20190618007489A

Accident · Substantial damage

FAA accident report · William S Harten CAVALON · Nephi, UT · June 18, 2019

Date
June 18, 2019 · 20:20 local
Place
Nephi, UT
Airport
Nephi Municipal
Phase of flight
Unknown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N882M
NTSB investigation
NTSBGAA19CA359
Reported as
William S Harten Cavalon
Reported engine
ROTAX 915IS
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Private pilot
Pilot’s flight hours
227 total82 in this make and model7 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.

After several hours of delays, the pilot was confident that the aircraft was ready for its first test flight with him at the controls. The pilot had never flown this type of gyroplane equipped with the Rotax 915 is engine before, and was surprised by the amount of yaw produced by the extra 35% of power. The aircraft entered a sideslip, which was erroneously identified by the pilot as a flight control malfunction. The aircraft climbed to about 50 feet AGL at about 50 knots groundspeed with a significant (30+ degree) sideslip angle, and then settled back toward the ground. The pilot aimed the gyroplane away from hard surfaces, and the aircraft impacted terrain, resulting in damage to the aircraft and lacerations to the pilots head.

As the FAA filed it

AFTER SEVERAL HOURS OF DELAYS, THE PILOT WAS CONFIDENT THAT THE AIRCRAFT WAS READY FOR ITS FIRST TEST FLIGHT WITH HIM AT THE CONTROLS. THE PILOT HAD NEVER FLOWN THIS TYPE OF GYROPLANE EQUIPPED WITH THE ROTAX 915 IS ENGINE BEFORE, AND WAS SURPRISED BY THE AMOUNT OF YAW PRODUCED BY THE EXTRA 35% OF POWER. THE AIRCRAFT ENTERED A SIDESLIP, WHICH WAS ERRONEOUSLY IDENTIFIED BY THE PILOT AS A FLIGHT CONTROL MALFUNCTION. THE AIRCRAFT CLIMBED TO ABOUT 50 FEET AGL AT ABOUT 50 KNOTS GROUNDSPEED WITH A SIGNIFICANT (30+ DEGREE) SIDESLIP ANGLE, AND THEN SETTLED BACK TOWARD THE GROUND. THE PILOT AIMED THE GYROPLANE AWAY FROM HARD SURFACES, AND THE AIRCRAFT IMPACTED TERRAIN, RESULTING IN DAMAGE TO THE AIRCRAFT AND LACERATIONS TO THE PILOTS HEAD.

NTSB investigation

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