19980510008829A

Accident · Substantial damage

FAA accident report · Univar 108-1 · Salt Lake City, UT · May 10, 1998

Date
May 10, 1998 · 14:50 local
Place
Salt Lake City, UT
Airport
Salt Lake City Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8178K
NTSB investigation
NTSBFTW98LA214
Reported as
Univar 1081
Reported engine
Franklin 6A4150B3
Fatal injuries
0
Pilot’s flight hours
287 total126 in this make and model28 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.

Nosed over landing. (.4)on may 10, 1998, at 1450 mountain daylight time, a Stinson 108-1, N8178K, sustained substantial damage when it nosed over during landing roll at Salt Lake City #2 airport. The private pilot and sole occupant received minor injuries. The cross-country flight originated at tooele, Utah, and was operating under title 14 CFR part 91. Visual meteorological conditions prevailed and no flight plan was filed. According to the pilot, while enroute to Salt Lake City #2 airport, he encountered severe wind and turbulence. He attempted 2 landings at the airport, and performed a go-around each time due to turbulence. He was successful on his third attempt to land, but while taxing to exit the runway, the aircraft encountered a gust of wind. The left wingtip struck the ground, causing the aircraft to turn 360 degrees, and come to rest on the left wing and nose. The pilot exited the aircraft, and another wind gust then caused the aircraft to nose over. According to the Salt Lake City police department's incident report, the aircraft sustained damage to the left main landing gear and the vertical stabilizer. Additionaly, the right wing was broken at the wing brace, the nose was dented, and the propeller was bent. The report stated that, at the time of the accident, the winds were reported at 20 to 25 knots, with gusts 30 to 35 knots. (-23)pilot rejected two landings because of gusty winds. Landed on the third attempt. After landing a gust of wind from the right caused the aircraft to veer to the left. The pilot added power but was unable to control the aircraft. The aircraft departed the left side of runway 16 and sustained substantial damage.

As the FAA filed it

NOSED OVER LANDING. (.4)ON MAY 10, 1998, AT 1450 MOUNTAIN DAYLIGHT TIME, A STINSON 108-1, N8178K, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT NOSED OVER DURING LANDING ROLL AT SALT LAKE CITY #2 AIRPORT. THE PRIVATE PILOT AND SOLE OCCUPANT RECEIVED MINOR INJURIES. THE CROSS-COUNTRY FLIGHT ORIGINATED AT TOOELE, UTAH, AND WAS OPERATING UNDER TITLE 14 CFR PART 91. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED. ACCORDING TO THE PILOT, WHILE ENROUTE TO SALT LAKE CITY #2 AIRPORT, HE ENCOUNTERED SEVERE WIND AND TURBULENCE. HE ATTEMPTED 2 LANDINGS AT THE AIRPORT, AND PERFORMED A GO-AROUND EACH TIME DUE TO TURBULENCE. HE WAS SUCCESSFUL ON HIS THIRD ATTEMPT TO LAND, BUT WHILE TAXING TO EXIT THE RUNWAY, THE AIRCRAFT ENCOUNTERED A GUST OF WIND. THE LEFT WINGTIP STRUCK THE GROUND, CAUSING THE AIRCRAFT TO TURN 360 DEGREES, AND COME TO REST ON THE LEFT WING AND NOSE. THE PILOT EXITED THE AIRCRAFT, AND ANOTHER WIND GUST THEN CAUSED THE AIRCRAFT TO NOSE OVER. ACCORDING TO THE SALT LAKE CITY POLICE DEPARTMENT'S INCIDENT REPORT, THE AIRCRAFT SUSTAINED DAMAGE TO THE LEFT MAIN LANDING GEAR AND THE VERTICAL STABILIZER. ADDITIONALY, THE RIGHT WING WAS BROKEN AT THE WING BRACE, THE NOSE WAS DENTED, AND THE PROPELLER WAS BENT. THE REPORT STATED THAT, AT THE TIME OF THE ACCIDENT, THE WINDS WERE REPORTED AT 20 TO 25 KNOTS, WITH GUSTS 30 TO 35 KNOTS. (-23)PILOT REJECTED TWO LANDINGS BECAUSE OF GUSTY WINDS. LANDED ON THE THIRD ATTEMPT. AFTER LANDING A GUST OF WIND FROM THE RIGHT CAUSED THE AIRCRAFT TO VEER TO THE LEFT. THE PILOT ADDED POWER BUT WAS UNABLE TO CONTROL THE AIRCRAFT. THE AIRCRAFT DEPARTED THE LEFT SIDE OF RUNWAY 16 AND SUSTAINED SUBSTANTIAL DAMAGE.

NTSB investigation

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