19961103034659A

Accident · Substantial damage

FAA accident report · Cessna A185E · Price, UT · November 3, 1996

Date
November 3, 1996 · 15:40 local
Place
Price, UT
Airport
Carbon County Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N19EC
NTSB investigation
NTSBSEA97LA024
Reported as
Cessna A185E
Reported engine
Continental IO520D
People aboard
2
Fatal injuries
0
Pilot’s flight hours
480 total9 in this make and model60 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.

New purchase. Lost control landing roll. Veered off runway. Gear attach bolt failed due stress. Unskilled in type. (.19) on November 3, 1996, approximately 1540 mountain standard time, a Cessna A185E, N19EC, purchased on the previous day by a private pilot, was substantially damaged during a loss of control on landing at the Carbon County Airport, Price, Utah. The pilot and passenger were uninjured. Visual meteorological conditions existed and the VFR flight plan which had been filed, had not been activated at the time of the accident. The flight, which was personal, was to have been operated under 14CFR91, and originated at houston, Texas, with its most recent stop at blanding, Utah. The pilot reported that the aircraft was landed normally on the centerline of runway 18 after which it began to deviate to the left. He reported applying right rudder which resulted in an over-correction and then applied left brake, after which the aircraft departed the runway. (.4) the pilot executed a landing to runway 18 (8,300 feet length) during which the tailwheel touched down followed by the main landing gear, and the aircraft bounced slightly. The aircraft began to track to the left and the p ilot corrected. The aircraft returned to and crossed over the centerline during which the pilot was unable to stop the right veer before the aircraft departed the right side of the runway. As the aircraft left the runway the left main landing gear separated. A single tire smear mark was observed on the runway beginning at the centerline, arcing right and then oscillating briefly before exiting the runway's edge. A blue smear mark consistent with the aircraft's blue left wingtip paint near the runway's edge was noted. Winds were out of the southwest at 4 knots 2 minutes after the accident. Metallurgical examination of the left main landing gear bolt revealed smearing of the bolt threads.

As the FAA filed it

NEW PURCHASE. LOST CONTROL LANDING ROLL. VEERED OFF RUNWAY. GEAR ATTACH BOLT FAILED DUE STRESS. UNSKILLED IN TYPE. (.19) ON NOVEMBER 3, 1996, APPROXIMATELY 1540 MOUNTAIN STANDARD TIME, A CESSNA A185E, N19EC, PURCHASED ON THE PREVIOUS DAY BY A PRIVATE PILOT, WAS SUBSTANTIALLY DAMAGED DURING A LOSS OF CONTROL ON LANDING AT THE CARBON COUNTY AIRPORT, PRICE, UTAH. THE PILOT AND PASSENGER WERE UNINJURED. VISUAL METEOROLOGICAL CONDITIONS EXISTED AND THE VFR FLIGHT PLAN WHICH HAD BEEN FILED, HAD NOT BEEN ACTIVATED AT THE TIME OF THE ACCIDENT. THE FLIGHT, WHICH WAS PERSONAL, WAS TO HAVE BEEN OPERATED UNDER 14CFR91, AND ORIGINATED AT HOUSTON, TEXAS, WITH ITS MOST RECENT STOP AT BLANDING, UTAH. THE PILOT REPORTED THAT THE AIRCRAFT WAS LANDED NORMALLY ON THE CENTERLINE OF RUNWAY 18 AFTER WHICH IT BEGAN TO DEVIATE TO THE LEFT. HE REPORTED APPLYING RIGHT RUDDER WHICH RESULTED IN AN OVER-CORRECTION AND THEN APPLIED LEFT BRAKE, AFTER WHICH THE AIRCRAFT DEPARTED THE RUNWAY. (.4) THE PILOT EXECUTED A LANDING TO RUNWAY 18 (8,300 FEET LENGTH) DURING WHICH THE TAILWHEEL TOUCHED DOWN FOLLOWED BY THE MAIN LANDING GEAR, AND THE AIRCRAFT BOUNCED SLIGHTLY. THE AIRCRAFT BEGAN TO TRACK TO THE LEFT AND THE P ILOT CORRECTED. THE AIRCRAFT RETURNED TO AND CROSSED OVER THE CENTERLINE DURING WHICH THE PILOT WAS UNABLE TO STOP THE RIGHT VEER BEFORE THE AIRCRAFT DEPARTED THE RIGHT SIDE OF THE RUNWAY. AS THE AIRCRAFT LEFT THE RUNWAY THE LEFT MAIN LANDING GEAR SEPARATED. A SINGLE TIRE SMEAR MARK WAS OBSERVED ON THE RUNWAY BEGINNING AT THE CENTERLINE, ARCING RIGHT AND THEN OSCILLATING BRIEFLY BEFORE EXITING THE RUNWAY'S EDGE. A BLUE SMEAR MARK CONSISTENT WITH THE AIRCRAFT'S BLUE LEFT WINGTIP PAINT NEAR THE RUNWAY'S EDGE WAS NOTED. WINDS WERE OUT OF THE SOUTHWEST AT 4 KNOTS 2 MINUTES AFTER THE ACCIDENT. METALLURGICAL EXAMINATION OF THE LEFT MAIN LANDING GEAR BOLT REVEALED SMEARING OF THE BOLT THREADS.

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 N19EC · 2

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