No fatalities

Helicopter Accident During Simulated Emergency Landing (N160TX)

Odessa, TX, US

On August 23, 2005, a Robinson R-44 (registration N160TX) was involved in an aviation accident near Odessa, TX. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to maintain main rotor RPM and the improper landing flare which resulted in a hard landing. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 5 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A commercial pilot performing a simulated emergency landing for passengers impacted the runway hard, causing the main rotor to strike the tail boom and separate it from the fuselage. The helicopter slid and rolled onto its right side.

Accident Overview

The accident occurred when a commercial pilot with 1,212 hours of flight experience conducted a simulated emergency landing demonstration for passengers. The pilot departed from runway 11 and remained in the landing pattern.

Flight Details

While on the left downwind leg, the pilot applied carburetor heat and radioed his intentions. At approximately 200 feet above ground level (agl), he lined up for a final approach to runway 11 and checked his instruments. All indications were reported as "normal."

Accident Sequence

The pilot then proceeded to "roll off" the engine power. As rotor RPM bled off very rapidly, the pilot elected to leave the collective in the full down position until he applied full engine throttle to start the flare. Shortly thereafter, the pilot realized the helicopter was going to impact the ground "hard." The helicopter contacted the runway with sufficient force that the main rotor blades struck the tail boom, causing the tail boom to separate from the fuselage.

Post-Impact

After the initial impact, the helicopter continued sliding down the runway for approximately 25 to 30 feet before rolling onto its right side and coming to rest.

Examination

An examination of the helicopter revealed structural damage to the fuselage, main rotor blades, tail rotor blades, and the tail rotor drive shaft. The pilot reported that there was no mechanical malfunction or failure with the helicopter.

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Frequently asked questions

What happened in the 23 Aug 2005 Robinson R-44 accident near Odessa, TX?

A commercial pilot performing a simulated emergency landing for passengers impacted the runway hard, causing the main rotor to strike the tail boom and separate it from the fuselage. The helicopter slid and rolled onto its right side.

Were there any fatalities in the 23 Aug 2005 Robinson R-44 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 23 Aug 2005 involved a Robinson R-44, registration N160TX, at Odessa, TX.

What was the probable cause of the accident?

The pilot's failure to maintain main rotor RPM and the improper landing flare which resulted in a hard landing.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20051026X01726. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.