Kitfox-List Digest Archive

Sat 04/17/04


Total Messages Posted: 10



Today's Message Index:
----------------------
 
     1. 05:29 AM - Page (Norm Beauchamp)
     2. 05:43 AM - Re: Weight and balance (Michel Verheughe)
     3. 06:21 AM - Most Adverse Aft C.G. ()
     4. 06:45 AM - Re: Weight and balance QUARANTINE_LEVEL=4.0 KILL_LEVEL=5.0  (Dcecil3@aol.com)
     5. 07:03 AM - Re: Used Kitfox and the DAR (Dcecil3@aol.com)
     6. 07:13 AM - Re: Crosswind limits ...Spin, (Aerobatics@aol.com)
     7. 08:00 AM - Re: Crosswind limits ...Spin, (RiteAngle3@aol.com)
     8. 01:28 PM - Re: Crosswind limits ...Spin, (Aerobatics@aol.com)
     9. 02:21 PM - Re: Weight and balance (Michel Verheughe)
    10. 05:36 PM - Re: Weight and balance (Dcecil3@aol.com)
 
 
 


Message 1


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    Time: 05:29:58 AM PST US
    From: Norm Beauchamp <nebchmp@wcc.net>
    Subject: Page
    QUARANTINE_LEVEL=4.0 KILL_LEVEL=5.0 --> Kitfox-List message posted by: Norm Beauchamp <nebchmp@wcc.net> Grant Fluent, Would you contact me off list please? Thanks. Norm Do Not Archive.


    Message 2


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    Time: 05:43:47 AM PST US
    From: Michel Verheughe <michel@online.no>
    Subject: Re: Weight and balance
    QUARANTINE_LEVEL=4.0 KILL_LEVEL=5.0 --> Kitfox-List message posted by: Michel Verheughe <michel@online.no> Dcecil3@aol.com wrote: > I don't know about the model 4 ,but the model 3 manual says to use the bottom > of the fusalage, between the landing gear for level. The way I did it in my model 3 is to set a water level on the floor of the cockpit. Isn't that good enough? Cheers, Michel


    Message 3


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    Time: 06:21:47 AM PST US
    From: <barryhuston@adelphia.net>
    Subject: Most Adverse Aft C.G.
    pts rule name description ---- ---------------------- -------------------------------------------------- --> Kitfox-List message posted by: <barryhuston@adelphia.net> Hi Folks ---- Most Adverse Aft C.G. Questions The Stated C.G. Envelope for the Model IV - 1200 is 10.2" to 16" Currently: As a 912 powered tail dragger fully loaded using actual pilot and passenger weights, the most adverse aft C.G. is at the limit of 16". Issue: In converting it to an amphibious float plane --- without wheels before adding the floats, the C.G. approaches 16.4" The Ideal location for the float C.G. is at the Plane gross C.G. and should be 3" to 6" ahead of the float step, therefore keeping the overall C.G.at 16.4'. Before I start moving equipment to less desirable locations I would be interested in opinions on how far the Aft C.G. can be stretched (if at all) and was wondering if a safety factor has been built into the C.G. envelope. Thanks Barry


    Message 4


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    Time: 06:45:20 AM PST US
    From: Dcecil3@aol.com
    Subject: Re: Weight and balance QUARANTINE_LEVEL=4.0 KILL_LEVEL=5.0
    KILL_LEVEL=5.0@matronics.com --> Kitfox-List message posted by: Dcecil3@aol.com Michel whatever works best. I was just quoteing the actual manual.There are a Gazillion ways to do everything , as long as you arrive at the same conclusion.You used a Water level, I used a 60" Carpenter's Framing Level .Some would prefer a Laser Level.the manual just says "Level the Plane" if you wanna balance it on the Empire State building it's your plane.Betcha Cessna dosen't have that much leway Best David Cecil


    Message 5


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    Time: 07:03:31 AM PST US
    From: Dcecil3@aol.com
    Subject: Re: Used Kitfox and the DAR
    KILL_LEVEL=5.0@matronics.com --> Kitfox-List message posted by: Dcecil3@aol.com Talked to the builder at lenght.Found out what I expected. When the Insurance CO. paid the claim on the Kitfox they also took the airworthiness certificate. The good news is the builder is still using the same Guy!!!!!!!!! so should have what I need soon. Now a Warning to all those would be damaged kitfox builders and to those of you considering selling your plane. The way it was explained to me by the FAA, if we find the Airworthiness Certificate (AWS) then it stays with the plane and the plane is a rebuild and you don't need a DAR to inspect the plane, Just an A&P to sign it off but, If the AWS is turned in to Oklahoma City then I can start from scratch it will be "My" kit and I'm the builder.The later is the best choice because, if you do it as a rebuild, you will forever implicate the original builder, his name not yours will be on the AWS Neat aint it all this Because the Insurance CO didn't send the AWS to OK City Best David Cecil


    Message 6


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    Time: 07:13:15 AM PST US
    From: Aerobatics@aol.com
    Subject: Re: Crosswind limits ...Spin,
    KILL_LEVEL=5.0@matronics.com --> Kitfox-List message posted by: Aerobatics@aol.com Just a thought re spins.... That airshow KF was a clipped wing.... big difference re spin recovery. The Older KF were shy on vertical fin, this is less of problem on a clipped wing regarding spin recovery. CG, also has a very large bearing on spin recovery. The best scenario is a nose heavy clipped wing, the worst is a full span with an aft CG. Personally, I would not spin it unless I knew exactly what was done before, safely. I kinda speak the obvious, but safety is our highest priority Best, Dave


    Message 7


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    Time: 08:00:30 AM PST US
    From: RiteAngle3@aol.com
    Subject: Re: Crosswind limits ...Spin,
    KILL_LEVEL=5.0@matronics.com --> Kitfox-List message posted by: RiteAngle3@aol.com In a message dated 4/17/04 7:13:46 AM Pacific Daylight Time, Aerobatics@aol.com writes: Personally, I would not spin it unless I knew exactly what was done before, safely. I kinda speak the obvious, but safety is our highest priority Best, Dave Dave, I agree with this 1000%, I haven't flown over 25000 hours by doing to many really stupid things, more than I'd like to admit I know. Spins in aircraft that haven't been successfully recovered from spin testing are NOT one of the things I'm going to do, that is a field left for the professional test pilots in my opinion. I had a cousin that was test pilot for Culver Aircraft in Wichita, spin testing a new 4 place in the late 40's and watched the company go bankrupt -- as he floated down in his parachute. He completed his career as a test pilot for Cessna Aircraft, doing both production and initial flight test work. When going to college I used to ride around with him on production test flights in all Cessna aircraft that were in production in the late '50's& early 60's--things have changed slightly! I have a file of all stall/spin type aircraft accidents over the last 10 years, however homebuilt aircraft are not listed in a way you can see what type they are unless you do an N number search due to many builders using their names as the manufacturer. It will sure make you think a bit when you look at it and study the causes! Safety is No Accident Elbie


    Message 8


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    Time: 01:28:18 PM PST US
    From: Aerobatics@aol.com
    Subject: Re: Crosswind limits ...Spin,
    --> Kitfox-List message posted by: Aerobatics@aol.com Wow 25,000 hours? er um ...my total now is only around 600 But, I design model, radio control aircraft for a living (past 25 years) and the evolutionary process for us is very fast, allowing us to make many changes, easily and quickly. We can learn a lot. The KF is a great plane, and not so great. The KF 2 I own, I love, BUT, its short coupled and under-finned. We would never even consider doing a model this way. I can only imagine, that with an aft CG location, is a formula for disaster. I speak only from practical experience from models. Once spinning, I suspect it could go flat further making recovery very difficult. With a forward CG location, it MIGHT be OK? But man, no way I want to take that chance. Spinning can vary a lot. When they test a production plane I bet the process is under a wide CG range, different types of entry, different weights and so on. Unless someone can prove to me it was done with a plane... I wont do it.... Rent an aerobat like a Pitts, Extra, Cessna aerobat etc. and get isntruction. There are many that are a blast. I still talk about my limited dual ( 4 hours) in a Pitts S2B wow! I mean really big wow! It was with a pro, in a certified aerobatic plane and I had a chute..... Dave KF 2 582


    Message 9


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    Time: 02:21:25 PM PST US
    From: Michel Verheughe <michel@online.no>
    Subject: Re: Weight and balance
    --> Kitfox-List message posted by: Michel Verheughe <michel@online.no> Dcecil3@aol.com wrote: > Michel whatever works best. I was just quoteing the actual manual. Of course, David. But you sound a bit offended as if I was trying to be patronizing with "a better way" of levelling. It was certainly not the case and I apologize if I gave that impression. You know that I am a novice and certainly not able to give any advice. My answer was rather to be understood as a question, like: "I do it on the top of the floor, which, I hope, is the same as the bottom of the fuselage, as indicated in the same manual as yours." Cheers, Michel


    Message 10


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    Time: 05:36:05 PM PST US
    From: Dcecil3@aol.com
    Subject: Re: Weight and balance
    --> Kitfox-List message posted by: Dcecil3@aol.com Michel Sorry if I sounded Offended I was just saying two things:1 Howerever you arrive at the same conclusion is fine just as long as it's the same 2 The nice thing about homebuilding is you can do it differently.we're not limited to GTO like GA aircraft(You can put Gas in it ,check the air in the Tires and check the Oil) sorry if I ruffled any feathers(No pun intended) David Cecil DO NOT ARCHIVE




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