ASN Wikibase Occurrence # 2511
This record has been locked for editing.
| Date: | Thursday 21 February 2008 |
| Time: | 11:48 |
| Type: |  Van's RV-9A |
| Owner/operator: | Private |
| Registration: | N159AS |
| MSN: | 90995 |
| Total airframe hrs: | 60 hours |
| Engine model: | Eggenfellner H-6 |
| Fatalities: | Fatalities: 0 / Occupants: 2 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Princeton Airport, NJ -
 United States of America
|
| Phase: | Initial climb |
| Nature: | Private |
| Departure airport: | Princeton, NJ (39N) |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
Prior to the accident flight, the airplane had accumulated about 1 flight hour since the pilot completed the installation of a new aftermarket fuel injection and ignition system. Shortly after takeoff on the accident flight, as the pilot turned onto the crosswind leg of the traffic pattern, the engine lost power, and the propeller "stopped." The pilot added that he believed the electrical system was functioning at the time because the electronic flight instrument system and the communication radio continued to function. The pilot subsequently performed a forced landing into the dense forest below. Although the wreckage was fire-damaged during the recovery process, examination of the engine revealed that while the pilot had installed a new after market fuel injection/ignition system , an original-equipment diode bridge remained in place. The diode bridge provided dual electrical paths to the engine control unit, thereby providing electrical power to the ignition system. The original ignition system, for which the diode bridge was designed, drew between 4 and 6 amperes for operation, while the aftermarket system drew between 8 and 12 amperes. The only manifestation of a failure of the diode bridge would be on engine operation; the remainder of the electrical system would continue to function normally.
Probable Cause: A loss of engine power due to the pilot/owner's improper installation of a new ignition/fuel control system for the engine. Contributing was the unsuitable terrain for a forced landing.
Accident investigation:
 |
|
Sources:
NTSB
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 22-Feb-2008 12:20 | Fusko | Added |
| 22-Feb-2008 12:21 | harro | Updated |
| 21-Dec-2016 19:13 | ASN Update Bot | Updated [Time, Damage, Category, Investigating agency] |
| 21-Dec-2016 19:14 | ASN Update Bot | Updated [Time, Damage, Category, Investigating agency] |
| 21-Dec-2016 19:16 | ASN Update Bot | Updated [Time, Damage, Category, Investigating agency] |
| 21-Dec-2016 19:20 | ASN Update Bot | Updated [Time, Damage, Category, Investigating agency] |
| 03-Dec-2017 09:34 | ASN Update Bot | Updated [Cn, Other fatalities, Departure airport, Destination airport, Source, Narrative] |
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