ASN Wikibase Occurrence # 352863
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Date: | Sunday 8 August 1999 |
Time: | 18:22 LT |
Type: | Piper PA-28-181 |
Owner/operator: | Greenville Aviation Flt School |
Registration: | N82974 |
MSN: | 28-8190089 |
Total airframe hrs: | 6133 hours |
Engine model: | Lycoming O-360-A4A |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Greenville, SC -
United States of America
|
Phase: | Approach |
Nature: | Private |
Departure airport: | Goldsboro, NC (GWW |
Destination airport: | (KGMU) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The flight departed with full fuel tanks and the fuel selector was positioned briefly to the left tank using only 2-3 gallons of fuel; the remainder of the flight the fuel selector was positioned to the right tank. The flight was cleared to land from a left base leg and while on short final approach, with the flaps extended 20 degrees, he added power but the engine did not respond. Attempts to restart the engine were unsuccessful. He cycled the fuel pump switch and fuel pressure decreased to zero. He declared a mayday and unable to land on the runway, collided with an embankment short of the displaced threshold. The left wing separated from the airplane during the impact sequence. Post accident examination of the airplane revealed only approximately 2 ounces of fuel drained from the intact right wing fuel tank. The left wing fuel tank was found to contain approximately 9 gallons. Fuel was added to the right wing fuel tank and the engine was started and operated to 800 rpm; damage to the propeller precluded operation to a higher rpm. Examination of the fuel vent system, fuel quantity indication system revealed no evidence of preimpact failure or malfunction.
Probable Cause: The improper position of the fuel selector by the pilot-in-command resulting in the loss of engine power due to fuel starvation. Also, the inadequate altitude flown by the pilot on final approach preventing a landing on the runway following the loss of engine power.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | MIA99LA221 |
Status: | Investigation completed |
Duration: | 1 year and 3 months |
Download report: | Final report |
|
Sources:
NTSB MIA99LA221
Revision history:
Date/time | Contributor | Updates |
09-Mar-2024 07:49 |
ASN Update Bot |
Added |
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