LAX06LA103 · Harwood Kenneth Lancair 360A
Harwood Kenneth Lancair 360A · Accident: total loss of engine power (mechanical failure) while maneuvering
From Palm Springs International Airport (PSP) to an unrecorded destination
Event
- NTSB case
- LAX06LA103
- 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
Harwood Kenneth Lancair 360A
- Aircraft type
- Harwood Kenneth LANCAIR 360
- 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
- N15KH
- Operator
- Joseph D. Dennis III · private individual
- Onboard fatalities
- Unknown
- Route
- From Palm Springs International Airport (PSP), Palm Springs, CATo not recorded
- 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
- Maneuvering
- 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)
- Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
- Wire, transmission
- 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
- Engine assembly, cylinder › Loose part/bolt/nut/clamp/etc
- Unknown › Maintenance, installation, inadequate
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The airplane collided with power lines during a forced landing following a loss of engine power. The pilot reported that while maneuvering at 2,000 feet the engine began losing power. The pilot decided to divert to a nearby airport to make the emergency landing. While en route to the alternate airport, the pilot observed a part of the engine departing through the cowling and the engine lost complete power. At that point he knew he was not going to make it to the airport and decided to make a forced landing on a highway. Examination of the engine showed that the number three cylinder separated from the crankcase at the mounting pad due to the separation of its mechanical attachments. Once the cylinder separated, the piston then became unsupported, which resulted in the subsequent separation of the connecting rod from the crankshaft journal. Severe fretting signatures were found on the cylinder flange and crankcase mounting pad. The threads on the top hold down studs were undamaged and indicated that these nuts became loose and backed off. The studs on the bottom of the cylinder were fractured in overload and separated at a level consistent with the upper surface of the cylinder mounting flange.
Probable cause
A loss of engine power caused by the separation of the number three cylinder due to the improper torque on the hold down nuts.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX06LA103
- Event ID
- 20060209X00190
- Case number
- LAX06LA103
- 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: ecb71ac14722879d089f5206e0492d4df4a55cb15b3488718ba5208feb28b3b5; retrieved 2026-09-22T05:07:12.441Z.