20011005026119A

Accident · No damage

FAA accident report · Beech T42A · Bend, OR · October 5, 2001

Date
October 5, 2001 · 15:50 local
Place
Bend, OR
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N55TE
NTSB investigation
NTSBSEA02LA003
Reported as
Beech T42A

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.

(.19) On October 5, 2001, about 1550 pacific daylight time, an experimental ellsberg one design, N55TE, nosed over during a forced landing about eight miles north of Bend, Oregon. The pilot, who was the sole occupant, received minor injuries, and the aircraft, which is owned and operated by the pilot, sustained substantial damage. The 14 CFR part 91 aerobatic practice flight, which departed Bend municipal airport about 1545, was being operated in visual meteorological conditions. No flight plan had been filed. There was no report of an ELT activation. According to the pilot, just after he entered the aerobatic box, and while still at cruise, the engine began to violently shake. He therefore shut the engine off, and began a glide toward a forced landing on a nearby road. During the descent, the entire aircraft continued to vibrate to such a degree that the pilot was concerned about the engine separating from the airframe. When he reached the ground, the pilot landed on a road, but during the landing roll, the aircraft departed the road and nosed over in the soft terrain. According to the pilot, a quick check of the engine area revealed that a propeller counterweight had separated from its mounting tab.

As the FAA filed it

(.19) ON OCTOBER 5, 2001, ABOUT 1550 PACIFIC DAYLIGHT TIME, AN EXPERIMENTAL ELLSBERG ONE DESIGN, N55TE, NOSED OVER DURING A FORCED LANDING ABOUT EIGHT MILES NORTH OF BEND, OREGON. THE PILOT, WHO WAS THE SOLE OCCUPANT, RECEIVED MINOR INJURIES, AND THE AIRCRAFT, WHICH IS OWNED AND OPERATED BY THE PILOT, SUSTAINED SUBSTANTIAL DAMAGE. THE 14 CFR PART 91 AEROBATIC PRACTICE FLIGHT, WHICH DEPARTED BEND MUNICIPAL AIRPORT ABOUT 1545, WAS BEING OPERATED IN VISUAL METEOROLOGICAL CONDITIONS. NO FLIGHT PLAN HAD BEEN FILED. THERE WAS NO REPORT OF AN ELT ACTIVATION. ACCORDING TO THE PILOT, JUST AFTER HE ENTERED THE AEROBATIC BOX, AND WHILE STILL AT CRUISE, THE ENGINE BEGAN TO VIOLENTLY SHAKE. HE THEREFORE SHUT THE ENGINE OFF, AND BEGAN A GLIDE TOWARD A FORCED LANDING ON A NEARBY ROAD. DURING THE DESCENT, THE ENTIRE AIRCRAFT CONTINUED TO VIBRATE TO SUCH A DEGREE THAT THE PILOT WAS CONCERNED ABOUT THE ENGINE SEPARATING FROM THE AIRFRAME. WHEN HE REACHED THE GROUND, THE PILOT LANDED ON A ROAD, BUT DURING THE LANDING ROLL, THE AIRCRAFT DEPARTED THE ROAD AND NOSED OVER IN THE SOFT TERRAIN. ACCORDING TO THE PILOT, A QUICK CHECK OF THE ENGINE AREA REVEALED THAT A PROPELLER COUNTERWEIGHT HAD SEPARATED FROM ITS MOUNTING TAB.

NTSB investigation

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