20010713020719A

Accident · No damage

FAA accident report · Ayres S-2R · Nezperce, ID · July 13, 2001

Date
July 13, 2001 · 18:00 local
Place
Nezperce, ID
Operating rules
Agricultural (Part 137)
Operator
WYTG
Damage
No damage
Aircraft
N5011X
NTSB investigation
NTSBSEA01LA131
Reported as
Ayres S2R

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 July 13, 2001, at about 1800 pacific daylight time, a rockwell international S2R, N5011X, struck the terrain in a waist high wheat field. The landing was in a draw area, (about two miles west of nez perce, ID) and then upwards in the field for approximately 350 yards. The wings were then folded-back, one propeller blade broken off and the blade bent, and the undercarriage broken off into large chunks (the left main gear). The propeller hub and two blades were broken off and the engine had separated from the fuselage. The propeller hub and blades landed ahead of the fuselage and separated engine. The final outcome of the uphill landing was the aircraft ahd made an approximately 180 degree turn. The sole occupant of the aircraft was fatally injured. The flight had originated from craigmont, ID, and was on its return trip when the accident occurred.

As the FAA filed it

(-23) ON JULY 13, 2001, AT ABOUT 1800 PACIFIC DAYLIGHT TIME, A ROCKWELL INTERNATIONAL S2R, N5011X, STRUCK THE TERRAIN IN A WAIST HIGH WHEAT FIELD. THE LANDING WAS IN A DRAW AREA, (ABOUT TWO MILES WEST OF NEZ PERCE, ID) AND THEN UPWARDS IN THE FIELD FOR APPROXIMATELY 350 YARDS. THE WINGS WERE THEN FOLDED-BACK, ONE PROPELLER BLADE BROKEN OFF AND THE BLADE BENT, AND THE UNDERCARRIAGE BROKEN OFF INTO LARGE CHUNKS (THE LEFT MAIN GEAR). THE PROPELLER HUB AND TWO BLADES WERE BROKEN OFF AND THE ENGINE HAD SEPARATED FROM THE FUSELAGE. THE PROPELLER HUB AND BLADES LANDED AHEAD OF THE FUSELAGE AND SEPARATED ENGINE. THE FINAL OUTCOME OF THE UPHILL LANDING WAS THE AIRCRAFT AHD MADE AN APPROXIMATELY 180 DEGREE TURN. THE SOLE OCCUPANT OF THE AIRCRAFT WAS FATALLY INJURED. THE FLIGHT HAD ORIGINATED FROM CRAIGMONT, ID, AND WAS ON ITS RETURN TRIP WHEN THE ACCIDENT OCCURRED.

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 N5011X · 1

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