LAX99LA276 · Mooney M20E
Lake Aero Styling & Repair Mooney M20E · Accident: total loss of engine power (mechanical failure) during initial climb
From 1O2 to an unrecorded destination
Event
- NTSB case
- LAX99LA276
- 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
- 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
Mooney M20E
- Aircraft type
- Mooney M20
- 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
- N6022Q
- Operator
- Lake Aero Styling & Repair
- Onboard fatalities
- Unknown
- Route
- From 1O2To 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
- 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
- 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
- Company maintenance personnel › Maintenance, annual inspection, inadequate
- Other maintenance personnel › Maintenance, installation, improper
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The airplane's engine lost power during takeoff climb out on a post maintenance check flight, which was performed following repair of damage caused by a gear-up landing. Among other repairs, the engine had been removed, inspected, and reinstalled. The pilot reported that soon after takeoff, while passing the departure end of the runway, the engine started losing power and running rough. He started a turn, intending to land downwind on the departure runway using the partial engine power available. During the turn the engine ceased producing power completely. Because of low airspeed and altitude, the pilot was unable to glide the aircraft to the runway and crashed in a vineyard. An FAA inspector examined the engine and reported there was a loose B-nut on a fuel injection system hose where the hose attached to the fuel divider on top of the engine. When the electric fuel pump was turned on fuel sprayed from the loose B-nut. The inspector reported that the B-nut required about one turn in the tightening direction to reach the snug position. No other discrepancies were noted. The engine was installed on a test stand and run. With the B-nut tight, the engine was started and ran smoothly. The engine was accelerated to full power and smoothly produced about 2,700 rpm. After about 5 minutes at full throttle, the B-nut was loosened. After 1/8 of a turn fuel came out of the hose end. After 1/4 turn the engine began to run rough and between 1/4 and 1/2 turn the engine abruptly stopped.
Probable cause
The failure of engine shop maintenance personnel to tighten the fuel line fitting during assembly of the engine, and failure of the installing maintenance personnel to detect and tighten the loose fitting during the engine installation and annual inspection.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX99LA276
- Event ID
- 20001212X19559
- Case number
- LAX99LA276
- 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: fdbfc47b0b86bc0d8395f586bba0e2b2d52fbfca302a12613fb301b7cb77e943; retrieved 2026-09-21T10:53:35.733Z.