20260530009049A

Accident · Substantial damage

FAA accident report · Piper PA-28-235 · Montevideo, MN · May 30, 2026

Date
May 30, 2026 · 19:30 local
Place
Montevideo, MN
Airport
Montevideo-Chippewa County
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N15291
Reported as
Piper PA-28-235
Reported engine
Lycoming 0-540 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Private pilot
Pilot’s flight hours
453 total48 in this make and model5 in the last 90 days

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 may 30, 2026, the aircraft experienced a rough running engine on approach after conducting a local flight for approximately an hour and a half. After applying carburetor heat, the engine lost all power. The aircraft was unable to make the runway and landed short, impacting terrain and causing substantial damage to the wing when the gear came up through the wing structure. Suspected cause of power loss is improper timing of the application of carburetor heat, causing a total loss of power with inadequate time for recovery

As the FAA filed it

ON MAY 30, 2026, THE AIRCRAFT EXPERIENCED A ROUGH RUNNING ENGINE ON APPROACH AFTER CONDUCTING A LOCAL FLIGHT FOR APPROXIMATELY AN HOUR AND A HALF. AFTER APPLYING CARBURETOR HEAT, THE ENGINE LOST ALL POWER. THE AIRCRAFT WAS UNABLE TO MAKE THE RUNWAY AND LANDED SHORT, IMPACTING TERRAIN AND CAUSING SUBSTANTIAL DAMAGE TO THE WING WHEN THE GEAR CAME UP THROUGH THE WING STRUCTURE. SUSPECTED CAUSE OF POWER LOSS IS IMPROPER TIMING OF THE APPLICATION OF CARBURETOR HEAT, CAUSING A TOTAL LOSS OF POWER WITH INADEQUATE TIME FOR RECOVERY