WPR09LA052 · Adkins Ridge Runner II
Adkins Ridge Runner II · Accident: loss of control in flight during initial climb
From Portland Mulino Airport (4S9) to Portland Mulino Airport (4S9)
Event
- NTSB case
- WPR09LA052
- 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
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- 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
Adkins Ridge Runner II
- Aircraft type
- Adkins RIDGE RUNNER
- 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
- N825PB
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Portland Mulino Airport (4S9), Mulino, ORTo Portland Mulino Airport (4S9), Mulino, OR
- 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
- Initial climb
- 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 control in flight
- 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
- Aircraft › Aircraft oper/perf/capability
- Personnel issues › Task performance
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The pilot had recently purchased the amateur-built experimental airplane and received operating limitations from the Federal Aviation Administration for flight testing of the airplane. On the day of the accident, the pilot first performed taxi tests and then began taking off, climbing to about 10 feet above the ground, reducing power and landing back on the runway. The pilot completed a few of these runs and then taxied back onto the runway for another run. He advanced the throttle and noted that the tachometer only went to 4,000 rpm. The airplane lifted off the runway and climbed to about 150 feet above the ground. The pilot said it would not "climb higher or speed up." The airspeed was reading about 45 to 50 knots. The pilot started looking for a place to land and seeing obstacles ahead and to the left, he executed a shallow right turn back towards the airfield. The airplane stalled without notice and the pilot was not able to recover prior to ground impact. The airplane came to rest in a nose down position in a flat grassy field. The engine was displaced rearward, and the forward portion of the fuselage was crushed and compressed aft. The pilot reported that he had accumulated 240.7 hours total flight time of which 0 hours were in the accident make and model airplane. Following the accident, the propeller was found to be in "high pitch preventing the engine from turning up to more than 4,000 rpm, limiting the horsepower."
Probable cause
The pilot's failure to attain an adequate airspeed that resulted in a stall/mush during the initial climb. Contributing to the accident were the pilot's lack of experience in this make and model airplane and the improper adjustment of the propeller pitch.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record WPR09LA052
- Event ID
- 20081201X45441
- Case number
- WPR09LA052
- 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, coordinates. 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: e4cf6577a8486199e0845553ac86c1381f6a690e2862320852c25488d58cd94d; retrieved 2026-09-15T10:35:05.650Z.