Hard landing Accident Eurocopter AS 350B2 N632SD,
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ASN Wikibase Occurrence # 278542
 
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Date:Wednesday 15 September 2021
Time:10:50 LT
Type:Silhouette image of generic AS50 model; specific model in this crash may look slightly different    
Eurocopter AS 350B2
Owner/operator:County of Oakland
Registration: N632SD
MSN: 3519
Year of manufacture:2002
Total airframe hrs:6357 hours
Engine model:Turbomeca Arriel 1D1
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Romeo, Michigan -   United States of America
Phase: En route
Nature:Training
Departure airport:Lapeer, MI (D95)
Destination airport:Romeo, MI
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The flight instructor reported that he intended to demonstrate to the student pilot a 180° autorotation with a power recovery near the ground. He planned to transition the helicopter into to a hover about 5 to 10 ft above ground level at the end of the maneuver. The instructor initially set the engine fuel control to the idle detent to simulate an engine failure and then entered an autorotation. As the autorotation progressed, the flight instructor repositioned the engine fuel control, but he failed to ensure that it had been placed into the flight detent. Without sufficient engine power at the end of the maneuver, the helicopter continued to descend with a low rotor speed, landed hard, and slid to a stop on the runway. Then the helicopter violently rocked side to side before the main rotor stopped rotating. During the accident sequence, the helicopter sustained substantial damage to a main rotor Starflex arm and the tail rotor driveshaft. Both the flight instructor and his student reported there were no mechanical malfunctions or failures of the helicopter that would have precluded normal operation.

Probable Cause: The flight instructor's failure to reposition the fuel control to the flight detent during a practice autorotation, which resulted in insufficient engine power to arrest the helicopter's decent and a hard landing.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN21LA431
Status: Investigation completed
Duration: 8 months
Download report: Final report

Sources:

NTSB CEN21LA431

Location

Revision history:

Date/timeContributorUpdates
31-May-2022 17:17 ASN Update Bot Added

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