Allegro-List Digest Archive
Sat 05/14/11 |
Total Messages Posted: 1 |
Today's Message Index: ---------------------- 1. 04:10 AM - Fuselage Composite Failure/Plane Total Loss (Rwmurrayhm@aol.com)
Message 1
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Time: 04:10:35 AM PST US
From: Rwmurrayhm@aol.com An Allegro 2007 was recently declared a total loss because of fuselage composite deformation and de-lamination. A crease or ripple began developing just in front of the pilot side door and ultimately traveled under the fuselage and up towards the passenger side door. Composite experts determined that the structural integrity of the fuselage was compromised. A small leak in the fuel tank had allowed fuel (MoGas) to seep into the underlying composite and soften it. The crease seems to follow the front of the fuel tank as it is glassed into the fuselage. Fantasy Air's subcontractor for the fuselage (Composit Airplanes of the Czech Republic) said in an e-mail: "It was produced over 200 fuselages and this is third (3.) case. It was always caused with bad landings. The laminate fuel tank is produced separated in special mold and is glued in fuselage after complete treatment against effect of fuel. But it is strength component of whole fuselage. Tank tightness is very responsibly tested - 3 days pressure. The whole fuselage is epoxy with glass reinforcements and sandwich material is HEREX. The fuel tank is the same just special chemicals resistant epoxy is used and sandwich material is SORICK. In accordance with photo sent I think that the fuselage is greatly damaged and from our point of view is unrepairable." I believe the fuel tank leak developed from a flat tire experienced upon landing. At the time there was no visible damage from the event. The tire was changed and the aircraft flew another 20 hours. Fuel never visibly leaked out or even stained the gel coat. Nor was there ever any discernible loss of fuel. It may have only taken a quart or two of fuel sitting in the composite for months to soften it. The flat tire was in May 2010; the damage became evident between November 2010 and January 2011. The aircraft was normally hangared with half a tank or more of fuel on board. Richard Murray
Subject: Fuselage Composite Failure/Plane Total Loss
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