ASN Wikibase Occurrence # 285392
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: | Monday 22 December 2008 |
| Time: | 16:04 LT |
| Type: |  Bell 407 |
| Owner/operator: | JBI Helicopter Services, Inc. |
| Registration: | N407GB |
| MSN: | 53584 |
| Year of manufacture: | 2003 |
| Total airframe hrs: | 889 hours |
| Engine model: | Rolls-Royce 250-C47B |
| Fatalities: | Fatalities: 0 / Occupants: 1 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Bow, New Hampshire -
 United States of America
|
| Phase: | En route |
| Nature: | Ferry/positioning |
| Departure airport: | Danielson Airport, CT (KLZD) |
| Pembroke, NH (NH33) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
Two days before the accident, the helicopter landed at an airport due to en route snow. On the day of the accident, company personnel spent about 5 hours cleaning and deicing it. The pilot subsequently conducted multiple ground and air taxi runs before departing toward his home heliport. About 45 minutes into the flight, when the helicopter was about 900 feet over tree-covered terrain, the engine lost power. The pilot then performed an approximately 180-degree autorotation to a curved street. The helicopter landed hard and sustained substantial damage to the fuselage. Prior to the loss of engine power, the pilot did not observe any caution or warning lights, and the FADEC (Full Authority Digital Engine Control) remained in the automatic mode. The pilot also noted no unusual noises or yawing of the helicopter prior to the loss of engine power. A subsequent download of the helicopter's incident recorder revealed "Engine Flameout," "Nr Droop," and "Ng Exceedance Low" faults. It also indicated that when the flameout detection occurred, "Fuel Enable" and "Auto Relight" functions became active. Subsequent examinations of the airframe, including the fuel supply system, revealed no anomalies that would have resulted in a flameout. The electronic control unit was downloaded, with no faults noted. The electronic control unit and the hydro mechanical unit were examined with no anomalies noted. The engine was mounted in a test cell and successfully run with no discrepancies noted. During a later engine test run, the fuel was intentionally shut off through a solenoid, and except for rotor rpm, the incident recorder indicated the same faults as noted in the accident sequence, confirming that the loss of engine power likely occurred due to an interruption of fuel flow for undetermined reasons.
Probable Cause: An interruption of fuel flow for undetermined reasons, which resulted in an engine flameout.
Accident investigation:
 |
|
Sources:
NTSB ERA09LA105
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 02-Oct-2022 09:09 | ASN Update Bot | Added |
Corrections or additions? ... Edit this accident description
The Aviation Safety Network is an exclusive service provided by:
Quick Links:
| ASN Home | Send Correction / Feedback |
| FSF Home | Disclaimer | Copyright |
| Contact Us | Privacy Policy |
| Press / Media |
CONNECT WITH US:
©2024 Flight Safety Foundation