Effect on operation
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2024_CEN25LA045.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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