20250625017879A

Accident · Destroyed

FAA accident report · Cirrus Design SR22 · Unionville, MO · June 25, 2025

Date
June 25, 2025 · 14:30 local
Place
Unionville, MO
Airport
Unionville Municipal
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N670P
NTSB investigation
NTSBCEN25LA223
Reported as
Cirrus Design SR22
Reported engine
Continental IO-550 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Student
Pilot’s flight hours
45 total11 in this make and model11 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.

Solo student pilot landing after second/final leg of cross country. Aircraft bounced upon

Landing, student initiated go-around. As student applied full power, he also retracted flaps. With aircraft at a high angle of attack, flap retraction increased the stall speed, causing the wing to lose lift from the onset of the stall about to take place. In addition, minimal airflow over tail reduced rudder effectiveness necessary to compensate for the torque and p-factor produced by the engine. Because of those forces acting on the aircraft, the aircraft departed controlled flight to the left only a few feet above the runway and proceeded toward a tree line east of the runway. The downward slope of the terrain allowed the aircraft to maintain a minimal amount of altitude above the ground, but was insufficient for clearing the tree line. Aircraft impacted trees on a southeasterly heading, coming to rest with the wreckage facing a westerly heading.

As the FAA filed it

SOLO STUDENT PILOT LANDING AFTER SECOND/FINAL LEG OF CROSS COUNTRY. AIRCRAFT BOUNCED UPON

LANDING, STUDENT INITIATED GO-AROUND. AS STUDENT APPLIED FULL POWER, HE ALSO RETRACTED FLAPS. WITH AIRCRAFT AT A HIGH ANGLE OF ATTACK, FLAP RETRACTION INCREASED THE STALL SPEED, CAUSING THE WING TO LOSE LIFT FROM THE ONSET OF THE STALL ABOUT TO TAKE PLACE. IN ADDITION, MINIMAL AIRFLOW OVER TAIL REDUCED RUDDER EFFECTIVENESS NECESSARY TO COMPENSATE FOR THE TORQUE AND P-FACTOR PRODUCED BY THE ENGINE. BECAUSE OF THOSE FORCES ACTING ON THE AIRCRAFT, THE AIRCRAFT DEPARTED CONTROLLED FLIGHT TO THE LEFT ONLY A FEW FEET ABOVE THE RUNWAY AND PROCEEDED TOWARD A TREE LINE EAST OF THE RUNWAY. THE DOWNWARD SLOPE OF THE TERRAIN ALLOWED THE AIRCRAFT TO MAINTAIN A MINIMAL AMOUNT OF ALTITUDE ABOVE THE GROUND, BUT WAS INSUFFICIENT FOR CLEARING THE TREE LINE. AIRCRAFT IMPACTED TREES ON A SOUTHEASTERLY HEADING, COMING TO REST WITH THE WRECKAGE FACING A WESTERLY HEADING.

NTSB investigation

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

Other reports on N670P · 1

Matched to the same aircraft by N-number and date.