MOORE EDWARD R MXS near Borrego Springs, CA — 2012-09-08
- Date
- 2012-09-08
- Location
- Borrego Springs, CA, USA
- Airport
- L08
- Aircraft
- MOORE EDWARD R MXS
- Registration
- N21MX
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Maneuvering
Probable cause
The pilot’s inability to maintain control of the airplane following the loss of aileron and elevator control due to the forward flight control torque tube assembly’s detachment from the forward bearing. Contributing to the accident was the inadequate construction of the forward bulkhead that held the flight control torque tube assembly in place and the improper installation of the thrust bearings.
Contributing factors
Contributing to the accident was the inadequate construction of the forward bulkhead that held the flight control torque tube assembly in place and the improper installation of the thrust bearings.
NTSB narrative
During the aerobatic practice flight, the airplane departed controlled flight. The pilot opened the canopy, which then separated from the airplane, and exited the airplane. Due to the low altitude, the pilot's parachute did not fully deploy before he impacted the ground. The accident airplane was 1 of 14 MX-model airplanes. It was the only model built from a kit as an experimental, amateur-built aircraft, and it was constructed differently than the other MX-model airplanes. Postaccident examination of the torque tube assembly revealed that the forward bulkhead holding the torque tube assembly in place was constructed in a way that allowed the bulkhead to flex, which subsequently led the torque tube assembly to detach from the forward bearing during the accident flight and resulted in the loss of aileron and elevator control. Examination also revealed that the forward and aft bearing houses were installed opposite of the correct direction, which allowed the bearings to detach from the torque tube assembly when the front bulkhead flexed.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Proper installation of the torque tube assembly could have prevented the accident.
NTSB coding
Evidence available
- Photos
- 25 docket documents
Docket documents25
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementinterview
- Aircraft Logbookother
- Aircraft Logbook Entry A&Pother
- Electronic Devices 17 - Attachment 1 (Garmin GPS 496) - Tabular Data (CSV)other
- Electronic Devices 17 - Attachment 2 (EI MVP-50P) - Tabular Data (CSV)other
- Email Between MX Aircraft and Angel Fire Issuesother
- Engine Logbookother
- Examination of Parachute by FAAother
- Exemplar MXS Torque Tube Installationother
- FAA Experimental Operating Limitationsother
- MXS Torque Tube Assembly Post Accidentother
- Record of Conversation – Mooreother
- On Board Image Recorder - Specialist's Factual Reportphotos
- Photo 1 – Accident Sitephotos
- Photo 2 – Cockpitphotos
- Photo 3 – Torque Tube Assembly Installation Exemplarphotos
- Photo 4 – Torque Tube Assembly Post Accidentphotos
- Electronic Devices 17 - Specialist's Factual Reportreport
- Lycoming Reportreport
- MX Aircraft Examination Reportreport
- Materials Laboratory 15 - Factual Report 12-118report
- Toxicological Reportreport
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