CT9000
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Everything posted by CT9000
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.....reasonable after putting in such a valiant effort, R series, S series, Ap5, Ap6, VE, etc. ....
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..... wondering why these Aussies needed to each have a Ruger 10 shot as well as a 12 gauge pump action just to open beer cans ......
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.....very clever person hiding the helium balloon like that ....
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......stop using explosives and just drink beer whilst driving the dozer ripping burrows .....
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.....it would become obvious that removing roots with a dozer would require a rooter as distinctly different to a rootee which is more labor intensive ........
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......thought came to mind that a "Singular Root" might also include a square root which is the shape of the rippers for the dozer ......
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......maintain his composure whilst denying driving after consuming large quantities of grog ......
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....oooohh look at that another bunny in disguise, loading up the hollow points unto the Ruger.....
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......there would be even more room for extra hotels, duty free shops, gift shops, and all those other high profit tenants.....
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......there would be even more room for extra hotels, duty free shops, gift shops, and all those other high profit tenants.....
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Ha Ha Ha good one Nev I can just imagine an ejection seat in a Bobcat.
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Hard hat would have fallen off before head hit hard edge anyway so no help. Buy a Bobcat instead.
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AAIB report •Jab EFATO UK April '23
CT9000 replied to Garfly's topic in Aircraft Incidents and Accidents
Rotax deem heat is not required on their turbocharged engines. -
AAIB report •Jab EFATO UK April '23
CT9000 replied to Garfly's topic in Aircraft Incidents and Accidents
Of course you can add a turbo (914) no need for carb heat because the compression of the intake air ( boost) increases the temp. -
surely a simple compressor stall is no big deal
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.......was pretty good for business at the local bunny farm sorry roo farm sorry pet food sorry local chichen farm.....
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......Tortice towing a house.....
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Thanks for the addition Nev, I think we are on the same page. I would like to add that speed is not the primary problem in a stall it is the wing load. The normal quoted stall speed is at 1G and is a bit meaning less. eg. if you have a quoted stall speed of say 45Kts. and push foward till the seat load gets light the stall speed may be less than half that, if you are in a steep level turn the stall speed may well be 1.5 times that cos you are pulling back to maintain level. It all comes down to load.
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The stall stick position can vary it is not a fixed thing but is real. Of course the CG will move it. Discussion of SSP is a good thing to help understand what is actually happening during the stall. As far as the response goes, by all means step on the rudder to stop the yaw. If a gust caused the wing to stall it would be only momentary and would have recovered from the stall condition before the pilot had time to react. I agree that the teaching methods may not be all that good. It is far smarter to teach that unloading the wing is what fixes the stall which is exactly what reducing back stick does.
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Re reading this story over a cuppa. I do not believe that the aircraft did actually stall. To stall you need to reach the "stall stick position" otherwise you cannot get to the critical angle of attack and therefore no stall. Yes it dropped a wing but that is not necessarily a stall just a response to a gust. Stalls are not to be feared just need to be managed.
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.....all the wildlife. Mean time CT having just secured a bulk supply of 22 Magnum ammo wants to know where all these giant cats can be found......
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....first nation inhabitants that can advise on the social support system lack of fairness.......
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Turbs. you need to get out a bit more. Maybe I should have mentioned avref
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......all the real pilots will know that the above photo is only a side view of the 03/21 runway. A bit short but plenty wide.........
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......had a bit of a laugh at the idea of a ferris wheel because although safe in Tassie they are a danger up north becuase of the light planes flying into them causing terror to the wheels riders......
