WPR25FA213 · Scott Macwilliam SR3500 MOOSE
Scott Macwilliam SR3500 MOOSE · Accident: loss of engine power (total) en route
From Sekiu Airport (11S) to an unrecorded destination
Event
- NTSB case
- WPR25FA213
- 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
- Ongoing
- API-reported fatalities
- 1 · 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
- Not recorded
Scott Macwilliam SR3500 MOOSE
- Aircraft type
- Scott Macwilliam SR3500
- 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
- N80TM
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Sekiu Airport (11S), Sekiu, WATo not recorded
- Aircraft age
- About 14 years (built 2011)
- 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
- Defining eventThe 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
- Loss of engine power (total)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
No findings designated as a cause are recorded in the NTSB data yet.
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
On July 15, 2025, at about 1440 Pacific daylight time, an experimental amateur-built Murphy Moose SR3500 airplane, N80TM, sustained substantial damage when it was involved in an accident near Quinault, Washington. The pilot received minor injuries, one passenger received serious injuries, and one passenger was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the airplane’s records, it had originally been constructed in Canada with a Vedeneyev M14P radial engine. In November 2023, it was imported to the United States and was altered to accommodate the installation of a Pratt & Whitney Canada T-74 (PT6A-20) engine. The pilot subsequently purchased the airplane in September 2024. The airplane was based at Olympia Regional Airport (OLM), Olympia, Washington. On the morning of the accident, the pilot did not note any anomalies with the airframe or engine during his preflight inspection. The pilot and passengers boarded the airplane, and flew to Sekiu Airport (11S), Sekiu, Washington. After having lunch in Sekiu, they departed for the return flight to OLM. (See Figure 1).
Figure 1: The airplane’s flight path and the location of the accident site, depicted in the yellow inset. According to the pilot, about 20 minutes after departure from 11S, the engine sound changed, and the engine began to exhibit a “weird vibration.” Shortly thereafter, the Master Caution light on the instrument panel illuminated, and the engine experienced a total loss of power. When the pilot realized he would not be able to glide the airplane to a nearby lake, he extended the flaps slow the airplane in anticipation of the forced landing. The airplane subsequently impacted densely forested, mountainous terrain within Olympic National Park. (See Figure 2).
Figure 2: An aerial photograph of the accident site. (Courtesy of the US Navy). The pilot reported he lost consciousness during the accident and did not regain consciousness until hours later. After removing the passengers from the airplane, the pilot manually activated the Emergency Locator Transmitter (ELT) and called 911. According to records provided by the National Park Service, the Olympic Park Dispatch was notified of the call at about 1840. The accident site was determined to be unreachable by foot, and at about 1915, a rescue helicopter from Naval Air Station Whidbey Island was dispatched to recover the airplane occupants. At about 2204, dispatch was notified that the airplane occupants had been hoisted into the rescue helicopter by long line. The wreckage has been retained for further examination.
Verbatim NTSB factual narrative from the NTSB dataset
Sources
NTSB record WPR25FA213
- Event ID
- 20250716200553
- Case number
- WPR25FA213
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
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: 34b2caa2b61c1bfaa856a69bc67c215177e796777d6947cb85f2c3a67302409e; retrieved 2026-09-15T09:06:48.020Z.