ASN Wikibase Occurrence # 288338
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| Date: | Sunday 11 July 2010 |
| Time: | 08:15 LT |
| Type: |  Beechcraft 58 Baron |
| Owner/operator: | |
| Registration: | N405RW |
| MSN: | TH325 |
| Year of manufacture: | 1973 |
| Total airframe hrs: | 3139 hours |
| Engine model: | Continental IO-520-C |
| Fatalities: | Fatalities: 0 / Occupants: 1 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | LaGrange, Georgia -
 United States of America
|
| Phase: | Standing |
| Nature: | Private |
| Departure airport: | La Grange-Calloway Airport, GA (LGC/KLGC) |
| Savannah/Hilton Head International Airport, GA (SAV/KSAV) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
The airplane had just been fueled by the lineman at the fixed-base operator (FBO), who secured the fuel caps after the service. During the climb after takeoff, the right-wing fuel cap came off of the wing, remaining attached only by the chain. An estimated 11 gallons of fuel was siphoned from the wing before the pilot returned to the airport and taxied back to the FBO. The pilot secured the cap and conducted a visual inspection of the right wing, before attempting to start the engine again. The right engine backfired, followed by a loud bang and whoosh sound; flames then rose from the right wing. A postaccident examination of the right wing revealed that the internal blast was a result of the backfire igniting fuel vapors that remained after the siphoning. The blast caused the upper wing skin to expand and separate from the retaining rivets. A soot trail originated at the exhaust pipes and traveled in an aft direction to the trailing edge of the wing.
Examination of the fuel cap revealed that the outer o-ring was dry and cracked, a washer was missing, the cap leaked under pressure, and that the force required to secure the cap exceeded the manufacturer's specification. The airplane's maintenance records did not indicate the last time the fuel cap was overhauled. Fuel cap maintenance is permissible by a Federal Aviation Administration (FAA) certified airframe mechanic or by an FAA-approved overhaul facility. While the cap's manufacturer has standards on the required forces to secure the fuel cap lock tab and a leak testing process, the airplane's maintenance manual does not mention either.
As a result of separate investigations, the airplane's manufacturer has included in applicable airplanes' maintenance manuals the following verbiage: 'Note: Inspect the fuel filler cap outer o-ring for flexibility, splits cracks or distortion. If the o-ring is damaged in any way replace or overhaul the fuel cap.â€
Probable Cause: The pilot not allowing sufficient time for fuel spill vapors to dissipate before starting the engine. Contributing to the accident was the inadequate maintenance of the fuel cap.
Accident investigation:
 |
|
Sources:
NTSB ERA10LA357
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 04-Oct-2022 21:22 | ASN Update Bot | Added |
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