ANC97FA031 · Buesing SX-300
Buesing SX-300 · Accident: partial loss of engine power (non-mechanical) en route
From Ketchikan International Airport (KTN) to Soldotna Airport (SXQ)
Event
- NTSB case
- ANC97FA031
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 2 · all aircraft and ground
- Ground fatalities
- 0
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Buesing SX-300
- Aircraft type
- Buesing SX-300
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N357SX
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Ketchikan International Airport (KTN), Ketchikan, AKTo Soldotna Airport (SXQ), Soldotna, AK
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · cruise
- First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Partial loss of engine power (non-mechanical)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Destroyed
Cause areas
- Induction air control, alternate air/door › Closed
- Pilot in command › Procedures/directives, not complied with
- Pilot in command › Weather evaluation, inadequate
- Ram/induction air › Open
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The homebuilt airplane was being operated as an IFR cross-country flight over mountainous/coastal terrain. While cruising at 14,000 ft, about 19 miles from the nearest airport, the pilot encountered a low engine power condition. He declared an emergency, & was given vectors to the airport. The airplane was capable of gliding about 24 miles from 14,000 ft, but was ditched in the ocean, about 5 miles from the airport. The occupants did not egress from the airplane before it sank. The airplane engine had a ram air/alternate air box attached to the fuel control servo which controlled the engine air source. Ram air was unheated & unfiltered, & was to be used when operating in clear/dry air conditions. Alternate air was heated & filtered, & was to be used during an engine emergency, takeoff & landing, when flying in dusty air, or when in conditions where inlet icing could be expected (visual moisture & temperatures of 40 deg F or below). The airplane's air control was found in the ram air position. Weather conditions near the accident site included a temperature & dew point of 35 deg with snow & ice pellets. Upper air conditions along the route of flight included temperatures between -28 to -45 deg C, & humidity levels between 69 & 81 percent. An AIRMET had been issued for the area. It included a caution for light & temporary moderate icing in clouds & in precipitation from 1,000 ft to 12,000 ft. The freezing level was 1,000 ft. The pilot was provided a PIREP that indicated a trace of ice had been encountered in the area.
Probable cause
the pilot's failure to properly evaluate the presence of icing conditions, and his failure to comply with procedures to use alternate engine air in icing conditions. Factors relating to the accident were: icing (weather) conditions, the pilot's improper application of emergency procedures to maximize available glide distance, and the lack of suitable terrain for a forced landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ANC97FA031
- Event ID
- 20001208X07467
- Case number
- ANC97FA031
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 06fc87bfd247343d64cf2488015f24cc99b7a7f9fe87f662b9be00e7b508558b; retrieved 2026-09-20T23:01:55.589Z.