No fatalities

24 Sep 2012: MCDONNELL DOUGLAS HELI CO 369FF (N911BL) — LAS VEGAS METROPOLITAN POLICE DEPARTMENT — Las Vegas, NV

Las Vegas, NV, United States

On 24 Sep 2012, a MCDONNELL DOUGLAS HELI CO 369FF (registration N911BL) operated by LAS VEGAS METROPOLITAN POLICE DEPARTMENT was involved in an aviation accident near Las Vegas, NV. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain sufficient airspeed while performing a 270-degree practice autorotation with a gusting tailwind at a high-density altitude. This summary draws on records from NTSB; 14 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On September 24, 2012, a McDonnell Douglas 369FF helicopter, N911BL, sustained substantial damage during a hard landing following a practice autorotation at North Las Vegas Airport. Two pilots, both flight instructors, received minor injuries.

Accident Details

On September 24, 2012, about 1600 Pacific daylight time, a McDonnell Douglas 369FF helicopter, registration N911BL, sustained substantial damage during a hard landing after a practice autorotation at North Las Vegas Airport, Las Vegas, Nevada. The helicopter was registered to the Las Vegas Metropolitan Police Department and was being operated as a public aircraft training flight. The two pilots, who both held flight instructor certificates, sustained minor injuries.

Flight Information

The local training flight had originated from North Las Vegas Airport approximately 30 minutes before the accident. Visual meteorological conditions prevailed at the time, and no flight plan had been filed.

Pilot Statements

The pilot-in-command (PIC)/pilot-giving-instruction reported that he and the pilot receiving instruction were alternately practicing autorotations. He decided to demonstrate a 270-degree autorotation to the touchdown point on taxiway Zulu. The maneuver began on a 180-degree heading, 800 feet above ground, at an airspeed of 85 knots. As the helicopter crossed the intended touchdown point, the PIC rolled the throttle back to initiate the autorotation. He estimated the wind to be from 180 to 230 degrees at 15 knots, gusting to 26 knots. During a left turn, he reported increasing his bank angle to maintain ground reference to the touchdown point due to a tailwind. The pilot receiving instruction reported that moments later, the helicopter was in a high rate of descent with decreasing airspeed.

Impact and Damage

The helicopter impacted terrain in a tail-low attitude. Subsequently, the tail boom separated from the fuselage, the helicopter rolled onto its right side, and the right landing skid support structure folded under the fuselage.

Weather Conditions

At 1605, the reported wind at North Las Vegas Airport, elevation 2,205 feet, was 270 degrees at 13 knots, gusting to 22 knots. The calculated density altitude, using a barometric pressure of 29.77 inches of mercury, was 5,116 feet.

Contributing factors

Causes

Instructor/check pilotAirspeed — Not attained/maintained

Other contributing factors

Effect on operation