Accident Robinson R22B N2328W,
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ASN Wikibase Occurrence # 355868
 
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Date:Friday 16 May 1997
Time:15:00 LT
Type:Silhouette image of generic R22 model; specific model in this crash may look slightly different    
Robinson R22B
Owner/operator:White Cloud Aviation
Registration: N2328W
MSN: 2129
Year of manufacture:1992
Total airframe hrs:954 hours
Engine model:Lycoming O-320-B2C
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Boise, ID -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Unknown
Departure airport:(KBOI)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The student pilot was on a checkride for a private pilot certificate with an FAA operations inspector acting as a check pilot. The check pilot stated that he had asked the student to demonstrate a hovering autorotation. Their procedures were discussed before starting the maneuver. The check pilot noted that the student stated that on the count of three, he would start the maneuver by rolling the throttle off first. The check pilot stated that as he was adjusting himself on the seat, at the count of one, the applicant rolled the throttle partially off, induced right pedal as hard as he could and pulled on the collective as quickly as he could. The check pilot noted that during the maneuver, the engine returned to full power because of the corrolator. The helicopter then climbed to approximately 15 feet and started to spin. The check pilot said that by then, he was on the controls and was asking the applicant to let go. He stated that the student pilot froze on the controls during the maneuver and refused to let go. After approximately eight or nine spins, he was unable to maintain control of the helicopter, with the applicant still at the controls at the time of the crash.

Probable Cause: improper handling of the helicopter by the student pilot/applicant, during a hover autorotation, which resulted in loss of tail rotor effectiveness. The check pilot's inadequate remedial action was a related factor.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: SEA97LA115
Status: Investigation completed
Duration: 1 year
Download report: Final report

Sources:

NTSB SEA97LA115

Location

Revision history:

Date/timeContributorUpdates
12-Mar-2024 16:31 ASN Update Bot Added

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