Bell 206B accident near Rainier, Washington, June 25, 2002
On June 25, 2002 at about 10:56 pm local time, a Bell 206B (helicopter), registered N1087L, was substantially damaged in an accident near Rainier, Washington. It was a public-use flight under public-use (government) rules. No one was hurt; 3 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 aircraft control while trying to land. Rough/uneven terrain, inaccurate performance data calculations, inadequate in-flight planning and lack of familiarity with the geographic area were factors.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 25, 2002 · about 10:56 pm local time
- Place
- Rainier, Washington · map
- Type
- Accident
- Injuries
- No one was hurt; 3 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Bell 206B · all 206Bs on the register
- Registration
- N1087L · no longer on the register · serial 3004
- Damage
- Substantial damage
- Flight
- Public-use flight · public-use (government) rules
The NTSB's narrative final · quoted from the NTSB record
The pilot reported that he was dispatched to Mount Rainier to provide air support for a rescue mission of an injured hiker. Load calculations prepared by the pilot indicated that the helicopter would be operating at the high end of its performance capabilities. The pilot also reported that this was his first time operating on Mount Rainier. After a briefing, the pilot took one climbing guide from one helibase, and then picked up a climbing ranger from another location before proceeding to the site where the injured hiker was located at about the 10,000 to 10,400 foot level. Since the pilot was unfamiliar with the mountain, the guide and ranger also provided assistance to the pilot in where to go. The pilot was to drop off the guide and ranger at about the 9,000 foot level. After flying over the site to survey the ground conditions on the glacier which consisted of crevasses and uneven ground from avalanche debris, and to check helicopter performance, the pilot attempted to land at several locations on the glacier between about 8,000 feet and 9,000 feet. The pilot then chose a location in which he positioned the helicopter nose into the slightly rising terrain. The climbing ranger stated that the landing skid from the aft cross tube forward was on the ground. The terrain from the aft cross tube back sloped down about 5 degrees. After the pilot set the helicopter down slowly on the ground, he used the pedals to test for compaction. The pilot stated that as he was lowering the collective, the helicopter suddenly pitched and he applied forward cyclic and lifted off the ground. The helicopter began to rotate clockwise. The pilot applied left pedal input which did not have any effect. The pilot realized that he had no tail rotor control and lowered the collective and impacted on the glacier with the nose pointing downhill. Both occupants on board the helicopter and one witness located about 500 feet above the accident site reported that after the helicopter set down, it appeared to them that the helicopter slid backwards which lowered the tail and raised the nose of the helicopter. The witness above the accident site stated that he thought that the pilot would have landed perpendicular to the terrain slope so that the skids would not act like skis when weighted and slide downhill. Prior to recovery of the helicopter from the glacier, it was lost in a crevasse and covered by snow and rock fall. The load calculation prepared by the pilot was reviewed after the accident. It was found that for the actual conditions at the accident site, the helicopter was operating from 60 to 285 pounds over its allowable load for hover out of ground effect performance.
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
Pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instructor: glider; instructor: helicopter; instrument: airplane; rotorcraft: glider; rotorcraft: helicopter
- Flight time: 6,851 hours in all; 862 in this make and model; 110 in the last 90 days; 62 in the last 30 days; 6,700 as pilot in command; 840 on instruments
- Last flight review: February 15, 2002
- Medical certificate: Class 2 (valid medical--no waivers/lim.)
- Seat: rear
- Injury: no injuries
The aircraft
- Maximum gross weight: 3,200 lb
- Seats: 4
- Landing gear: fixed
- Engine: Allison 250-C18 (turboshaft); 0 hours total
The flight
- Departed from: Camp Schurman WA at 10:40 pm
- Destination: Mt. Rainier WA
Weather at the time
- Light: daylight
- Wind: at 6 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 77°F (25°C), dew point 48°F (9°C)
- Altimeter: 30.17 inHg
- Observation at 10:56 pm from SMP, 30 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Crew | 1 | |||
| Passengers | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
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.
