Accident Eurocopter AS-350-B2 N311TV,
ASN logo
ASN Wikibase Occurrence # 385892
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Friday 18 May 2001
Time:09:25 LT
Type:Silhouette image of generic AS50 model; specific model in this crash may look slightly different    
Eurocopter AS-350-B2
Owner/operator:U.S. Helicopters Inc.
Registration: N311TV
MSN: 3024
Year of manufacture:1994
Total airframe hrs:1790 hours
Engine model:Turbomeca Arriel 1D1
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Houston, TX -   United States of America
Phase: Approach
Nature:Executive
Departure airport:Houston-Sugar Land Regional Airport, TX (SGR/KSGR)
Destination airport:Houston, TX (66TS)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The helicopter was on final approach, approximately 15 feet above the roof top helipad, when the helicopter's controls "became very stiff." The pilot observed the "HYD" light on the caution panel illuminated; however, the audible hydraulic warning horn did not activate. Subsequently, the helicopter impacted the helipad with the right skid, and rolled onto its right side. Examination of the helicopter's cockpit revealed that the hydraulic cut-off switch, which is located on the collective control, was found in the cut-off position and its red plastic guard was broken (when the switch is in the cut-off position the hydraulic warning horn will not sound). The cockpit was examined for shattered pieces of the guard; however, none were found. The hydraulic system was examined and no leaks were noted. A functional test of the hydraulic pump and regulator/manifold revealed no anomalies with either unit.

Probable Cause: the failure of the pilot to maintain control of the helicopter following an inadvertent deactivation of the hydraulic system, during final approach. A contributory factor was the unguarded hydraulic cut-off switch.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: FTW01LA121
Status: Investigation completed
Duration: 4 months
Download report: Final report

Sources:

NTSB FTW01LA121

Location

Revision history:

Date/timeContributorUpdates
05-Apr-2024 08:58 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org