Accident Robinson R22 Beta N74536,
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ASN Wikibase Occurrence # 284626
 
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Date:Monday 9 July 2007
Time:09:10 LT
Type:Silhouette image of generic R22 model; specific model in this crash may look slightly different    
Robinson R22 Beta
Owner/operator:Rotorspins LLC
Registration: N74536
MSN: 3892
Year of manufacture:2005
Engine model:Lycoming O-360-J2A
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Albuquerque, New Mexico -   United States of America
Phase: Unknown
Nature:Training
Departure airport:Albuquerque-Double Eagle II Airport, NM (KAEG)
Destination airport:Edgewood, CO (1N1)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The student pilot, he was on a solo cross country flight. Prior to departure from a local airport, he refueled the helicopter with 15 gallons of fuel. After departure, the helicopter headed north, turned to the east, and then turned to a southerly direction. While in cruise flight at 6,800 feet mean sea level (msl), the student reported that the helicopter began losing altitude. In an attempt to recover the altitude, the student increased collective and reduced forward airspeed. At 1,000 feet above ground level and airspeed of 50 to 60 knots, the student further increased the collective and the helicopter "pitched, then turned rapidly to the right." The student partially lowered the collective and did not attempt to use the pedals to stop the turn as the helicopter continued to lose altitude. After the helicopter rotated approximately 160 degrees to the right, the helicopter "stopped or slowed turning." While heading in a northerly direction, the student then noticed a radio tower in front of the helicopter and applied right cyclic to avoid the tower. The student attempted to land the helicopter to a parking lot. During the attempted landing, the helicopter contacted power lines, impacted the parking lot, and came to rest on its left side. Examination of the helicopter revealed no anomalies with the airframe or engine. The calculated density altitude for the weather conditions at the time of the accident was approximately 9,600 feet.

Probable Cause: The pilot's failure to maintain aircraft control during an encounter with the loss of tail rotor effectiveness. Contributing factors were the high density altitude and the power lines.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: DEN07CA115
Status: Investigation completed
Duration: 1 month
Download report: Final report

Sources:

NTSB DEN07CA115

Revision history:

Date/timeContributorUpdates
30-Sep-2022 19:30 ASN Update Bot Added

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