Bell 206B accident near Rockport, Washington, September 12, 2016
On September 12, 2016 at about 8:45 pm local time, a 1993 Bell 206B (helicopter), registered N6181A, was substantially damaged in an accident during standing (engine(s) operating) near Rockport, Washington. It was an external-load flight under public-use (government) rules. No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to maintain helicopter control while on the ground, which resulted in mast bumping.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- September 12, 2016 · about 8:45 pm local time
- Place
- Rockport, Washington · map
- Type
- Accident
- Injuries
- No one was hurt; 2 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Bell 206B III, built 1993 · all 206Bs on the register
- Registration
- N6181A · registry record · serial 4277
- Damage
- Substantial damage
- Flight
- External-load flight · public-use (government) rules
The NTSB's narrative final · quoted from the NTSB record
The commercial pilot reported that, after landing the helicopter on a flat area in remote, mountainous terrain, she reduced the throttle to the idle position and the left front seat passenger exited the helicopter. The pilot reported that, while the passenger was securing the door, the helicopter started to oscillate laterally. The pilot adjusted the flight controls and increased the throttle, and the lateral oscillations stopped. The passenger stated that the helicopter "bounced and lurched" while he was securing the door but that the tail rotor did not come in contact with any objects or terrain. The pilot subsequently shut down the engine and conducted a postflight inspection, which revealed substantial damage to the transmission system. The pilot stated there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. Damage observed on the pylon mount assembly and main rotor mast was consistent with a mast bumping event, during which the static stops contact the mast due to excessive rotor blade flapping. During ground operations with the rotor turning, the main rotor may be affected by wind gusts and flap to its limits, resulting in a light static stop-to-mast contact. In such an event, mast bumping may manifest itself as a light shudder felt throughout the helicopter. The more extreme the flapping, the more severe the shudder. Mast bumping can also occur during ground operation if the cyclic is incorrectly positioned or is moved sufficiently to tilt the rotor disc to an extreme position.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Miscellaneous/other during standing (engine(s) operating) defining event
- Attempted remediation/recovery during standing (engine(s) operating)
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: instructor: helicopter; instructor: instrument helicopter; instrument: helicopter; rotorcraft: helicopter
- Flight time: 3,239 hours in all; 863 in this make and model; 75 in the last 90 days; 30 in the last 30 days; 3,090 as pilot in command; 1,716 on instruments
- Last flight review: May 12, 2016
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: rgt
- Injury: no injuries
The aircraft
- Airframe total time: 7,513 hours
- Last inspection: 100-hour inspection, August 8, 2016
- Maximum gross weight: 3,350 lb
- Seats: 5
- Landing gear: fixed
- Engine: Rolls Royce 250-C20 R4 (turboshaft); 7,368 hours total
- Operator: Hi Line Helicopters, Inc.
The flight
- Departed from: Rockport WA at 8:30 pm
- Destination: Rockport WA
Weather at the time
- Light: daylight
- Wind: from 340° at 6 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 75°F (24°C), dew point 36°F (2°C)
- Altimeter: 30.17 inHg
- Observation at 8:53 pm from KBLI, 55 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
9 documents, released by the NTSB on September 14, 2017. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 - Doi Oas | PDF, 9 pages | View Download |
| 2 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 - Operator | PDF, 9 pages | View Download |
| 3 | Pilot's Statement | PDF, 1 page | View Download |
| 4 | Passenger's Statement | PDF, 1 page | View Download |
| 5 | Doi Oas Inspection Report | PDF, 3 pages | View Download |
| 6 | Repair Station Examination Report | PDF, 16 pages | View Download |
| 7 | Pylon Mount Log Book Entry | PDF, 1 page | View Download |
| 8 | Statement of Party Representatives to NTSB Investigation | PDF, 3 pages | View Download |
| 9 | Photos | PDF, 8 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
