LAX07LA218 · Clement Zenith Zodiac CH601
Clement Zenith Zodiac CH601 · Accident: total loss of engine power (mechanical failure) on approach
From Rosamond Skypark Airport (L00) to Rosamond Skypark Airport (L00)
Event
- NTSB case
- LAX07LA218
- 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
Clement Zenith Zodiac CH601
- Aircraft type
- Clement ZENITH ZODIAC CH601
- 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
- N239PC
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Rosamond Skypark Airport (L00), Rosamond, CATo Rosamond Skypark Airport (L00), Rosamond, CA
- 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
- Approach · VFR pattern turn to base
- 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
- Total 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
- Owner/builder › Maintenance, adjustment, improper
- Throttle/power lever › Improper
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The accident flight was the airplane's maiden flight where the pilot was to complete a series of shallow banks. After doing the predetermined maneuvers, which included four simulated approaches to landing, he descended to traffic pattern altitude. As he maneuvered onto the base leg, he reduced the engine power from about 4,500 rpm to 2,000 rpm. The airplane began to lose a significant amount of altitude, and in response, the pilot moved the throttle control forward. The engine then had a total loss of power. The airplane descended and impacted the roof of a private residence. Examination of the airplane and engine following the accident revealed the upper spark plugs were all a similar black coloration, indicating that the fuel/air mixture was rich. Additional evidence of a rich mixture was found with dark black residue lining the tail pipe exhaust. After starting the engine during a postaccident examination, the throttle control was manipulated and the engine responded appropriately. The engine emitted a thick white smoke during operation. Investigators noted that when retarding the throttle toward the idle position, the throttle arms did not move against the idle adjustment screw stops. Manual manipulation of both throttle arms to the carburetors' adjustment screws resulted in a loss of power. The same action was repeated four times, producing the same results. The right carburetor bowl contained a brown colored liquid similar in color to a maple syrup; the odor was consistent with a varnished fuel. The left carburetor bowl contained a small amount of fluid that was similar to that of the fluid found in the right carburetor, though a shade lighter in color. The fuel found in the center fuel tank was also varnished. In the 7 months prior to the accident, the engine had only been run on 11 occasions, all on the ground, for a total of 2 hours of operational time.
Probable cause
A total loss of engine power during approach due to the improper idle screw/stop adjustment. A factor contributing to the accident was deteriorated fuel.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX07LA218
- Event ID
- 20070726X01018
- Case number
- LAX07LA218
- 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: 9f8d2379890555d296c9e8dd19d41b92dc181a55f129416a9c0914799609f597; retrieved 2026-09-21T18:27:10.018Z.