20020831028909A

Accident · Destroyed

FAA accident report · Piper PA-28-140 · Price, TX · August 31, 2002

Date
August 31, 2002 · 18:00 local
Place
Price, TX
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N3961K
NTSB investigation
NTSBFTW02LA244
Reported as
Piper PA28140

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) On August 31, 2002 @ 1600 CDT, a Piper PA-28-140, N3961K, during a flight from canton, Texas to the gregg county airport in longview, Texas, experienced power loss which forced the pilot to land in a field near Price, Texas. The forced landing caused major damage to the aircraft, severing the right wing, right main landing gear and nose landing gear, crumpling the fuselage, removing sheet metal and supporting ribs from the passenger side floor, cracking the windshield, breaking the pilot's control yoke and bending the throttle control and propeller. The airplane was owned and operated by Mr. Veldon clyde ross under the provision of title 14 CFR part 91 and visual flight rules. Visual meteorological conditions prevailed and a flight plan was not filed for personal flight. The pilot received no injuries.

As the FAA filed it

(-23) ON AUGUST 31, 2002 @ 1600 CDT, A PIPER PA-28-140, N3961K, DURING A FLIGHT FROM CANTON, TEXAS TO THE GREGG COUNTY AIRPORT IN LONGVIEW, TEXAS, EXPERIENCED POWER LOSS WHICH FORCED THE PILOT TO LAND IN A FIELD NEAR PRICE, TEXAS. THE FORCED LANDING CAUSED MAJOR DAMAGE TO THE AIRCRAFT, SEVERING THE RIGHT WING, RIGHT MAIN LANDING GEAR AND NOSE LANDING GEAR, CRUMPLING THE FUSELAGE, REMOVING SHEET METAL AND SUPPORTING RIBS FROM THE PASSENGER SIDE FLOOR, CRACKING THE WINDSHIELD, BREAKING THE PILOT'S CONTROL YOKE AND BENDING THE THROTTLE CONTROL AND PROPELLER. THE AIRPLANE WAS OWNED AND OPERATED BY MR. VELDON CLYDE ROSS UNDER THE PROVISION OF TITLE 14 CFR PART 91 AND VISUAL FLIGHT RULES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND A FLIGHT PLAN WAS NOT FILED FOR PERSONAL FLIGHT. THE PILOT RECEIVED NO INJURIES.

NTSB investigation

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