20000916015659A

Accident · Substantial damage

FAA accident report · Cessna A185F · Burnet, TX · September 16, 2000

Date
September 16, 2000 · 12:00 local
Place
Burnet, TX
Airport
Burnet Municipal Kate Craddock Fld
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N34NC
NTSB investigation
NTSBFTW00LA261
Reported as
Cessna A185F
Fatal injuries
0
Pilot’s flight hours
4,000 total350 in this make and model41 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) Accident #FTWOOLA261 (.4)on September 16, 2000, at 1200 central daylight time, a Cessna 185F tailwheel equipped airplane, N34NC, was substantially damaged while landing on runway 01 at Burnet municipal airport, Burnet, Texas. The commercial pilot, who was the registered owner and operator of the airplane, and his passenger sustained minor injuries. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 code of federal regulations part 91 personal flight. The flight originated from tp mccampbell airport, ingleside, Texas, at 1024 and was destined for Burnet, Texas. According to the pilot, he utilized the "proper crosswind landing technique," during the approach to runway 01. As the airplane touched down, it encountered a "crosswind gust," and subsequently, the airplane swerved to the right, the left wing "dipped," the wing-tip contacted the runway surface, and the airplane nosed over. The airplane came to rest inverted on the runway. The pilot added that the winds were from 100 degrees at 7 knots, gusting between 10 and 15 knots. According to an FAA inspector, who examined the airplane, the top of the vertical stabilizer, rudder, and both main wing spars sustained structural damage. He added that the three propeller blades were curled.

As the FAA filed it

(-23) ACCIDENT #FTWOOLA261 (.4)ON SEPTEMBER 16, 2000, AT 1200 CENTRAL DAYLIGHT TIME, A CESSNA 185F TAILWHEEL EQUIPPED AIRPLANE, N34NC, WAS SUBSTANTIALLY DAMAGED WHILE LANDING ON RUNWAY 01 AT BURNET MUNICIPAL AIRPORT, BURNET, TEXAS. THE COMMERCIAL PILOT, WHO WAS THE REGISTERED OWNER AND OPERATOR OF THE AIRPLANE, AND HIS PASSENGER SUSTAINED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND A FLIGHT PLAN WAS NOT FILED FOR THE 14 CODE OF FEDERAL REGULATIONS PART 91 PERSONAL FLIGHT. THE FLIGHT ORIGINATED FROM TP MCCAMPBELL AIRPORT, INGLESIDE, TEXAS, AT 1024 AND WAS DESTINED FOR BURNET, TEXAS. ACCORDING TO THE PILOT, HE UTILIZED THE "PROPER CROSSWIND LANDING TECHNIQUE," DURING THE APPROACH TO RUNWAY 01. AS THE AIRPLANE TOUCHED DOWN, IT ENCOUNTERED A "CROSSWIND GUST," AND SUBSEQUENTLY, THE AIRPLANE SWERVED TO THE RIGHT, THE LEFT WING "DIPPED," THE WING-TIP CONTACTED THE RUNWAY SURFACE, AND THE AIRPLANE NOSED OVER. THE AIRPLANE CAME TO REST INVERTED ON THE RUNWAY. THE PILOT ADDED THAT THE WINDS WERE FROM 100 DEGREES AT 7 KNOTS, GUSTING BETWEEN 10 AND 15 KNOTS. ACCORDING TO AN FAA INSPECTOR, WHO EXAMINED THE AIRPLANE, THE TOP OF THE VERTICAL STABILIZER, RUDDER, AND BOTH MAIN WING SPARS SUSTAINED STRUCTURAL DAMAGE. HE ADDED THAT THE THREE PROPELLER BLADES WERE CURLED.

NTSB investigation

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