Bell 206B N34698
17 August 2004 · Mead, Washington, United States · Fatal
Summary
On 17 August 2004 at about 16:40 local time, a Bell 206B registered N34698 was involved in an accident near Mead, Washington, United States. One person was on board and one died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 16:40
- Classification
- Accident
- Location
- Mead, Washington, United States
- Coordinates
- 47.7889, -117.3494
- Aircraft
- Bell 206B
- Registration
- N34698
- Category
- Helicopter
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 133: Rotorcraft Ext. Load
- Purpose of flight
- Public Use
- Phase of flight
- Not recorded
- Route
- Spokane → Mead
- Aircraft damage
- Destroyed
- Weather
- VMC
- Light
- Day
- NTSB number
- SEA04TA163
People
1 person died.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 1 | 1 | 0 | 0 | 0 |
Probable cause
The reversal of the reel machine during a sock line pull which resulted in a loss of control while hovering out of ground effect. Factors were the failure of company management to develop adequate procedures for conducting sock line pulls, the inadequate communication between the chief pilot and the pilot, the inadequate communication between the ground personnel and the pilot, and the pilot's lack of recent experience in Class C external load operations.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
The helicopter was pulling sock line (rope) that was to be used to install a static wire at the top of 220-foot-tall towers supporting a 500-kV power line. (The stringing of sock line is a Class C external load operation, meaning an operation in which the external load is jettisonable and remains in contact with land or water during the rotorcraft operation.) The sock line was attached to the helicopter's remote cargo hook and played out of a truck mounted reel machine operating in the power payout mode. The reel machine operator stated that "suddenly the rope wrapped over another rope or pulled down in the drum, causing the rope to reverse on the drum." The reel machine operator immediately moved the machine's shift lever from "OUT" to "NEUTRAL," but by the time he had accomplished this, the rope between the reel and the helicopter went taut. Numerous witnesses, who were all members of the line crew installing the wires, reported that when the rope went taut, the helicopter pitched up and rolled right. The helicopter descended, impacted the ground and came to rest on its right side. Post-accident interviews revealed that the pilot, the line crew, and company management did not adequately recognize and mitigate the risks inherent in the procedures they were using to conduct the sock line pull. Specifically, the rigging used was a 25-foot long line with a 31-pound ballast weight, while other operators pulling sock line use longer long lines (50 to 100 feet) and heavier ballast (150 to 300 pounds) in order to provide pilots with an earlier warning of an impending shock load due to a snag so that the pilot will have more time to respond. Additionally, at the pilot's request, the reel machine was being operated in the power payout mode, instead of the free wheeling mode. This was due to a miscommunication between the pilot and the chief pilot, who stated that when he discussed the operation with the pilot, he assumed the pilot understood that he intended for the reel to be freewheeling. In the freewheel mode, when a snag occurs, at worst, the reel stops. In the power payout mode, when a snag occurs, the line can double back on the reel and begin to pull back in, as occurred in this accident. Also, while preparing for the sock line pull, the line crew was paying out sock line on the ground and experienced a snag, which resulted in the line being pulled in instead of paying out, just as occurred in the accident. However, there was no communication of this occurrence to the pilot. Finally, although the pilot had 21,803 hours rotorcraft flight time, 16,000 hours in the accident make and model helicopter, and 4,000 hours conducting external load operations, his most recent Class C external load experience was 5 years and 3 months prior to the accident.
Quoted verbatim from the NTSB record.
Other Bell 206 accidents
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 27 Jun 2004 | Bell 206B | Cushing, Oklahoma, United States | - | Fatal | 2 |
| 24 Jun 2004 | Bell 206-L1 | Vermillion Bay, Louisiana, United States | American Helicopters, Inc. | Fatal | 3 |
| 16 Aug 2004 | Bell 206B | Kahului, Hawaii, United States | - | Minor injuries | - |
| 26 Jan 2004 | Bell 206B | Turner, Oregon, United States | - | No injuries | - |
| 20 May 2004 | Bell 206L-3 | Palmdale, California, United States | Orbic Helicopters | Minor injuries | - |
| 28 Jan 2004 | Bell 206-L4 | Patterson, Louisiana, United States | - | No injuries | - |
All 1,732 records for this type
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 5 Sep 2004 | Piper PA-18 | Blaine, Washington, United States | Guy R and Tyler R Glahn | Minor injuries | - |
| 1 Aug 2004 | Cessna 150C | Mazama, Washington, United States | - | Serious injuries | - |
| 3 Sep 2004 | Hardin LANCAIR 320 | Chewelah, Washington, United States | - | Minor injuries | - |
| 16 May 2004 | Stinson SR-10E | Eliza Island, Washington, United States | - | No injuries | - |
| 16 Jul 2004 | Cessna 150L | La Center, Washington, United States | - | Minor injuries | - |
| 21 Mar 2004 | Cessna 172E | Raymond, Washington, United States | - | No injuries | - |