20000406006009A

Accident · Substantial damage

FAA accident report · Piper PA-24 · Herlong, CA · April 6, 2000

Date
April 6, 2000 · 19:30 local
Place
Herlong, CA
Airport
Herlong Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N180BC
NTSB investigation
NTSBLAX00LA147
Reported as
Piper PA24
Reported engine
Lycoming O360A1A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,600 total2,380 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.

(-23) Pilot reported that he circled the Herlong Airport twice, noting that the wind sock was blowing intermittently in different directions. Upon landing, the wind blew the airplane off of the runway and into the barbed wire fence. The pilot reported that he pulled the mixture control before hitting the fence. The airplane wings sustained substantial damage from the steel fence posts. (.4)on April 6, 2000, at 1930 hours pacific daylight time, a Piper PA-24, N180BC, veered off the runway and impacted a metal fence after landing at the Herlong, California, airport. The airplane, owned and operated by the pilot, sustained substantial damage. The private pilot was not injured. The personal cross-country flight, conducted under the provisions of 14 CFR part 91, had originated in creswell, Oregon, about 1800, and was terminating at the time of the accident. Night visual meteorological conditions prevailed and no flight plan was filed. The pilot reported that after flying over the airport to check the wind conditions, he performed a normal landing to runway 24. During the landing rollout, while at about 50 mph, a strong gust of wind hit him from the left. The airplane veered to the right off the runway, then continued through a metal fence and into a field. There was damage to the left wing, aileron, and landing gear. The pilot reported that the winds at Herlong at the time of the accident were from the southwest at 25 to 35 knots, gusting to 35 knots and higher. According to the manufacturer, there is no published maximum crosswind component for the PA-24.

As the FAA filed it

(-23) PILOT REPORTED THAT HE CIRCLED THE HERLONG AIRPORT TWICE, NOTING THAT THE WIND SOCK WAS BLOWING INTERMITTENTLY IN DIFFERENT DIRECTIONS. UPON LANDING, THE WIND BLEW THE AIRPLANE OFF OF THE RUNWAY AND INTO THE BARBED WIRE FENCE. THE PILOT REPORTED THAT HE PULLED THE MIXTURE CONTROL BEFORE HITTING THE FENCE. THE AIRPLANE WINGS SUSTAINED SUBSTANTIAL DAMAGE FROM THE STEEL FENCE POSTS. (.4)ON APRIL 6, 2000, AT 1930 HOURS PACIFIC DAYLIGHT TIME, A PIPER PA-24, N180BC, VEERED OFF THE RUNWAY AND IMPACTED A METAL FENCE AFTER LANDING AT THE HERLONG, CALIFORNIA, AIRPORT. THE AIRPLANE, OWNED AND OPERATED BY THE PILOT, SUSTAINED SUBSTANTIAL DAMAGE. THE PRIVATE PILOT WAS NOT INJURED. THE PERSONAL CROSS-COUNTRY FLIGHT, CONDUCTED UNDER THE PROVISIONS OF 14 CFR PART 91, HAD ORIGINATED IN CRESWELL, OREGON, ABOUT 1800, AND WAS TERMINATING AT THE TIME OF THE ACCIDENT. NIGHT VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED. THE PILOT REPORTED THAT AFTER FLYING OVER THE AIRPORT TO CHECK THE WIND CONDITIONS, HE PERFORMED A NORMAL LANDING TO RUNWAY 24. DURING THE LANDING ROLLOUT, WHILE AT ABOUT 50 MPH, A STRONG GUST OF WIND HIT HIM FROM THE LEFT. THE AIRPLANE VEERED TO THE RIGHT OFF THE RUNWAY, THEN CONTINUED THROUGH A METAL FENCE AND INTO A FIELD. THERE WAS DAMAGE TO THE LEFT WING, AILERON, AND LANDING GEAR. THE PILOT REPORTED THAT THE WINDS AT HERLONG AT THE TIME OF THE ACCIDENT WERE FROM THE SOUTHWEST AT 25 TO 35 KNOTS, GUSTING TO 35 KNOTS AND HIGHER. ACCORDING TO THE MANUFACTURER, THERE IS NO PUBLISHED MAXIMUM CROSSWIND COMPONENT FOR THE PA-24.

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 N180BC · 2

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