Bell 206B-III N22704
3 January 1989 · S.timbalier 151 · Minor injuries
Summary
On 3 January 1989 at about 18:50 local time, a Bell 206B-III registered N22704 was involved in an accident near S.timbalier 151. One person was on board and one had minor injuries. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 18:50
- Classification
- Accident
- Location
- S.timbalier 151
- Nearest airport
- S. Tim 151 (151)
- Coordinates
- Not recorded
- Aircraft
- Bell 206B-III
- Registration
- N22704
- Category
- Helicopter
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 133: Rotorcraft Ext. Load
- Purpose of flight
- Other Work Use
- Phase of flight
- Not recorded
- Route
- S.t. 151 → S.t. 151
- Aircraft damage
- Destroyed
- Weather
- VMC
- Light
- Day
- NTSB number
- FTW89LA036
People
1 person had minor injuries.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 1 | 0 | 0 | 1 | 0 |
Probable cause
A COLLISION BETWEEN THE AIRCRAFT AND THE PLATFORM DURING THE EMERGENCY AUTOROTATION WHICH CAUSED THE LEFT SKID AND FLOAT TO SEPARATE AND DESTABILIZED THE AUTOROTATION. THE COLLISION WAS PROBABLY UNADOIDABLE DUE TO THE MANEUVER THAT WAS BEING CONDUCTED AT THE ONSET OF THE EMERGENCY. THE EMERGENCY LANDING WAS ATTEMPTED FOLLOWING AN ENGINE FAILURE THAT WAS THE RESULT OF A TOTAL COMPRESSOR FAILURE. THE COMPRESSOR FAILURE WAS CAUSED BY A FATIGUE FAILURE OF THE SIXTH STAGE WHEEL WHICH SEPARATED. THE FAILURE WAS INITIATED DUE TO A CASTING INCLUSION IN THE WHEEL WHICH WAS NOT DETECTED DURING THE MANUFACTURING PROCESS.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
THE ACFT EXPERIENCED AN ENG FAILURE DURING A SLING LOAD PICK UP ON AN OFFSHORE PLATFORM. DURING THE AUTOROTATION, THE LEFT SKID AND FLOAT STRUCK A HANDRAIL ON THE RIG AND SEPARATED. THE ACFT IMPACTED THE WATER, NOSE LOW, AND ROLLED OVER AS A RESULT OF THE SEPARATED FLOAT. INVESTIGATION REVEALED THAT THE ENG FAILURE WAS A RESULT OF A 6TH STAGE COMPRESSOR WHEEL FATIGUE FAILURE. THE WHEEL FATIGUE ORIGINATED AT A CASTING INCLUSION THAT HAD NOT BEEN DETECTED DURING THE MANUFACTURING PROCESS.
Quoted verbatim from the NTSB record.
Other Bell 206 accidents
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 8 Jan 1989 | Bell 206B III | Park City, Utah, United States | Avman Inc | No injuries | - |
| 2 Jun 1989 | Bell 206L | Abbeville, Louisiana, United States | Taylor Energy Vthe | No injuries | - |
| 10 Aug 1989 | Bell 206B | Nanuet, New York, United States | Eagle Helicopter | No injuries | - |
| 2 Nov 1989 | Bell 206L-3 | Saint Paul, Minnesota, United States | Air Methods, Inc. | No injuries | - |
| 19 Aug 1989 | Bell 206B | Oak Grove, Louisiana, United States | - | No injuries | - |
| 6 Jul 1989 | Bell 206L-1 | Chiefland, Florida, United States | Kenn Aire Medical Corp. | No injuries | - |