What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On may 3, 2001, about 1050 adt, a wheel equipped Piper PA-32-300, N4089W, sustained substantial damage while attempting a landing at Chefornak, Alaska. The aircraft was being operated as a visual flight rules (VFR) cross country commercial flight, when the accident occurred. A licensed commercial pilot operated the aircraft. The aircraft is owned by a leasing company and operated by a part 135 on demand operator. Visual meteorological conditions prevailed in the area of the accident. During an interview with an FAA inspector on may 4, 2001, the pilot reported that when he was on final approach, configured with full flaps, airspeed at the threshold 80 mph, the aircraft stalled. The aircraft struck the runway in the stall and bounced back into the air, and with a crosswind of 10 to 15 knots the aircraft struck the tundra about 30 feet from the runway. The aircraft came to rest with the left gear sheared off, nose gear collapsed, propeller bent back formed to the fuselage and the right wing bent down at a 90 degree angle. Investigation is ongoing for possible violations.
As the FAA filed it
(-23) ON MAY 3, 2001, ABOUT 1050 ADT, A WHEEL EQUIPPED PIPER PA-32-300, N4089W, SUSTAINED SUBSTANTIAL DAMAGE WHILE ATTEMPTING A LANDING AT CHEFORNAK, ALASKA. THE AIRCRAFT WAS BEING OPERATED AS A VISUAL FLIGHT RULES (VFR) CROSS COUNTRY COMMERCIAL FLIGHT, WHEN THE ACCIDENT OCCURRED. A LICENSED COMMERCIAL PILOT OPERATED THE AIRCRAFT. THE AIRCRAFT IS OWNED BY A LEASING COMPANY AND OPERATED BY A PART 135 ON DEMAND OPERATOR. VISUAL METEOROLOGICAL CONDITIONS PREVAILED IN THE AREA OF THE ACCIDENT. DURING AN INTERVIEW WITH AN FAA INSPECTOR ON MAY 4, 2001, THE PILOT REPORTED THAT WHEN HE WAS ON FINAL APPROACH, CONFIGURED WITH FULL FLAPS, AIRSPEED AT THE THRESHOLD 80 MPH, THE AIRCRAFT STALLED. THE AIRCRAFT STRUCK THE RUNWAY IN THE STALL AND BOUNCED BACK INTO THE AIR, AND WITH A CROSSWIND OF 10 TO 15 KNOTS THE AIRCRAFT STRUCK THE TUNDRA ABOUT 30 FEET FROM THE RUNWAY. THE AIRCRAFT CAME TO REST WITH THE LEFT GEAR SHEARED OFF, NOSE GEAR COLLAPSED, PROPELLER BENT BACK FORMED TO THE FUSELAGE AND THE RIGHT WING BENT DOWN AT A 90 DEGREE ANGLE. INVESTIGATION IS ONGOING FOR POSSIBLE VIOLATIONS.
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 N4089W · 2
Matched to the same aircraft by N-number and date.