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What Size Tub for a Tail Weight?


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The ones I've seen have all been standard washtubs. Screw on the casters, bend a piece of rebar to attach to (so it can't pull out), make sure everything is how you want it, then mix Quikrete in your wheelbarrow and fill 'er up! Should last for decades of heavy use.

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The shop at my airport has had the bottom third of a 55 gallon drum on casters, filled with wing bolts (someone told me B-25) for 41 years.  Airport is closing, mechanic was taking everything with him, tried to lift it with an engine hoist. Just about the time it began to lift off the floor, the metal rod and hook pulled through the bottom of the drum.  Good thing it didn't happen during any of my annual inspections!

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Thanks for your responses.


I know exactly how to make it.  What I need is the wash tub size and how many bags to get.  There are many sizes available.  I want it to be heavy enough for an F, but not too heavy.  My hangar is large and I won’t be swinging the gear of a Citation in the foreseeable future so I don’t want too much weight to move around.

Edited by MBDiagMan
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18 minutes ago, MBDiagMan said:

Thanks for your responses.


I know exactly how to make it.  What I need is the wash tub size and how many bags to get.  There are many sizes available.  I want it to be heavy enough for an F, but not too heavy.  My hangar is large and I won’t be swinging the gear of a Citation in the foreseeable future so I don’t want too much weight to move around.

I use a different method than what you're going to make, but if it will help you calculate what you need; I found that approximately 200 lbs of weight on the tail held my E model just about right.  If you take that number and figure out the volume of quickcrete needed, you should have the info you need.

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Yes, the required weight is what I need.  I can calculate everything else.  I thought there had been so many of these things made that people would off the top of their heads know how many bags and which size washtub.  Thanks to all.

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My IA uses about 200 lbs of stacked concrete block.    They're much easier to move around than a tub full of concrete.   I'm going to start using a Harbor Freight 1klb dolly with blocks stacked on it.   That way the dolly and blocks can be moved around easily and repurposed when necessary.    I've seen people try to dispose of concrete tubs at the airport and it's not pretty.

 

Edited by EricJ
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I’ve got one that is a welded steel frame made of 1-1/2” angle iron on 4 heavy casters.  It holds 4- 12” solid concrete blocks (80# each) stacked 2 high on each side of a telescoping post.

Being blocks makes it somewhat portable.
 

Clarence

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How are "standard aircraft jacks" called for by the SI different from non-aircraft jacks?  Is it a question of compatible support points, or is there something more to it?

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1 hour ago, tmo said:

How are "standard aircraft jacks" called for by the SI different from non-aircraft jacks?  Is it a question of compatible support points, or is there something more to it?

Probably a CYA thing

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2 hours ago, ragedracer1977 said:

And there's a long thread on it where I think @M20Doc contacted Mooney and they said keep tying the tail down 

not sure, its been brought up numerous times, I use the “A” frame method along with a tail stand, gives it 4 points and rock solid..... my pucker factor isn’t as high as it use to be compared to the 1st time :)

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9 hours ago, RLCarter said:

It’s been discussed before but here is the Service Bulletin

Mooney says after 50 years to not hold the tail down, but to lift by the engine. Hartzell and McCauley say to not use a prop jack to lift by. Lycoming says to not lift the nose ofnthe olane using the engine, the lift points are designed to lift only the engine.

So apparently we're supposed to jack the wings and magically levitate the nose wheel into the air.

I've stacked two cases of oil, a large roll of wrenches and a couple feet of bound approach plates on my tail, then held it stable by hand.

You gotta do what you gotta do . . . .

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@Hank yep, pick what your comfortable with. I had to pull the gear out of the 172 a few years ago, built the cradle per the maintenance manual, seemed like I had to jack it up into the Flight Levels before the cradle would go under it......... Jacking Airplanes up just feels wrong.....

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10 minutes ago, Hank said:

Mooney says after 50 years to not hold the tail down, but to lift by the engine.

I've not heard the 50-year caveat before.    Where did that come from?   Was there associated advice about tying the aircraft down for a storm with or without the tail tie down after 50 years?

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8 hours ago, ragedracer1977 said:

And there's a long thread on it where I think @M20Doc contacted Mooney and they said keep tying the tail down 

I actually checked with Lycoming, who said the engine lift ring is meant to lift the engine, not the airplane.  

Clarence

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