Smith, Ted Aerostar AEROSTAR 601P accident near Klammath Falls, Oregon, April 27, 1997
On April 27, 1997 at about 7:45 pm local time, a Smith, Ted Aerostar AEROSTAR 601P, registered N30LL, was substantially damaged in an accident near Klammath Falls, Oregon. It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to set the throttle of his second failed engine to 'Cracked-1/2-Open' as called for in the Engine Failure/Restart checklist, followed by a high-power engine surge. Factors include the pilot's delay in landing for refueling, the pilot becoming lost/disoriented, drug impairment, and fuel exhaustion.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- April 27, 1997 · about 7:45 pm local time
- Place
- Klammath Falls, Oregon · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Smith, Ted Aerostar AEROSTAR 601P AEROSTAR 6
- Registration
- N30LL · registry record · serial 61P-0379-1
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
About three hours and twenty minutes after departing Bellingham, Washington, for Midland, Texas, the pilot contacted Klamath Falls (Oregon) Tower and told the controller of his intention to land. About 10 minutes later, while about 30 miles north of Klamath Falls, the pilot reported he was low on fuel and was not able to find the city. The tower responded with instructions that would take the pilot south to the airport. But because the pilot seemed not to be following the instructions, but was instead continuing to the west, he was switched to Seattle Center. Center provided the pilot with a southeasterly heading direct to Klamath Falls, but less than a minute later radar and radio contact with the aircraft was lost. Other pilots overheard the pilot transmit that he had lost power in one engine, and later state that he had lost power in both. Soon thereafter the aircraft was seen to descend to about 200 to 300 feet above the surface of Lake of the Woods. The aircraft then began to slow and its nose began to rise. As it was slowing, one of the engines surged back to a high power setting, and the aircraft almost immediately rolled quickly to the side and dove nearly straight down into the lake. During the post-accident inspection of the airframe, the throttle for the right engine was found retarded to idle, but the throttle for the left engine was found in the full-forward (maximum power) position. A review of the Aerostar owner's manual revealed that the Engine Failure/Restart checklist called for the throttle for a failed engine (both engines in this case) to be retarded to the 'Cracked 1/2 inch open' position. Toxicological results indicate the presence in the pilot's blood of chlordiazepoxide and three of its active metabolites, norchlordiazepoxide, nordiazepam, and oxazepam. Chlordiazepoxide (Librium) is a tranquilizer often used to treat anxiety and tension. At sufficient levels it can have significant adverse effects on judgement, alertness, and performance. It is known to cause drowsiness, mental dullness, and euphoria. The results also indicate the presence of diphenhydramine in the pilot's blood. Diphenhydramine is a sedating antihistamine, and in sufficient quantities is known to produce drowsiness, impaired coordination, blurred vision, and reduced mental alertness.
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: private
- Ratings: multi-engine land; single-engine land
- Flight time: 6,550 hours in all
- Medical certificate: Class 3 (valid medical--w/ waivers/lim.)
- Seat: left
The aircraft
- Airframe total time: 4,000 hours
- Last inspection: annual inspection, July 1, 1996
- Maximum gross weight: 6,000 lb
- Seats: 6
- Landing gear: retractable
- Engine: Lycoming IO-540-S1A5 (piston); 0 hours total
The flight
- Departed from: BLI Bellingham WA at 4:23 pm
- Destination: MDD Midland TX
- Flight plan: none
- Runway 0
Weather at the time
- Light: daylight
- Wind: from 240° at 4 knots
- Visibility: 30 statute miles
- Sky: clear
- Temperature: 55°F (13°C), dew point 0°F (-18°C)
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Crew | 1 |
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.
