No fatalities

Practice Autorotation Leads to Engine Failure and Substantial Damage for Robinson R44 Near Grants, New Mexico (N7523S)

Grants, NM, United States

On May 10, 2012, a ROBINSON HELICOPTER COMPANY R44 II (registration N7523S) operated by iPrerogative, Inc was involved in an aviation accident near Grants, NM. No fatalities were reported. Investigators recorded the probable cause as: The loss of engine power due to an excessively rich fuel mixture that occurred during operations at idle power settings at a high density altitude. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 2026-08-03Data APIEditorial standards

On May 10, 2012, a Robinson R44 II helicopter experienced an engine power loss during a practice autorotation near Grants, New Mexico. The occupants were uninjured but the helicopter sustained substantial damage.

Incident Overview

On May 10, 2012, at approximately 1015 mountain daylight time, a Robinson R44 II helicopter, registration N7523S, performed an autorotation following a loss of engine power near Grants, New Mexico. The flight was conducted under 14 Code of Federal Regulations Part 91 as a positioning flight, operated by iPrerogative Inc. of Washington, Utah. Visual meteorological conditions prevailed, and the flight operated on a visual flight rules flight plan. The helicopter had departed the Albuquerque International Airport (KABQ), Albuquerque, New Mexico, about 0900, and was destined for Page Municipal Airport (KPGA), Page, Arizona.

Flight Crew and Injuries

The helicopter was occupied by a certificated flight instructor (CFI) and a commercial pilot. Neither occupant was injured.

Sequence of Events

According to a statement from the CFI, while cruising over mountainous terrain at 10,000 feet mean sea level (msl), the CFI slowed the helicopter to 70 knots and initiated a practice autorotation to maintain autorotation proficiency. The pilot reported checking 80 percent engine rpm at least twice during the maneuver. At approximately 9,200 feet msl (about 600 feet above ground level), the CFI attempted to restore engine power, but the engine had ceased producing power, as verified by the engine tachometer. The pilot continued the autorotation, lined up with the best available landing area, and landed. Upon touchdown, the helicopter’s main rotor blade contacted the tail boom, severing it. Substantial damage was sustained to the main rotor blades, tail boom, and tail rotor blades.

Postaccident Examination

A postaccident engine run was conducted by the National Transportation Safety Board and a technical representative from Lycoming Engines. The engine started and ran for several minutes; however, it occasionally ran rough at idle power with a full rich mixture setting. Leaning the fuel mixture via the cockpit mixture control improved engine performance. The density altitude at the time of the engine run was approximately 8,100 feet.

Maintenance History

A review of maintenance records revealed that maintenance work was performed in Florida at an altitude of 100 feet mean sea level. Any adjustment to the fuel control unit, which sets the idle mixture, would have been set at this altitude by maintenance personnel.

Contributing factors

Causes

Related operating info

Other contributing factors

Instructor/check pilotAbility to respond/compensate

Frequently asked questions

What happened in the 10 May 2012 ROBINSON HELICOPTER COMPANY R44 II accident near Grants, NM?

On May 10, 2012, a Robinson R44 II helicopter experienced an engine power loss during a practice autorotation near Grants, New Mexico. The occupants were uninjured but the helicopter sustained substantial damage.

Were there any fatalities in the 10 May 2012 ROBINSON HELICOPTER COMPANY R44 II accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 10 May 2012 involved a ROBINSON HELICOPTER COMPANY R44 II, registration N7523S, operated by iPrerogative, Inc, at Grants, NM.

What was the probable cause of the accident?

The loss of engine power due to an excessively rich fuel mixture that occurred during operations at idle power settings at a high density altitude. Contributing to the accident was the flight instructor’s poor decision-making in choosing to practice an unnecessary autorotation over mountainous terrain.