20000603014579A

Accident · Substantial damage

FAA accident report · Piper PA-32-260 · Clinton, OK · June 3, 2000

Date
June 3, 2000 · 15:00 local
Place
Clinton, OK
Airport
Clinton Municipal Airport
Phase of flight
Missed Approach IFR
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3869W
NTSB investigation
NTSBFTW00LA263
Reported as
Piper PA32260
Reported engine
Lycoming O540E4B5
People aboard
2
Fatal injuries
0
Pilot’s flight hours
3,000 total200 in this make and model75 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) When banking a/c in the base leg of short final to Clinton muni airport the engine quit. Pilot switched fuel tanks but the engine would not restart. Attempted to land in a field short and right of the runway. A/c bounced once then on second impact the nose gear collapsed. (.4) on June 3, 2000, at 1500 central daylight time, a Piper PA-32-260 airplane, N3869W, was substantially damaged during a forced landing at the Clinton Municipal Airport, near Clinton, Oklahoma. The private pilot, who was the registered owner and operator of the airplane, and his passenger were not injured. Visual meteorological conditions prevailed for the 14 code of federal regulations part 91 personal flight and no flight plan was filed. The local flight originated from the Clinton Municipal Airport. According to the FAA inspector, the airplane's engine lost total power as the pilot was maneuvering the airplane on final approach to runway 17. During the ensuing forced landing the airplane contacted a dirt terrace and came to a stop upright. The nose gear collapsed, and the airplane came to a stop upright. Following the accident, the pilot reported that "he was not sure if the fuel selector was in the detent for the selected tank and he did not have time to check prior to landing." The FAA inspector reported that the engine firewall was structurally damaged, and both wings were comprised at their respective attaching points to the fuselage. There was also damage to the "structure at the main landing gear attach points". This damage was initailly reported to the NTSB as minor. Subsequently, on October 3, 2000, the damage was reported as substantial. Additionally, multiple attempts to obtain a completed NTSB form 6120.1/2, pilot/operator aircraft accident report, from the pilot/owner were unseuccessful

As the FAA filed it

(-23) WHEN BANKING A/C IN THE BASE LEG OF SHORT FINAL TO CLINTON MUNI AIRPORT THE ENGINE QUIT. PILOT SWITCHED FUEL TANKS BUT THE ENGINE WOULD NOT RESTART. ATTEMPTED TO LAND IN A FIELD SHORT AND RIGHT OF THE RUNWAY. A/C BOUNCED ONCE THEN ON SECOND IMPACT THE NOSE GEAR COLLAPSED. (.4) ON JUNE 3, 2000, AT 1500 CENTRAL DAYLIGHT TIME, A PIPER PA-32-260 AIRPLANE, N3869W, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING AT THE CLINTON MUNICIPAL AIRPORT, NEAR CLINTON, OKLAHOMA. THE PRIVATE PILOT, WHO WAS THE REGISTERED OWNER AND OPERATOR OF THE AIRPLANE, AND HIS PASSENGER WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE 14 CODE OF FEDERAL REGULATIONS PART 91 PERSONAL FLIGHT AND NO FLIGHT PLAN WAS FILED. THE LOCAL FLIGHT ORIGINATED FROM THE CLINTON MUNICIPAL AIRPORT. ACCORDING TO THE FAA INSPECTOR, THE AIRPLANE'S ENGINE LOST TOTAL POWER AS THE PILOT WAS MANEUVERING THE AIRPLANE ON FINAL APPROACH TO RUNWAY 17. DURING THE ENSUING FORCED LANDING THE AIRPLANE CONTACTED A DIRT TERRACE AND CAME TO A STOP UPRIGHT. THE NOSE GEAR COLLAPSED, AND THE AIRPLANE CAME TO A STOP UPRIGHT. FOLLOWING THE ACCIDENT, THE PILOT REPORTED THAT "HE WAS NOT SURE IF THE FUEL SELECTOR WAS IN THE DETENT FOR THE SELECTED TANK AND HE DID NOT HAVE TIME TO CHECK PRIOR TO LANDING." THE FAA INSPECTOR REPORTED THAT THE ENGINE FIREWALL WAS STRUCTURALLY DAMAGED, AND BOTH WINGS WERE COMPRISED AT THEIR RESPECTIVE ATTACHING POINTS TO THE FUSELAGE. THERE WAS ALSO DAMAGE TO THE "STRUCTURE AT THE MAIN LANDING GEAR ATTACH POINTS". THIS DAMAGE WAS INITAILLY REPORTED TO THE NTSB AS MINOR. SUBSEQUENTLY, ON OCTOBER 3, 2000, THE DAMAGE WAS REPORTED AS SUBSTANTIAL. ADDITIONALLY, MULTIPLE ATTEMPTS TO OBTAIN A COMPLETED NTSB FORM 6120.1/2, PILOT/OPERATOR AIRCRAFT ACCIDENT REPORT, FROM THE PILOT/OWNER WERE UNSEUCCESSFUL

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 N3869W · 1

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