20030608012499A

Accident · Substantial damage

FAA accident report · Amtr EXEC90 · Searcy, AR · June 8, 2003

Date
June 8, 2003 · 16:00 local
Place
Searcy, AR
Phase of flight
Autorot Descent (Rotorcraft)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8246J
NTSB investigation
NTSBCHI03LA155
Reported as
Amtr EXEC90
People aboard
1
Fatal injuries
0
Pilot’s flight hours
960 total76 in this make and model97 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 June 6, 2003, at approximately 1600 hours CDT, N8246J, a rotorway executive 90 experimental helicopter, was involved in an accident. It was discovered that while in cruise flight, the pilot in command experienced an engine power decrease. The trouble was an overheating engine. The pilot in command executed an emergency landing and upon power decrease, the engine faltered then failed. An autorotation was entered and at ground contact, the aircraft pivoted to the right. With the energy still directed in the original tract and upon ground contact with the left skid, a rolling motion was produced. The aircraft rolled to the left coming to rest on the left side. The aircraft sustained substantial damage, no injuries were inflected, and no flight plan was filed. The weather was VFR.

As the FAA filed it

(-23) ON JUNE 6, 2003, AT APPROXIMATELY 1600 HOURS CDT, N8246J, A ROTORWAY EXECUTIVE 90 EXPERIMENTAL HELICOPTER, WAS INVOLVED IN AN ACCIDENT. IT WAS DISCOVERED THAT WHILE IN CRUISE FLIGHT, THE PILOT IN COMMAND EXPERIENCED AN ENGINE POWER DECREASE. THE TROUBLE WAS AN OVERHEATING ENGINE. THE PILOT IN COMMAND EXECUTED AN EMERGENCY LANDING AND UPON POWER DECREASE, THE ENGINE FALTERED THEN FAILED. AN AUTOROTATION WAS ENTERED AND AT GROUND CONTACT, THE AIRCRAFT PIVOTED TO THE RIGHT. WITH THE ENERGY STILL DIRECTED IN THE ORIGINAL TRACT AND UPON GROUND CONTACT WITH THE LEFT SKID, A ROLLING MOTION WAS PRODUCED. THE AIRCRAFT ROLLED TO THE LEFT COMING TO REST ON THE LEFT SIDE. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE, NO INJURIES WERE INFLECTED, AND NO FLIGHT PLAN WAS FILED. THE WEATHER WAS VFR.

NTSB investigation

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