SEA99FA113 · Alexander VAN'S RV-8
Alexander VAN'S RV-8 · Accident: partial loss of engine power (mechanical failure)
From 1S4 · SCAPOOSE, OR to Independence State Airport (7S5)
Event
- NTSB case
- SEA99FA113
- 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
- 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
Alexander VAN'S RV-8
- Aircraft type
- Alexander VAN S RV-8
- 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
- N41VA
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From 1S4 · SCAPOOSE, ORTo Independence State Airport (7S5), Independence, 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
- Unknown
- 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 (mechanical failure)
- 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
- Engine assembly, connecting rod › Fatigue
- Fluid, fuel › Fire
- Pilot in command › Bail-out/emergency ejection, initiated
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
While en route during an unknown phase of operation, the O-360-A1A engine, which had been overhauled by a facility in Canada and converted with 'high compression' pistons/cylinders, developed a partial power loss after about 35 hours of total operation. Metallurgical examination revealed that the #2 connecting rod fractured in two places due to fatigue at the rod end resulting in release of the rod from the crankshaft. No evidence of engine disassembly or maintenance by the owner/builder was found. Post-crash examination revealed holes in the upper engine case and disintegration of the #1 piston. A witness reported observing the aircraft at low altitude over gently rolling terrain trailing black smoke during which the pilot was observed to exit the aircraft. The aircraft rolled into a descending right turn and impacted the terrain 600 feet from the pilot's ground impact, and a post-crash explosion and fired ensued. Reconstruction of portions of the aircraft revealed sooting and evidence of pre-impact fire forward of the firewall in the vicinity of the gascolator as well as pre-impact heat damage to the Plexiglas windscreen and canopy. The only evidence of heat/fire distress observed during post-mortem was the pilot's eyebrows and forward hairline. The aircraft's canopy is airfoil shaped and during flight conditions would tend to create an aerodynamic low pressure condition near the top of the canopy. If the canopy were opened in flight with fire conditions existing along its forward exterior surface, the entrainment of hot air and fire within the upper cockpit interior environment may have become intolerable for the pilot.
Probable cause
Fatigue of the number two connecting rod end resulting in a fracture at the rod end and release from the crankshaft, an ensuing in-flight fuel fed fire, followed by the pilot's abandoning the aircraft in flight. A contributing factor was pressure on the pilot induced by the conditions/events (in-flight fire entering the upper cockpit).
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record SEA99FA113
- Event ID
- 20001212X19358
- Case number
- SEA99FA113
- 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: ea24d0b29e365d93262d1a25aa78e2583924f5b46f7749428bdaca5ce044c9ee; retrieved 2026-09-20T21:59:18.938Z.