19980524015589A

Accident · Substantial damage

FAA accident report · Cessna 170A · Provo, UT · May 24, 1998

Date
May 24, 1998 · 14:00 local
Place
Provo, UT
Airport
Provo Municipal Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9732A
NTSB investigation
NTSBFTW98LA237
Reported as
Cessna 170A
Reported engine
Continental O300B
People aboard
1
Fatal injuries
0
Pilot’s flight hours
582 total38 in this make and model34 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.

Downwind landing and lack of tailwheel experience resulted in loss of control, dragged wingtip and groundloop. (.4)the pilot said that as he approached his destination, he was unable to contact either the airport or other air traffic to obtain wind information to find out which runway was in use. Flying over the airport, he saw that the wind sock indicated the winds were calm, so he landed on runway 13. He said the airplane 'felt soft on the left side' and began 'weaving' down the runway. The left wheel broke off the landing gear, and the airplane ground looped. A witness told the pilot he thought he 'may have experienced a right quartering tail wind gust.' An FAA inspector, who examined the airplane, said the failure appeared to be overload. (-23)pilot landed at Provo Utah on runway 13, during the landing role the airplane ground looped. The pilot landed in a tailwind condition which contributed to the loss of control and the ground loop. The pilot was following the other traffic in the pattern. The pilot was the only person onboard.

As the FAA filed it

DOWNWIND LANDING AND LACK OF TAILWHEEL EXPERIENCE RESULTED IN LOSS OF CONTROL, DRAGGED WINGTIP AND GROUNDLOOP. (.4)THE PILOT SAID THAT AS HE APPROACHED HIS DESTINATION, HE WAS UNABLE TO CONTACT EITHER THE AIRPORT OR OTHER AIR TRAFFIC TO OBTAIN WIND INFORMATION TO FIND OUT WHICH RUNWAY WAS IN USE. FLYING OVER THE AIRPORT, HE SAW THAT THE WIND SOCK INDICATED THE WINDS WERE CALM, SO HE LANDED ON RUNWAY 13. HE SAID THE AIRPLANE 'FELT SOFT ON THE LEFT SIDE' AND BEGAN 'WEAVING' DOWN THE RUNWAY. THE LEFT WHEEL BROKE OFF THE LANDING GEAR, AND THE AIRPLANE GROUND LOOPED. A WITNESS TOLD THE PILOT HE THOUGHT HE 'MAY HAVE EXPERIENCED A RIGHT QUARTERING TAIL WIND GUST.' AN FAA INSPECTOR, WHO EXAMINED THE AIRPLANE, SAID THE FAILURE APPEARED TO BE OVERLOAD. (-23)PILOT LANDED AT PROVO UTAH ON RUNWAY 13, DURING THE LANDING ROLE THE AIRPLANE GROUND LOOPED. THE PILOT LANDED IN A TAILWIND CONDITION WHICH CONTRIBUTED TO THE LOSS OF CONTROL AND THE GROUND LOOP. THE PILOT WAS FOLLOWING THE OTHER TRAFFIC IN THE PATTERN. THE PILOT WAS THE ONLY PERSON ONBOARD.

NTSB investigation

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

Other reports on N9732A · 2

Matched to the same aircraft by N-number and date.