CEN09FA462 · Beech V35 B
Beech V35 B · Accident: loss of engine power (total) en route
From Wiley Post Airport (PWA) to Enid Woodring Regional Airport (WDG)
Event
- NTSB case
- CEN09FA462
- 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
- 1 · 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
Beech V35 B
- Aircraft type
- Beechcraft 35
- 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
- N9112S
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Wiley Post Airport (PWA), Oklahoma City, OKTo Enid Woodring Regional Airport (WDG), Enid, OK
- 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 · climb to cruise
- 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
- Aircraft › Aircraft power plant
- Not determined › Not determined
- Personnel issues › Action/decision
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The airplane had a previous history of in-flight engine stoppages, and the engine lost power twice within the week before the accident. The pilot did not have his mechanic investigate the cause of those events, as he believed when the engine lost power the airplane was in a fuel cross feed position, and all he had to do was to switch to a main fuel tank. On the day of the accident the airplane was two miles from the airport after departure when the pilot reported a loss of engine power to air traffic controllers. The pilot executed an off-airport emergency landing to a congested area, adjacent to a major six-lane thoroughfare. The airplane was substantially damaged when it impacted a tree and the concrete base of a light pole, during the emergency landing. The engine was recovered from the wreckage and installed in an engine test cell. It started on the first attempt and ran at full throttle with no anomalies noted. A postexamination of the other airplane systems showed no anomalies.
The pilot had been treated for anxiety, depression, high blood pressure, and obstructive sleep apnea, among other significant conditions. He had been on multiple medications at the time of the accident including at least an antidepressant, a blood thinner and a potentially impairing prescription medication often used for the treatment of chronic pain. The pilot denied any medical conditions or the use of medications in his most recent application for an airman medical certificate. It was not possible to conclusively determine whether distraction or impairment due to his medical conditions or to medication use may have played a role in his decision-making following the loss of engine power.
The pilot’s fatal injuries were likely a result of the impact between his chest and the control yoke. It could not be conclusively determined the extent to which the forward cabin structure and the control yoke in particular were moving aft relative to the rest of the cabin structure following the primary impact with the ground, but it is possible that the likelihood or severity of the pilot’s impact with the control yoke would have been reduced through the availability and use of a shoulder harness.
Probable cause
The pilot’s decision to operate an airplane with known deficiencies, and the loss of engine power during climb for undetermined reasons.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN09FA462
- Event ID
- 20090725X91959
- Case number
- CEN09FA462
- 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: a5a6396a4bf1e8ed6f362dcda9a467f089dcd2a26efc86c0e663ee9ce9221da3; retrieved 2026-09-13T20:23:20.879Z.