ASN Wikibase Occurrence # 21408
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| Date: | Friday 20 June 2008 |
| Time: | 19:43 |
| Type: | Harmon F1 Rocket |
| Owner/operator: | Private |
| Registration: | N623BL |
| MSN: | 60 |
| Total airframe hrs: | 190 hours |
| Engine model: | Lycoming IO-540-D4A5 |
| Fatalities: | Fatalities: 2 / Occupants: 2 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Belleplain, NJ -
 United States of America
|
| Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
| Nature: | Private |
| Departure airport: | Woodbine, NJ (1N4) |
| Woodbine, NJ (1N4) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
While performing aerobatics, the engine lost all power. Evidence indicates that the pilot attempted to restart the engine, and that the airplane impacted wires while the pilot attempted to execute a forced landing to a road. The airplane came to rest on the road and was partially consumed by the postcrash fire. No evidence of preimpact failure or malfunction of the airframe or engine was discovered. The airplane was equipped with two fuel tanks. The flight manual advised that, “Prolonged uncoordinated flight with low fuel quantities may uncover the fuel tank outlets, causing fuel starvation and engine failure.” The pilot however, had modified the left fuel tank with an inverted fuel system, to allow the engine to operate while the airplane was in unusual attitudes or inverted. Examination of the left fuel tank revealed that it had been modified with the inclusion of a flop tube (a flexible hose with a weight attached at its free end). When the airplane was right side up, the hose would feed fuel from the bottom of the left fuel tank, and when the plane would roll inverted, the weight would cause the hose to flop to the top of the left fuel tank, and feed its fuel from there, allowing the engine to continue to run. Examination of the right side of the fuel system revealed it was similar to the system described in the kit manufacturer’s assembly manual and did not have a flop tube. The floor mounted fuel selector was found set to the right tank.
Probable Cause: A total loss of engine power due to fuel starvation as a result of the pilot's failure to select the proper tank prior to performing aerobatics.
Accident investigation:
 |
|
Sources:
NTSB
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 21-Jun-2008 22:25 | 78Delta | Added |
| 22-Jun-2008 10:10 | harro | Updated |
| 24-Jun-2008 23:26 | Fusko | Updated |
| 12-Jul-2008 23:20 | Fusko | Updated |
| 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 11:19 | ASN Update Bot | Updated [Cn, Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative] |
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