Greg, all,

 

It seems from the earlier discussion there needs to be deliberate alignment 
(aerodynamically (rudder) and tailwheel (physically)) between the two possible 
competing directional controls.

I had not had this problem, however given the two controls are locked together 
physically without any latitude for equalisation, they can be trying to take 
the A/C in different directions, depending on which has the most authority at 
the time, which mostly is going to be dependent on weight on the tailwheel.

As soon as the tailplane flies the rudder takes over and if it is misaligned 
there will be a sudden transition. By my understanding.

Probably best aligned dynamically with test runs up to tailplane lift off.

Without actually viewing the mechanical setup, I am unsure how this can be 
achieved, however the diagram sent helps. There does not seem to be any 
alignment ability.to allow for wear considerations.

 

My input for what it’s worth.

 

Bob Wilson  

 

From: [email protected] [mailto:[email protected]] On Behalf 
Of Greg Wilson
Sent: Thursday, 27 July 2017 6:44 AM
To: [email protected]
Subject: Re: [DOG mailing list] Hoffman Props

 

 


Greg Wilson



 

---- On Wed, 26 Jul 2017 22:38:12 +1000 Michael Stockhill<[email protected] 
<mailto:[email protected]> > wrote ----

 

Thanks, Tom and Laurie,

 

I live in Polson, Montana.  I did fly another H36 and don't recall it having 
that tendency, however it had its own problems, being very tail heavy and with 
a tailwheel fork issue of its own that caused it to set up an oscillation that 
would shake your teeth out. I was able to sort that out for the owner.

 

You have given me lots of ideas for some trouble shooting. It is refreshing to 
know that this tendency may not be typical of the breed.

 

M

 

On Jul 26, 2017 1:00 AM, "Laurie Hoffman via dog" <[email protected] 
<mailto:[email protected]> > wrote:

Thanks Tom,

I was thinking something along these lines. An issue between rudder and 
tailwheel interplay perhaps. I know of instances of steering/rudder cables 
being too tight that have caused Dimona operators over controlling problems 
during the ground run. The comment of the previous owner of Michael's aircraft 
and the faulty tailwheel repair seems to confirm the possibility.

I'm no engineer though and Rob, Nigel, Macca and others would know best.

I don't have the wide T/W experience that you have Michael, about 1000hrs in 
SuperCubs, a few in Pawnees, Callair and some several hundreds in TMGs. I've 
flown quite a few TMG types and I have to say that after something like 15 
years of operating, our Dimona is an absolute delight both in the air and on 
the ground.

The other owners and myself have taken off and landed in what on occasions were 
horrendous cross wind conditions and the Dimona has handled them all 
wonderfully despite not having differential braking.

If possible i would strongly recommend that you fly in another H36 to see if 
there is any difference to yours. Just remind me where you are located pls.

I don't believe asymmetric blade effect to be of any real consequence with the 
L2000 and doesn't appear to be noticeable with the L2400.

Compared with the other aircraft that you have flown the Dimona certainly does 
need sensitive control input. Just a thought, but after your extensive 
experience with US clockwise rotating engines and even though you are aware of 
the difference, any chance that you may still be unconsciously applying right 
rudder during rotation? Also wondering if you have any gliding experience in 
FRP aircraft Michael with which you can compare the H36.

Best Regards

Laurie 

 

 

 

 

 


  _____  


On Wednesday, July 26, 2017, 12:17:05 PM GMT+10, <[email protected] 
<mailto:[email protected]> > wrote:

 

 

 

 

Dear all,

My dimona S.n. 3506 had developed ovalized bolt holes on the tailwheel steering 
horn over time (circled green in attached drawing from H36 parts manual). 
Although I had previously adjusted the turnbuckles to align the rudder and 
tailwheel, a subsequent off center touchdown would misalign the rudder and 
wheel – resulting in a startling  condition in which straight rudder input 
yielded a strong turning output, ground loop imminent.

The cause of the problem became apparent when I held the rudder firmly while 
twisting the tailwheel –  three degrees of play was then evident. Disassembly 
of the tailwheel drive  horn revealed the wear on the horn tube where it is 
fixed to the tailwheel shaft with two M10 bolts. Repair was accomplished by 
slightly reaming the oval holes until roundness was restored, and then bushing 
the M10 bolts for a tight fit – no play even before tightening the bolts. 

I now include visual tailwheel udder alignment check as part of my positive 
control check before flight..even a little misalignment results in nasty 
directional behavior right after the wheels leave the ground and right after 
they touch down.

Cheers,

Tom

 

 

Sent from Windows Mail

 

From: Michael Stockhill <mailto:[email protected]> 
Sent: ‎Tuesday‎, ‎July‎ ‎25‎, ‎2017 ‎8‎:‎40‎ ‎PM
To: [email protected] <mailto:[email protected]> , Laurie 
Hoffman <mailto:[email protected]> 

 

Thanks Laurie and Ian.

 

I've owned my Dimona 16 years.  I have about a thousand hours in taildraggers 
up to a DC-3, owned a Cessna 180, and flew a dehavilland Beaver for a few 
seasons before moving onto other things.  I have flown many different tailwheel 
types and must say that my Dimona's ground handling is the most sensitive (to 
the point of occasionally being seriously uncomfortable) of anything I recall 
having flown. (When I asked the previous owner about crossword handling, he 
said to just go someplace else.)

 

There were at least a couple instances where I had PIO on the rudders during 
landing before I determined that the tailwheel fork had been repaired with zero 
degrees castor or rake. It was very squirrelly and easy to over control on the 
ground before I reworked the tailwheel fork. That made it much better, but it 
has always wanted to head for the weeds (to the right) as the tail comes up for 
takeoff. (Perhaps when the tailwheel leaves the surface.)

 

Much of the time I attributed this to habitual taildragger habit patterns of 
using right rudder during takeoff to compensate for P factor and gyroscopic 
effects rather than left rudder on the Dimona.

 

Inflight handling, trim, and rigging are fine, other than pretty heavy ailerons 
in powered cruise flight.

 

Although the book suggests a three point takeoff, I have always raised the tail 
at thirty knots or so (I have never really noted that speed as it is only when 
the airplane is ready, so don't hold me to that number). Wings are level with 
no aileron input to cause adverse yaw, but there is a significant yaw excursion.

 

I seem pretty much used to this now, but have been working with a friend so he 
can fly my bird.  He was a Naval aviator--a Top Gun spin instructor in F-18s 
etc.  After a few takeoffs threatening a visit with the weeds he said he's 
never flown anything before that he couldn't comfortably take off.  I have 
offered to come up with a way of providing him with a cat shot!

 

This doesn't seem normal. It is like there is quarter right rudder as the 
tailwheel leaves the ground, so we have lots of fun overcorrecting.

 

I really want to revisit neutral rudder and tailwheel to see if there is any 
deflection, but last time I looked I couldn't see anything out of the ordinary. 
I will get into the service manual soon (after an engine repair on my PIK-20E, 
with is another eventful story) and look into rigging.

 

So anyway, what do you folks experience?  This is way more than P factor. It is 
always a challenge to stay anywhere near the runway centerline on takeoff roll. 
I tend to let it find a line it likes rather than risk overcontolling.  None of 
this seems normal for an aircraft with a long tail arm, although the maingear 
seems quite a bit forward of most designs and configurations.

 

Cheers,

 

Michael

 

On Jul 25, 2017 4:48 PM, "Laurie Hoffman via dog" <[email protected] 
<mailto:[email protected]> > wrote:

I get the impression that Michael experiences the aircraft pulling to the right 
on most/all of his take offs on rotation?

 

Cross winds would explain only some of these. I can't recall ever noticing it 
Michael. Is it yawing only or is there some initial roll there too?

 

If you simulate the low speed flight in the air does that reproduce it? 
Possibly a rigging or control deflection issue.

 

Best Regards

Laurie 

 

 

 

 

 


  _____  


On Tuesday, July 25, 2017, 10:33:18 PM GMT+10, Ian Mc Phee <[email protected] 
<mailto:[email protected]> > wrote:

 

 

Yep RHS x winds are always an issue.  Have a look at the bight of prop and 
upward going prop and downward going prop. Big difference

 

Ian McPhee 

0428847642 

Box 657 Byron Bay NSW 2481 

 

On 25 Jul 2017 10:03 am, "Michael Stockhill" <[email protected] 
<mailto:[email protected]> > wrote:

Have any Dimona operators found that their bird diverges to the right when 
rotating for takeoff? Mine consistently does that as the tailwheel lifts off. 
After 400 or so flights I think I am past adding right rudder for a prop that 
turns contrary to all the taildraggers I have flown.

 

 Michael Stockhill 

Polson MT

 

On Jul 22, 2017 3:23 PM, "Laurie Hoffman via dog" <[email protected] 
<mailto:[email protected]> > wrote:

Rob you forgot to mention that on two of those occasions when we had prop work 
done, that there were other faults also.

The blades looked like they had been refinished by someone who had never spray 
painted before. At least once there was an issue with seal installation with 
grease being sprayed everywhere on use.

Laurie

Sent from Yahoo7 Mail on Android 
<https://overview.mail.yahoo.com/mobile/?.src=Android> 

 

On Sun, 23 Jul, 2017 at 6:16 am, Ian Williams

<[email protected] <mailto:[email protected]> > wrote:

Hi Rob,

Can you explain the difference in TBO between the BT and T blades ?   I thought 
both were the same.

Best regards

Ian Williams

Sent from my iPad


On 22/07/2017, at 7:51 PM, Rob Thompson <[email protected] 
<mailto:[email protected]> > wrote:

I just heard that GFA has adopted the CASA rules on overhauling propellers. See 
http://services.casa.gov.au/airworth/airwd/ADfiles/equip/prop/PROP-001.pdf

 

This means that as soon as it is documented in the system there is no longer a 
calendar time for overhauls.  

 

Ian McPhee has been dealing with Prop Care (www.propcare.com.au 
<http://www.propcare.com.au> ) in Brisbane for Hoffman overhauls and hopefully 
they will be soon doing work on Hoffman props.

 

We are continuing to have a nightmare run with Eric at Australian Air Props at 
Bankstown. 3 times in the past 2 years our prop has come back to us with 
problems. Once WAY out of balance then next time set much too coarse and only 
pulling 2000 at full power. Then recently he sent it back to us with the 
counterweights set incorrectly and the rpm was fluctuating on run up and early 
take off roll. 

 

Add to that he charges a fortune because he knows that the only other option in 
Australia is to send the props to Germany. Up near $4000 now for about 10-15 
hours work.

 

Fingers crossed that the Brisbane mob will be able to do them.

 

Rob Thompson

0429 493 828

 

 

 




  _____  


From: [email protected] <mailto:[email protected]>  
<[email protected] <mailto:[email protected]> > on behalf of 
Michael Stockhill <[email protected] <mailto:[email protected]> >
Sent: Monday, 17 July 2017 4:23 AM
To: [email protected] <mailto:[email protected]> ; Laurie 
Hoffman
Subject: Re: [DOG mailing list] H36 Ignition Switch (and brakes) 

 

For what it is worth, the mag switches on my Aztec with similar magnetos are 
rated at 6 amps 125V a.c./dc.  The p lead grounds the primary coil. I found one 
source that says the primary coil puts out about 150 volts. The secondary coil 
puts out 10-15000 Volts. 40 amp or even 20 amp rated switch looks like overkill 
for whatever reason. Maybe consevative because we only get one of them. 

 

Michael

 

On Jul 15, 2017 1:29 AM, "Laurie Hoffman via dog" <[email protected] 
<mailto:[email protected]> > wrote:

Hi Tom and Mike,

 

Rob and I have the wreck of an H36 from which we have salvaged many parts for 
our functioning H36, especially the L2400 which we had top overhauled.

 

Tom, I gritted my teeth and dived back into the wreck to recover the ignition 
switch and a panel switch. The wreck is already well dismantled however I still 
had a cow of a job getting access to the switches and removing these. I dread 
to think how much time it would take to install a new switch in the original 
position in a complete panel. My strong recommendation is that if you have an 
ignition switch failure seriously consider installing a new switch in another 
location on the panel, simply reroute the wiring from the old to the new and 
then cover up the old switch and placard the new.

 

Although psychically the switch toggles and bodies appear the same, the 
switches have a very different rating. The panel switch is rated 15A while the 
ignition switch is rated 40A!

 

The link that you posted to a new switch I just noticed is only rated 20A. 
Maybe something like this one Tom.... 

Longacre 45423 40 Amp Weatherproof Toggle switch #1731 | eBay 
<http://www.ebay.com.au/itm/Longacre-45423-40-Amp-Weatherproof-Toggle-switch-1731-/272686767789?epid=708201179&hash=item3f7d65dead:g:4QcAAOSw~FJZJvde>
 

 





$ 22.95 

        


  <https://s.yimg.com/nq/storm/assets/enhancrV2/23/logos/ebay.png> 


Longacre 45423 40 Amp Weatherproof Toggle switch #1731 | eBay


Longacre 45423 40 Amp Weatherproof Toggle switch #1731 in | eBay!

        

 

 

In Oz I have found Narva (driving light manufacturers) switches which look 
suitable. Heavy duty and this one rated at 50A for 12v.

Heavy Duty - Products - Narva 
<http://www.narva.com.au/products/browse/heavy-duty-2> 

 


        

Heavy Duty - Products - Narva

        

 

 

The wreck is a Mk2 by the way while our operational H36 is a Mk1 so if anyone 
needs a good Mk2 wing or two, let us know!

 

 

 

Re hydraulic fluid, we use only OM16 which I gather is equivalent to 5606.

 

Best Regards

Laurie 

 

 

 


  _____  


From: Michael Stockhill <[email protected] <mailto:[email protected]> >
To: [email protected] <mailto:[email protected]>  
Sent: Saturday, 15 July 2017, 10:13
Subject: Re: [DOG mailing list] H36 Ignition Switch (and brakes)

 

Hi Tom et al 

 

I think I found that the MS  O rings are okay.  Mine were fine through two 
rebuilds (preventative maintenance each time I  put on new tires) over 16 years.

 

Mike

 

 

On Jul 14, 2017 10:01 AM, "Tom Preisser" <[email protected] 
<mailto:[email protected]> > wrote:

Hi Laurie,

 

I have what I believe to be an ignition switch in my spares.  Can't be positive 
without digging behind the panel to look at my installed switch, but you can 
check your removed switch against it.  The spec is MS 35058-22 
http://www.bandc.aero/ toggleswitch-MS35058-22.aspx 
<http://www.bandc.aero/toggleswitch-MS35058-22.aspx> 

 

And I think it could be a different spec to the other fuel pump, etc switches 
(beefier), given that it has a separate entry than the 15A switches in the old 
H36 parts manual (with part numbers no longer valid for Diamond)...

 

BTW on brakes (and thanks Mike for your advice)... just now installing a new 
caliper piston which makes the O ring fit much better in the cylinder (seems I 
had to take off too much corroded material from the groove of the original 
installed one, so it no longer sealed tightly)...

 

For those of you running DOT3 fluid, I have obtained some EPDM O-rings to use 
rather than the BNR (nitrile) MS-28775-218 O-rings supplied to me by Diamond 
(which they may have sent probably because the HK36 and DA20 use 5606 aviation 
brake fluid).  See this RAS thread for the details on why BNR is not suitable 
for DOT3...

https://groups.google.com/ forum/#!topic/rec.aviation. soaring/4MiwHrkryFg 
<https://groups.google.com/forum/#%21topic/rec.aviation.soaring/4MiwHrkryFg> 

 

And I talked to a lady who has worked at Cleveland Brakes for decades, and she 
gasped!! when I said that Hoffmann used DOT3.  She says Cleveland only 
recommends aviation brake fluid - but I'm sticking with DOT3 as per the US type 
certificate!

 

Cheers, 

 

Tom

 

 

On Thu, Jul 13, 2017 at 7:26 PM, Laurie Hoffman via dog 
<[email protected] <mailto:[email protected]> > wrote:

Hi All,

 

After extensive investigation into intermittent electrical problems eventually 
developing into a situation where the motor had to be shut down in flight due 
to rough running, it appears that the culprit is the ignition switch.

 

Physically, the switch appears identical to the other original panel toggle 
switches operating fuel pump, avionics, strobe etc.

 

Does anyone know if they are the same switch and also is there anyone out there 
in DOG land who might have specs for the switches?

 

Best Regards

Laurie 

 

 

 

 


  _____  


From: Greg Wilson <[email protected] <mailto:[email protected]> >
To: [email protected] <mailto:[email protected]>  
Sent: Sunday, 18 June 2017, 8:10
Subject: [DOG mailing list] Easy fit ADSB

 

These are a very easy install and cheap too.

https://www.recreationalflying.com/threads/wow-these-are-good-looking-gadjets.161803/


Greg Wilson



 

 

 



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