20260417003909A

Accident · Destroyed

FAA accident report · Cirrus Design SR22 · Santa Fe, NM · April 17, 2026

Date
April 17, 2026 · 08:30 local
Place
Santa Fe, NM
Airport
Santa Fe Regional
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N654MC
NTSB investigation
NTSBWPR26LA162
Reported as
Cirrus Design SR22
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
735 total33 in this make and model

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 April 17, 2026, at about 0954 mountain standard time, a Cirrus Design Corp SR22,

Sustained substantial damage when it was involved in an accident near la cienega, new

Mexico. The pilot receiving instruction and the flight instructor were not injured. The airplane

Was operating as a title 14 code of federal regulations part 91 instructional flight.

The pilot receiving instruction reported that during the preflight inspection, no issues were

Found, and the airplane was filled with approximately 90 gallons of fuel. During the takeoff and

Initial climb, the flight instructor noticed that the engine was not producing maximum power.

He confirmed that the throttle was set to full forward and the mixture was adjusted to full rich.

At approximately 500 ft above ground level (AGL), while the pilot receiving instruction initiated a

Left turn to follow the instrument departure procedure, when the engine lost total power. The

Flight instructor took control of the airplane, leveled the wings, and deployed the Cirrus

Airframe parachute system (caps). Subsequently, the airplane descended under the

Parachute canopy and landed in a residential area near several homes.

Examination of the airplane revealed that the fuselage, wings, and empennage sustained

Substantial damage. The wreckage was recovered to a secure location for further examination

As the FAA filed it

ON APRIL 17, 2026, AT ABOUT 0954 MOUNTAIN STANDARD TIME, A CIRRUS DESIGN CORP SR22,

SUSTAINED SUBSTANTIAL DAMAGE WHEN IT WAS INVOLVED IN AN ACCIDENT NEAR LA CIENEGA, NEW

MEXICO. THE PILOT RECEIVING INSTRUCTION AND THE FLIGHT INSTRUCTOR WERE NOT INJURED. THE AIRPLANE

WAS OPERATING AS A TITLE 14 CODE OF FEDERAL REGULATIONS PART 91 INSTRUCTIONAL FLIGHT.

THE PILOT RECEIVING INSTRUCTION REPORTED THAT DURING THE PREFLIGHT INSPECTION, NO ISSUES WERE

FOUND, AND THE AIRPLANE WAS FILLED WITH APPROXIMATELY 90 GALLONS OF FUEL. DURING THE TAKEOFF AND

INITIAL CLIMB, THE FLIGHT INSTRUCTOR NOTICED THAT THE ENGINE WAS NOT PRODUCING MAXIMUM POWER.

HE CONFIRMED THAT THE THROTTLE WAS SET TO FULL FORWARD AND THE MIXTURE WAS ADJUSTED TO FULL RICH.

AT APPROXIMATELY 500 FT ABOVE GROUND LEVEL (AGL), WHILE THE PILOT RECEIVING INSTRUCTION INITIATED A

LEFT TURN TO FOLLOW THE INSTRUMENT DEPARTURE PROCEDURE, WHEN THE ENGINE LOST TOTAL POWER. THE

FLIGHT INSTRUCTOR TOOK CONTROL OF THE AIRPLANE, LEVELED THE WINGS, AND DEPLOYED THE CIRRUS

AIRFRAME PARACHUTE SYSTEM (CAPS). SUBSEQUENTLY, THE AIRPLANE DESCENDED UNDER THE

PARACHUTE CANOPY AND LANDED IN A RESIDENTIAL AREA NEAR SEVERAL HOMES.

EXAMINATION OF THE AIRPLANE REVEALED THAT THE FUSELAGE, WINGS, AND EMPENNAGE SUSTAINED

SUBSTANTIAL DAMAGE. THE WRECKAGE WAS RECOVERED TO A SECURE LOCATION FOR FURTHER EXAMINATION

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.