20250711009139A

Accident · Substantial damage

FAA accident report · Pipistrel Italia S R L Alpha Trainer · Hurricane, UT · July 11, 2025

Date
July 11, 2025 · 10:50 local
Place
Hurricane, UT
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N209ZM
NTSB investigation
NTSBWPR25LA209
Reported as
Pipistrel Italia S R L Alpha Trainer
Reported engine
ROTAX 912UL series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
274 total125 in this make and model43 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 July 11, 2025, privacy data omitted departed 1L8 with an intended destination of gcn for a touch and go and a return flight to 1L8. An IMC flight plan was filed to allow the passenger (a certificated pilot) to train for their instrument rating. The flight to gcn went uneventfully and during the last 30 minutes of the return flight, the PIC named in the report assumed control of the aircraft. At ~15 nautical miles from the intended destination, the PIC began to perform several commercial maneuvers. During the second maneuver, the PIC entered a turn with an aggressive initial bank angle while under reduced power. This caused the aircraft’s nose to dip and the aircraft to rapidly increase airspeed. Airspeed indications were noted as being 140 knots which exceeded the allowable vne of 135 knots. The PIC was able to recover by pulling back on the controls and reducing the throttle to idle; however, at some point during this transition the aircraft began to experience aerodynamic buffeting and the left flaperon departed the aircraft. The PIC did not experience significant change in aircraft flight characteristics after that maneuver and decided to continue to 1L8 where the aircraft landed uneventfully. A post damage assessment identified that all but four feet of the left flaperon was missing and that there was an ~one foot tear in the composite skin on the underside of the left wing root. A 44709 re-examination and counselling are being recommended and this investigation is being closed with no further action required at this time.

As the FAA filed it

ON JULY 11, 2025, ^PRIVACY DATA OMITTED^ DEPARTED 1L8 WITH AN INTENDED DESTINATION OF GCN FOR A TOUCH AND GO AND A RETURN FLIGHT TO 1L8. AN IMC FLIGHT PLAN WAS FILED TO ALLOW THE PASSENGER (A CERTIFICATED PILOT) TO TRAIN FOR THEIR INSTRUMENT RATING. THE FLIGHT TO GCN WENT UNEVENTFULLY AND DURING THE LAST 30 MINUTES OF THE RETURN FLIGHT, THE PIC NAMED IN THE REPORT ASSUMED CONTROL OF THE AIRCRAFT. AT ~15 NAUTICAL MILES FROM THE INTENDED DESTINATION, THE PIC BEGAN TO PERFORM SEVERAL COMMERCIAL MANEUVERS. DURING THE SECOND MANEUVER, THE PIC ENTERED A TURN WITH AN AGGRESSIVE INITIAL BANK ANGLE WHILE UNDER REDUCED POWER. THIS CAUSED THE AIRCRAFT’S NOSE TO DIP AND THE AIRCRAFT TO RAPIDLY INCREASE AIRSPEED. AIRSPEED INDICATIONS WERE NOTED AS BEING 140 KNOTS WHICH EXCEEDED THE ALLOWABLE VNE OF 135 KNOTS. THE PIC WAS ABLE TO RECOVER BY PULLING BACK ON THE CONTROLS AND REDUCING THE THROTTLE TO IDLE; HOWEVER, AT SOME POINT DURING THIS TRANSITION THE AIRCRAFT BEGAN TO EXPERIENCE AERODYNAMIC BUFFETING AND THE LEFT FLAPERON DEPARTED THE AIRCRAFT. THE PIC DID NOT EXPERIENCE SIGNIFICANT CHANGE IN AIRCRAFT FLIGHT CHARACTERISTICS AFTER THAT MANEUVER AND DECIDED TO CONTINUE TO 1L8 WHERE THE AIRCRAFT LANDED UNEVENTFULLY. A POST DAMAGE ASSESSMENT IDENTIFIED THAT ALL BUT FOUR FEET OF THE LEFT FLAPERON WAS MISSING AND THAT THERE WAS AN ~ONE FOOT TEAR IN THE COMPOSITE SKIN ON THE UNDERSIDE OF THE LEFT WING ROOT. A 44709 RE-EXAMINATION AND COUNSELLING ARE BEING RECOMMENDED AND THIS INVESTIGATION IS BEING CLOSED WITH NO FURTHER ACTION REQUIRED AT THIS TIME.

NTSB investigation

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