20251231020299I

Incident · No damage

FAA incident report · Piper PA-28R-200 · Hot Springs, AR · December 31, 2025

Date
December 31, 2025 · 12:15 local
Place
Hot Springs, AR
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N15744
Reported as
Piper PA-28R-200
Reported engine
Lycoming I0360 series
People aboard
4
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
265 total

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On December 31, 2025, the pilot of a PA-28 privacy data omitted experienced engine roughness and a partial loss of power while adjusting the mixture during approach to Hot Springs. The pilot reported the power loss to ATC and stated the intention to conduct an off-airport landing. The aircraft landed safely and without injury on a highway on the outskirts of Hot Springs.

On January 2, 2026, FAA inspectors arrived on scene, examined the aircraft, and interviewed the pilot. The examination revealed that the mixture control cable end fitting had become detached from the fuel control. The retaining nut securing the cable end fitting to the fuel control arm was missing, which allowed the mixture control to move freely and prevented positive control of fuel metering from the cockpit. The loss of effective mixture control resulted in engine roughness and reduced power.

As the FAA filed it

ON DECEMBER 31, 2025, THE PILOT OF A PA-28 ^PRIVACY DATA OMITTED^ EXPERIENCED ENGINE ROUGHNESS AND A PARTIAL LOSS OF POWER WHILE ADJUSTING THE MIXTURE DURING APPROACH TO HOT SPRINGS. THE PILOT REPORTED THE POWER LOSS TO ATC AND STATED THE INTENTION TO CONDUCT AN OFF-AIRPORT LANDING. THE AIRCRAFT LANDED SAFELY AND WITHOUT INJURY ON A HIGHWAY ON THE OUTSKIRTS OF HOT SPRINGS.

ON JANUARY 2, 2026, FAA INSPECTORS ARRIVED ON SCENE, EXAMINED THE AIRCRAFT, AND INTERVIEWED THE PILOT. THE EXAMINATION REVEALED THAT THE MIXTURE CONTROL CABLE END FITTING HAD BECOME DETACHED FROM THE FUEL CONTROL. THE RETAINING NUT SECURING THE CABLE END FITTING TO THE FUEL CONTROL ARM WAS MISSING, WHICH ALLOWED THE MIXTURE CONTROL TO MOVE FREELY AND PREVENTED POSITIVE CONTROL OF FUEL METERING FROM THE COCKPIT. THE LOSS OF EFFECTIVE MIXTURE CONTROL RESULTED IN ENGINE ROUGHNESS AND REDUCED POWER.