20211003017029A

Accident · Substantial damage

FAA accident report · Kellner Peter T SONERAI II · Minot, ND · October 3, 2021

Date
October 3, 2021 · 14:30 local
Place
Minot, ND
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9115Y
NTSB investigation
NTSBCEN22LA007
Reported as
Kellner Peter T Sonerai II
Reported engine
Volkswagen 2175CC
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
430 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.

Pilot was conducting his initial flight in the experimental aircraft. After initial climb out and making pattern altitude, he noticed high engine temperature. He throttled back and the temperature came down. On his first landing attempt he did not feel that he was as stable as he would like and conducted a go around. On climb out he noticed what appeared to be engine oil begin to appear on the windscreen which obscured his forward visibility. He also noted that the engine temp was high and the engine did not appear to be making as much power as before. He pulled the power back to cruise and leveled off prior to reaching pattern altitude.

Pilot radioed tower and stated that he needed to expediate his landing. Upon landing he felt that things were ok as he approached touchdown, but then several feet above the runway the aircraft stalled and dropped to the runway in a two point stance causing the aircraft to bounce in the air. He then tried to settle back down and bounced again. On the third attempt he believes he pulled back to FAR on the stick causing the tail to hit first. At this point he gave the engine full throttle to try to stabilize and climb out, the aircraft listed right and he was not able to recover. The aircraft contacted the ground and cartwheeled off the runway coming to rest upright on all three wheels. Fuel began to flow between his legs and he quickly unbuckled, opened the canopy and exited the aircraft.

As the FAA filed it

PILOT WAS CONDUCTING HIS INITIAL FLIGHT IN THE EXPERIMENTAL AIRCRAFT. AFTER INITIAL CLIMB OUT AND MAKING PATTERN ALTITUDE, HE NOTICED HIGH ENGINE TEMPERATURE. HE THROTTLED BACK AND THE TEMPERATURE CAME DOWN. ON HIS FIRST LANDING ATTEMPT HE DID NOT FEEL THAT HE WAS AS STABLE AS HE WOULD LIKE AND CONDUCTED A GO AROUND. ON CLIMB OUT HE NOTICED WHAT APPEARED TO BE ENGINE OIL BEGIN TO APPEAR ON THE WINDSCREEN WHICH OBSCURED HIS FORWARD VISIBILITY. HE ALSO NOTED THAT THE ENGINE TEMP WAS HIGH AND THE ENGINE DID NOT APPEAR TO BE MAKING AS MUCH POWER AS BEFORE. HE PULLED THE POWER BACK TO CRUISE AND LEVELED OFF PRIOR TO REACHING PATTERN ALTITUDE.

PILOT RADIOED TOWER AND STATED THAT HE NEEDED TO EXPEDIATE HIS LANDING. UPON LANDING HE FELT THAT THINGS WERE OK AS HE APPROACHED TOUCHDOWN, BUT THEN SEVERAL FEET ABOVE THE RUNWAY THE AIRCRAFT STALLED AND DROPPED TO THE RUNWAY IN A TWO POINT STANCE CAUSING THE AIRCRAFT TO BOUNCE IN THE AIR. HE THEN TRIED TO SETTLE BACK DOWN AND BOUNCED AGAIN. ON THE THIRD ATTEMPT HE BELIEVES HE PULLED BACK TO FAR ON THE STICK CAUSING THE TAIL TO HIT FIRST. AT THIS POINT HE GAVE THE ENGINE FULL THROTTLE TO TRY TO STABILIZE AND CLIMB OUT, THE AIRCRAFT LISTED RIGHT AND HE WAS NOT ABLE TO RECOVER. THE AIRCRAFT CONTACTED THE GROUND AND CARTWHEELED OFF THE RUNWAY COMING TO REST UPRIGHT ON ALL THREE WHEELS. FUEL BEGAN TO FLOW BETWEEN HIS LEGS AND HE QUICKLY UNBUCKLED, OPENED THE CANOPY AND EXITED THE AIRCRAFT.

NTSB investigation

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