LAX06CA088 · Huntington KIS
Huntington KIS · Accident: partial loss of engine power (mechanical failure) during initial climb
From Camarillo International Airport (KCMA) to Camarillo International Airport (KCMA)
Event
- NTSB case
- LAX06CA088
- 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
Huntington KIS
- Aircraft type
- Huntington KIS
- 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
- N506RJ
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Camarillo International Airport (KCMA), Camarillo, CATo Camarillo International Airport (KCMA)
- 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
- 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
- Substantial
Cause areas
- Miscellaneous, engine › Malfunction
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The experimental airplane experienced a partial loss of engine power in the takeoff initial climb, and collided with obstacles and terrain during an emergency landing in an open field to the west of the airport. The pilot stated that he was taking the newly constructed airplane for its second flight. The engine that was installed in the airplane was a automotive Subaru EJ20. He took off from runway 26 and was climbing at 90 mph. Everything seemed normal and then he noticed that his airspeed was 60 mph and the engine sound had decreased. There were no pops or abnormal engine sounds associated with the decrease in airspeed and the engine rpm was down at 1,700 instead of the normal 6,000. The pilot immediately manipulated the throttle to ensure it was fully opened, he then turned the ignition switch off and on in an attempt to reset the electronic engine control. Both actions failed to regain full power of the engine. He notified the tower that he had lost engine power. He decided to land in a field that was off the end of the runway. He was flying at 60 mph and had a rate of descent of a couple of hundred feet per minute. He made an forced landing into the field and was assisted by emergency responders shortly afterwards. The pilot said that the Subaru engine has a reduced power mode intended to operate the engine at a substantially reduced power output if an engine problem was detected by the engine electronic control system computer. He thinks that the engine switched to this low power mode shortly after takeoff. The method he knew of to correct this situation was to turn the ignition off then back on and this should have cleared the fault and allowed the engine to resume normal power output. The underlying reason for the engine going to the reduced power mode was not determined.
Probable cause
a partial loss of engine power due to the engine's electronic control system reverting to a designed reduced power mode of operation.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX06CA088
- Event ID
- 20060217X00207
- Case number
- LAX06CA088
- 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, 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: 98bca81fd1bf20053b8ac7f93cd1b40e6bac33d43c0ad1304419fb9605b040f3; retrieved 2026-09-21T09:00:48.742Z.