19990205001129A

Accident · Substantial damage

FAA accident report · Amtr EXEC162F · Tucson, AZ · February 5, 1999

Date
February 5, 1999 · 13:43 local
Place
Tucson, AZ
Airport
Ryan Field Airport
Phase of flight
Hovering
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N88XS
NTSB investigation
NTSBLAX99LA089
Reported as
Amtr EXEC162F
Reported engine
AMTRRW ROTWY162
Fatal injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
800 total20 in this make and model20 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.

Experimental rotorway executive helicopter was involved in hover practice when a gust of wind caused the acft to strike the ground hard. Other circumstances are unknown.(.19) on February 5, 1999, at 1345 hours mountain standard time, a stern rotorway exec 162, N88XS, registered to william m. wilson, Tucson, Arizona, encountered a wind gust at the Ryan field, Tucson, the student pilot reported that he had been hovering in the area and was not having any difficulty handling the controls when suddenly he lost control, a skid impacted the ground, and the amateur built experimental helicopter rolled over. The helicopter was substantially damaged, and the student pilot received a minor injury. Visual meteorological conditions prevailed at the time of the solo instructional flight that originated from the airport about 1230. (.4)after flying for about 1 hour, the student pilot hovered 2 feet above ground level about 50 yards away from a witness. The local wind speed had varied between calm and 5 knots during the flight. The witness and pilot reported that suddenly an estimated 25 knot (maximum) wind gust developed. The gust pushed the helicopter sideways, the pilot lost control, a skid contacted the ground, and the helicopter rolled over onto its side. (-23)student pilot was practicing hovering in caml winds when 15 knots wind gust caught pilot off guard. Tv wx info was source of brief.

As the FAA filed it

EXPERIMENTAL ROTORWAY EXECUTIVE HELICOPTER WAS INVOLVED IN HOVER PRACTICE WHEN A GUST OF WIND CAUSED THE ACFT TO STRIKE THE GROUND HARD. OTHER CIRCUMSTANCES ARE UNKNOWN.(.19) ON FEBRUARY 5, 1999, AT 1345 HOURS MOUNTAIN STANDARD TIME, A STERN ROTORWAY EXEC 162, N88XS, REGISTERED TO WILLIAM M. WILSON, TUCSON, ARIZONA, ENCOUNTERED A WIND GUST AT THE RYAN FIELD, TUCSON, THE STUDENT PILOT REPORTED THAT HE HAD BEEN HOVERING IN THE AREA AND WAS NOT HAVING ANY DIFFICULTY HANDLING THE CONTROLS WHEN SUDDENLY HE LOST CONTROL, A SKID IMPACTED THE GROUND, AND THE AMATEUR BUILT EXPERIMENTAL HELICOPTER ROLLED OVER. THE HELICOPTER WAS SUBSTANTIALLY DAMAGED, AND THE STUDENT PILOT RECEIVED A MINOR INJURY. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE SOLO INSTRUCTIONAL FLIGHT THAT ORIGINATED FROM THE AIRPORT ABOUT 1230. (.4)AFTER FLYING FOR ABOUT 1 HOUR, THE STUDENT PILOT HOVERED 2 FEET ABOVE GROUND LEVEL ABOUT 50 YARDS AWAY FROM A WITNESS. THE LOCAL WIND SPEED HAD VARIED BETWEEN CALM AND 5 KNOTS DURING THE FLIGHT. THE WITNESS AND PILOT REPORTED THAT SUDDENLY AN ESTIMATED 25 KNOT (MAXIMUM) WIND GUST DEVELOPED. THE GUST PUSHED THE HELICOPTER SIDEWAYS, THE PILOT LOST CONTROL, A SKID CONTACTED THE GROUND, AND THE HELICOPTER ROLLED OVER ONTO ITS SIDE. (-23)STUDENT PILOT WAS PRACTICING HOVERING IN CAML WINDS WHEN 15 KNOTS WIND GUST CAUGHT PILOT OFF GUARD. TV WX INFO WAS SOURCE OF BRIEF.

NTSB investigation

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