20100511005309A

Accident · Substantial damage

FAA accident report · Bell 407 · Abingdon, VA · May 11, 2010

Date
May 11, 2010 · 14:00 local
Place
Abingdon, VA
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N31VA
NTSB investigation
NTSBERA10TA261
Reported as
Bell 407
Reported engine
Rolls-Royce 250
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
0 total0 in this make and model0 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.

At approximately 1355 EDT the aircraft crew was conducting a training flight that originated at Virginia highlands airport (vji) in Abingdon, VA. The purpose of the flight was for aircraft orientation training. The aircraft flew one traffic pattern at the airport and proceeded toward a small confined area used for training. During the flight to the area a very low growl noise was heard by the crew. The flight instructor then took over the control of the aircraft. As the aircraft made a right turn toward the confined area at approximately 200 feet AGL and 80 knots, the engine surged and began to make a very loud growl noise, the engine failed, and the pilot initiated the emergency engine out procedure. The pilot performed an autorotation, the aircraft made a hard landing, bounced once, and came to rest on a slight slope in a field. The hard landing resulted in the aircraft skids being splayed and the left tail horizontal stabilizer vertical fin being contacted by the main rotor blade removing approximately 3 inches from the tip of the fin. The flir system imaging unit at the bottom left hand mid-section of the aircraft had pushed up through the floor of the cabin area and the data link microwave antenna had torn from the bottom section of the aircraft just forward of the aft skid tube.

As the FAA filed it

AT APPROXIMATELY 1355 EDT THE AIRCRAFT CREW WAS CONDUCTING A TRAINING FLIGHT THAT ORIGINATED AT VIRGINIA HIGHLANDS AIRPORT (VJI) IN ABINGDON, VA. THE PURPOSE OF THE FLIGHT WAS FOR AIRCRAFT ORIENTATION TRAINING. THE AIRCRAFT FLEW ONE TRAFFIC PATTERN AT THE AIRPORT AND PROCEEDED TOWARD A SMALL CONFINED AREA USED FOR TRAINING. DURING THE FLIGHT TO THE AREA A VERY LOW GROWL NOISE WAS HEARD BY THE CREW. THE FLIGHT INSTRUCTOR THEN TOOK OVER THE CONTROL OF THE AIRCRAFT. AS THE AIRCRAFT MADE A RIGHT TURN TOWARD THE CONFINED AREA AT APPROXIMATELY 200 FEET AGL AND 80 KNOTS, THE ENGINE SURGED AND BEGAN TO MAKE A VERY LOUD GROWL NOISE, THE ENGINE FAILED, AND THE PILOT INITIATED THE EMERGENCY ENGINE OUT PROCEDURE. THE PILOT PERFORMED AN AUTOROTATION, THE AIRCRAFT MADE A HARD LANDING, BOUNCED ONCE, AND CAME TO REST ON A SLIGHT SLOPE IN A FIELD. THE HARD LANDING RESULTED IN THE AIRCRAFT SKIDS BEING SPLAYED AND THE LEFT TAIL HORIZONTAL STABILIZER VERTICAL FIN BEING CONTACTED BY THE MAIN ROTOR BLADE REMOVING APPROXIMATELY 3 INCHES FROM THE TIP OF THE FIN. THE FLIR SYSTEM IMAGING UNIT AT THE BOTTOM LEFT HAND MID-SECTION OF THE AIRCRAFT HAD PUSHED UP THROUGH THE FLOOR OF THE CABIN AREA AND THE DATA LINK MICROWAVE ANTENNA HAD TORN FROM THE BOTTOM SECTION OF THE AIRCRAFT JUST FORWARD OF THE AFT SKID TUBE.

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 N31VA · 1

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