20010503039779A

Accident · Substantial damage

FAA accident report · Piper PA-32-300 · Chefornak, AK · May 3, 2001

Date
May 3, 2001 · 10:50 local
Place
Chefornak, AK
Airport
Chefornak Airport
Phase of flight
Final Approach
Operating rules
Air taxi and commuter (Part 135)
Operator
GSBA
Damage
Substantial damage
Aircraft
N4089W
NTSB investigation
NTSBANC01LA053
Reported as
Piper PA32300
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,000 total2,300 in this make and model180 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) 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.