Re: Lawsuit Madness - OMG
Quote:
Originally Posted by jtheune View Post
I was wondering the same thing. I just spent a few minutes trying to find anything about the mythical 8 gallons of fuel starvation accident but can't find anything.
I couldn't find any reference to Dan's repeated assertion either. Certainly such an incident/accident would have an official report somewhere. He wouldn't make something like that up, would he? After all he is of such high moral character that they won't even let him play lawyer in Oregon
Why do you keep posting on a public forum when you've made such a monkey of yourself?
US Pilot’s CTSW engine suffers fuel starvation: NASA report Narrative: aircraft CTSW NASA ASRS Report 739488, May 2007 I kept climbing until I knew I was power off gliding distance from the runway. At that point I closed the throttle again and the engine not only lost power but came to a complete stop. (Not wind-milling anymore.) Left tank of the flight design was empty.
Right tank had (mythical?) 8 gals. This is a 31.5 gal system so we are saying that one quarter of the total fuel was still on board the aircraft. The ct flight design burns 4-5 gph. So I should have been good for at least another hour and a half. Also there is no option for switching tanks with a fuel selector and there is no auxiliary fuel pump like you have on most other GA aircraft. The only conclusion we could come up with logically was fuel starvation in the left tank and no options to access the fuel in the right tank.
22. On 30 June 2009 and 28 May 2012 The British version of the FAA and/or the NTSB investigated a fuel starvation of CTSWs and ordered Flight Design to warn its British pilots (Flight Design did not warn Plaintiff or other United States pilots)
AAIB Bulletin: 6/2010 G-CERA EW/G2009/06/06
ACCIDENT
Aircraft Type and Registration: Flight Design CTSW, G-CERA
No & Type of Engines: 1 Rotax 912ULS piston engine
Year of Manufacture: 2007
Date & Time (UTC): 30 June 2009 at 1101 hrs
Previous power loss incidents on this aircraft type have been attributed by some to the fuel outlets in the tanks becoming uncovered due to fuel sloshing during uncoordinated turns with low fuel levels, resulting in fuel starvation.
(However) In this case the aircraft reportedly had significant fuel on board and was not manoeuvring.
23. Another British fuel starvation of which defendants were aware:
TITLE Fuel System, …. A CTSW ran out of fuel when apparently 5 litres remained in one tank and no fuel indicated in the other. The reported circumstances of the accident indicate that the engine became starved of fuel. The nature of the tank design is not conducive to accurate gauging, with any sustained sideslip or nose-down attitude effectively generating quantities of unusable fuel in excess of the 0.5 litres stated by the aircraft manufacturer. In fact the manufacturer’s own tests, conducted with the aircraft on the ground, indicated a significant increase in the unusable fuel quantity when the aircraft attitude changed from the straight and level. The manufacturer additionally noted that it was possible to restart the engine following temporary fuel starvation; however, this might not be a practical procedure for pilots in the course of a normal flight and, moreover, would not comply with BCARS959, which refers to the first 86 © Crown copyright 2010 AAIB Bulletin: 8/2010 G-VINH EW/C2009/08/02 evidence of malfunctioning.
Safety Recommendation 2010-045
It is recommended that Flight Design GmbH, together with P&M Aviation, revise their assessment of the unusable fuel in the CTSWaircraft.
Additional safety action
Following this accident, P&M Aviation declared their intention to publish a Service Letter which will explain the effects of aircraft attitude and turbulence on fuel feed at low fuel levels. In addition, it will point out that the minimum quantity that the fuel sight gauge will indicate is 3 litres. (appx. 8/10 gallon) Finally, a placard will be required to be fitted to the aircraft advising the pilot that he or she must ensure that at least 1 cm of fuel is visible on both fuel contents sight gauges at all times.
CLASSIFICATION The CAA have classified this bulletin as Mandatory
COMPLIANCE Read and amend operations as directed, append to manual.
APPLICABILITY All UK registered CT2K and CTSW aircraft.
7)
A placard must be attached to the instrument panel as follows:
MONITOR FUEL SIGHT GAUGES REGULARLY.
BOTH GAUGES MUST SHOW SOME FUEL.
LAND IF NO FUEL IS SEEN IN EITHER SIGHT GAUGE.