Accident Sonex Aircraft Sonex N555SX,
ASN logo
ASN Wikibase Occurrence # 287171
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Friday 6 February 2009
Time:15:00 LT
Type:Silhouette image of generic SONX model; specific model in this crash may look slightly different    
Sonex Aircraft Sonex
Owner/operator:
Registration: N555SX
MSN: 523
Total airframe hrs:259 hours
Engine model:UL Power 260i
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Crossville, Tennessee -   United States of America
Phase: Initial climb
Nature:Test
Departure airport:Crossville Memorial Airport, TN (CSV/KCSV)
Destination airport:Crossville Memorial Airport, TN (CSV/KCSV)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot of the amateur-built airplane was initiating a test flight to check a new propeller. After advancing the throttle, the airplane accelerated with normal power. However, at an altitude of 300 feet, the engine lost total power. The pilot turned back to the departure runway and landed on soft ground to the south of the runway. The landing gear collapsed, substantially damaging the firewall. Examination of the airplane revealed that continuity existed throughout the engine drivetrain, and the engine had no visible damage. The fuel was sampled and no contamination was observed. Examination of the fuel filter revealed no obstructions, the fuel pump operated normally, and the air filter was clean. The spark plugs were determined to be functional; however, no electrical energy was being delivered to the spark plugs. Further examination revealed that the electronic control unit (ECU) was not transmitting voltage to the dual coils. The ECU was manufactured to automotive specifications, and was supposed to be installed in an area of the airplane where temperatures do not exceed 65 degrees Celsius (preferably on the cabin side of the firewall). The ECU on the accident airplane was installed on the engine side of the firewall.

Probable Cause: A total loss of engine power during initial climb due to the failure of the ignition power supply as a result of the improper installation of the electronic control unit.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA09CA162
Status: Investigation completed
Duration: 2 months
Download report: Final report

Sources:

NTSB ERA09CA162

Location

Revision history:

Date/timeContributorUpdates
04-Oct-2022 08:00 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org