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|
Attributes | |
ACN | 1641768 |
Time | |
Date | 201904 |
Local Time Of Day | 1801-2400 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Make Model Name | RV-9 |
Operating Under FAR Part | Part 91 |
Flight Phase | Landing |
Route In Use | Visual Approach |
Flight Plan | None |
Component | |
Aircraft Component | Engine |
Person 1 | |
Function | Pilot Flying Single Pilot |
Qualification | Flight Crew Private |
Experience | Flight Crew Last 90 Days 25 Flight Crew Total 845 Flight Crew Type 825 |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy Ground Event / Encounter Object Ground Excursion Runway |
Narrative:
At night; cleared to land. Below 500 feet; after selecting 20 degrees of flaps; and bringing the nose up to slow down; a total loss of engine power occurred. An attempt to restart the engine failed. Gliding down I landed on the extended runoff area prior to the threshold of the runway. The aircraft continued rolling and was unable to stop before contact with plastic barriers placed across the pavement. The nose gear wheel pant was damaged with the fiberglass cracked.after the incident I found the two electronic ignition power switches in the off position. The only explanation is that during the run-up; these were turned off to check the internal power from the emag ignition; and they were never turned back on. The ignition supplies its own power; unless the engine RPM drops below approximately 1400 RPM. Once the engine RPM got too low; both ignition emag devices stopped supplying the spark plugs.
Original NASA ASRS Text
Title: Vans RV-9 pilot reported the engine quit on short final; leading to slight damage to a wheel pant after a runway excursion. Reporter stated after landing he found the ignition power switches in the wrong position; causing the engine to shut down.
Narrative: At night; cleared to land. Below 500 feet; after selecting 20 degrees of flaps; and bringing the nose up to slow down; a total loss of engine power occurred. An attempt to restart the engine failed. Gliding down I landed on the extended runoff area prior to the threshold of the runway. The aircraft continued rolling and was unable to stop before contact with plastic barriers placed across the pavement. The nose gear wheel pant was damaged with the fiberglass cracked.After the incident I found the two electronic ignition power switches in the OFF position. The only explanation is that during the run-up; these were turned off to check the internal power from the EMAG ignition; and they were never turned back on. The ignition supplies its own power; unless the engine RPM drops below approximately 1400 RPM. Once the engine RPM got too low; both ignition EMAG devices stopped supplying the spark plugs.
Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.