ASN Wikibase Occurrence # 286492
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: | Thursday 8 October 2009 |
Time: | 08:00 LT |
Type: | Schweizer 269C-1 |
Owner/operator: | |
Registration: | N1835E |
MSN: | 0255 |
Year of manufacture: | 2006 |
Total airframe hrs: | 1750 hours |
Engine model: | Lycoming HIO-360-G1A |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Lewiston, Maine -
United States of America
|
Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
Nature: | Private |
Departure airport: | Auburn Airport, ME (LEW/KLEW) |
Destination airport: | Auburn Airport, ME (LEW/KLEW) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot of a helicopter was conducting a non-revenue sightseeing flight for one passenger. After lifting off, the pilot stated that he was hovering eastbound with the winds out of the west. A METAR taken on the airport approximately 5 minutes before the accident indicated the wind was from 340 degrees at 11 knots with gusts to 16 knots. The pilot further stated that the helicopter's nose made a sudden yaw to the right, which could not be corrected with reduction of throttle and full left pedal application. The helicopter touched down after a 270 degree turn, came to rest upright, with substantial damage to the main rotor blades, skids and tailboom. According to a Federal Aviation Administration Advisory Circular (AC) 90-95 titled "Unanticipated Right Yaw in Helicopters", operation of a helicopter with a tailwind as reported by the pilot or with a left quartering tailwind as determined by the METAR and the pilot's statement can result in unanticipated right yaw or loss of tail rotor effectiveness (LTE).
Probable Cause: The loss of tail rotor effectiveness (LTE) resulting from hovering the helicopter in a tailwind.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | ERA10CA010 |
Status: | Investigation completed |
Duration: | 6 months |
Download report: | Final report |
|
Sources:
NTSB ERA10CA010
Location
Revision history:
Date/time | Contributor | Updates |
03-Oct-2022 11:34 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation