20060515030499A

Accident · Substantial damage

FAA accident report · Hughes 269C · Boise, ID · May 15, 2006

Date
May 15, 2006 · 15:25 local
Place
Boise, ID
Phase of flight
Pwr Off Vert Land/Autorotate
Operating rules
General operating rules (Part 91)
Operator
UABS
Damage
Substantial damage
Aircraft
N2096W
NTSB investigation
NTSBSEA06LA096
Reported as
Hughes 269C
People aboard
2
Fatal injuries
0
Pilot’s flight hours
5,714 total293 in this make and model46 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) During an FAR 141 training flight, the instructor pilot and the student pilot performed a simulated engine out autorotation training maneuver. The throttle of the helicopter was rolled to the closed position to simulate the engine failure. Shortly after closing the throttle, the crew noticed that the engine had quit for real. The maneuver now became an engine out forced landing in the desert south of Boise, Idaho airport. When the helicopter weas autorotated to a landing, it touched down and skidded to a stop in such a way that the motion of the helicopter caused the rotor blades to strike the aft structure of the tail assembly, severing the tail boom near the point where the tail rotor was mounted. The density altitude of the helicopter at the time the throttle was chopped for the engine out simulation was near 6500 feet.

As the FAA filed it

(-23) DURING AN FAR 141 TRAINING FLIGHT, THE INSTRUCTOR PILOT AND THE STUDENT PILOT PERFORMED A SIMULATED ENGINE OUT AUTOROTATION TRAINING MANEUVER. THE THROTTLE OF THE HELICOPTER WAS ROLLED TO THE CLOSED POSITION TO SIMULATE THE ENGINE FAILURE. SHORTLY AFTER CLOSING THE THROTTLE, THE CREW NOTICED THAT THE ENGINE HAD QUIT FOR REAL. THE MANEUVER NOW BECAME AN ENGINE OUT FORCED LANDING IN THE DESERT SOUTH OF BOISE, IDAHO AIRPORT. WHEN THE HELICOPTER WEAS AUTOROTATED TO A LANDING, IT TOUCHED DOWN AND SKIDDED TO A STOP IN SUCH A WAY THAT THE MOTION OF THE HELICOPTER CAUSED THE ROTOR BLADES TO STRIKE THE AFT STRUCTURE OF THE TAIL ASSEMBLY, SEVERING THE TAIL BOOM NEAR THE POINT WHERE THE TAIL ROTOR WAS MOUNTED. THE DENSITY ALTITUDE OF THE HELICOPTER AT THE TIME THE THROTTLE WAS CHOPPED FOR THE ENGINE OUT SIMULATION WAS NEAR 6500 FEET.

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 N2096W · 1

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