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500A IO-550 Conversion

 
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floydgm(at)hotmail.com
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PostPosted: Fri Aug 17, 2007 6:11 pm    Post subject: 500A IO-550 Conversion Reply with quote

Merlyn Products currently has an IO-550 STC project in the works for the
500A. Rumor has it anyway.

Mike
Northern Commanders LLC

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nico(at)cybersuperstore.c
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PostPosted: Fri Aug 17, 2007 8:16 pm    Post subject: 500A IO-550 Conversion Reply with quote

Very interesting, Mike.
If you look on the TCFG website (www.aerocommander.com) click on Aircraft
Models > Piston Twins > 500 A Colemill, you will see that I posted a picture
of what I believed at the time to be of a 500A Colemill. The specs, however,
are of a straight 500A because I had nothing on the Colemill.
You will also see that there are some pictures of a 500B Merlyn with its
four-blade props and all. The specs on the Merlyn page are of a straight
500B because I have nothing on the Merlyn either. (Does anyone have specs
and history on these models?)
Do you know whether what I have on the website are genuine Colemill and
Merlyn mods or are they experimental aircraft? Also, do you know how the
Merlyn would stack up against the Colemill, in your opinion?
Thanks
Nico

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floydgm(at)hotmail.com
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PostPosted: Fri Aug 17, 2007 8:37 pm    Post subject: 500A IO-550 Conversion Reply with quote

I do not know the answers to all of your questions but here is the website I
have found:

http://www.merlynproducts.com/commander.html

I am in Spokane right now and will find out on Monday what Merlyn is doing.

Mike
Northern Commanders LLC

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barry.collman(at)air-brit
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PostPosted: Sat Aug 18, 2007 4:29 am    Post subject: 500A IO-550 Conversion Reply with quote

Hi Nico,

By clicking on "Aircraft Models > Piston Twins > 500A Colemill", I couldn't find a photo of the Colemill 500A (Colemill Super 300), but did find photos of the Merlyn 500B. (Aircraft Models > Piston Twins > 500B Merlyn).

Let me know the registration of the Colemill 500A and I'll check it out.

Merlyn Commanders
The Merlyn 500B pictured is almost certainly s/n 1155-84, N6258X.
While owned by Jerry W Rodgers and PG&E Inc., this had Lycoming TIO-540-J2B(D) 350hp engines with Hartzell HC-C4YR-2UF/FC6660 4-blade propellers, signed-off as installed on August 23rd 1995.
These propellers are of 69.75 in. diameter, vs. the usual 80 in. of the standard 500A props.
Must make for a quieter cabin, unless the increase in fuselage/prop clearance is eaten away by an extra blade being involved.
There were Experimental - Market Survey Certificates issued on March 14th 1997 and June 11th 1997, before one in the Standard - Normal category was issued on October 7th 1997.
Jerry kindly flew me from Nashville to Oklahoma City in this Commander after the Fly-In in June 1997. He had also attended the Fly-In held at San Antonio the previous year.
I think there's now an STC for this, SA5969NM, covering the 500B, 500U & 500S.
Model 500S serial numbers 3155, 3255 & 3319 have also had this engine installed.

Model 500B serial numbers 999-30 and 1525-187 have had Lycoming TIO-540-AE2A(MC) 350hp engines with Hartzell HC-C3YR-2UF/FC8468 or FC8468-6 propellers installed. This enables a Gross weight increase to 7,200lb under STC SA01212SE.

I would really like to get some performance figures for Commanders with these two engines.

Colemill Commanders
The 500A can be modified to a Colemill "Super 300" under STCs SA340SO and SA366SO. These also approve a GW increase from 6,000lb to 6,530lb.
(Other 500A Models can have a GW increase from 6,000lb to 6,250lb if Service Change No. 50 is accomplished.)
Of the 99 examples built of the 500A, at least 21 have been converted to 500B and 31 modified to Colemill "Super 300".
Additionally, the first of these 99 was converted to the first Model 680F. (s/n 500A-871-1 to 680F-871-1).

The Colemill conversion replaces the Continental IO-470-M 260hp engines with Continental IO-520-E 300hp engines.
The original Hartzell HC-A2XF-2B/8433-4 propellers are also replaced, with Hartzell EHC-A3VF-2B/V7636D.

Again, some performance feed-back for the Colemill examples will be welcome.

Very Best Regards,
Barry


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nico(at)cybersuperstore.c
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PostPosted: Sat Aug 18, 2007 6:00 am    Post subject: 500A IO-550 Conversion Reply with quote

Mike,
I visited Merlyn's website and found many interesting things, which answered
some of my questions. I am going to contact these folks for more information
and permission to publish some of their material on our website.
It appears as if these STC's are existing and flying mods. Perhaps if Bilbo
had known about these, he could have had his 500A dressed up in one of
these.
Thanks for introducing me to them.
Nico

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nico(at)cybersuperstore.c
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PostPosted: Sat Aug 18, 2007 6:12 am    Post subject: 500A IO-550 Conversion Reply with quote

Thanks, Barry. There’s a lot of useful information from your bunker of Commander intelligence about these products. I would like to incorporate that into the website, with your permission.

I posted my reply to Mike Floyd before I read your email.

Thanks
Nico



From: owner-commander-list-server(at)matronics.com [mailto:owner-commander-list-server(at)matronics.com] On Behalf Of Barry Collman
Sent: Saturday, August 18, 2007 5:27 AM
To: commander-list(at)matronics.com
Subject: Re: 500A IO-550 Conversion


Hi Nico,



By clicking on "Aircraft Models > Piston Twins > 500A Colemill", I couldn't find a photo of the Colemill 500A (Colemill Super 300), but did find photos of the Merlyn 500B. (Aircraft Models > Piston Twins > 500B Merlyn).



Let me know the registration of the Colemill 500A and I'll check it out.



Merlyn Commanders

The Merlyn 500B pictured is almost certainly s/n 1155-84, N6258X.

While owned by Jerry W Rodgers and PG&E Inc., this had Lycoming TIO-540-J2B(D) 350hp engines with Hartzell HC-C4YR-2UF/FC6660 4-blade propellers, signed-off as installed on August 23rd 1995.

These propellers are of 69.75 in. diameter, vs. the usual 80 in. of the standard 500A props.

Must make for a quieter cabin, unless the increase in fuselage/prop clearance is eaten away by an extra blade being involved.

There were Experimental - Market Survey Certificates issued on March 14th 1997 and June 11th 1997, before one in the Standard - Normal category was issued on October 7th 1997.

Jerry kindly flew me from Nashville to Oklahoma City in this Commander after the Fly-In in June 1997. He had also attended the Fly-In held at San Antonio the previous year.

I think there's now an STC for this, SA5969NM, covering the 500B, 500U & 500S.

Model 500S serial numbers 3155, 3255 & 3319 have also had this engine installed.



Model 500B serial numbers 999-30 and 1525-187 have had Lycoming TIO-540-AE2A(MC) 350hp engines with Hartzell HC-C3YR-2UF/FC8468 or FC8468-6 propellers installed. This enables a Gross weight increase to 7,200lb under STC SA01212SE.



I would really like to get some performance figures for Commanders with these two engines.



Colemill Commanders

The 500A can be modified to a Colemill "Super 300" under STCs SA340SO and SA366SO. These also approve a GW increase from 6,000lb to 6,530lb.

(Other 500A Models can have a GW increase from 6,000lb to 6,250lb if Service Change No. 50 is accomplished.)

Of the 99 examples built of the 500A, at least 21 have been converted to 500B and 31 modified to Colemill "Super 300".

Additionally, the first of these 99 was converted to the first Model 680F. (s/n 500A-871-1 to 680F-871-1).



The Colemill conversion replaces the Continental IO-470-M 260hp engines with Continental IO-520-E 300hp engines.

The original Hartzell HC-A2XF-2B/8433-4 propellers are also replaced, with Hartzell EHC-A3VF-2B/V7636D.



Again, some performance feed-back for the Colemill examples will be welcome.



Very Best Regards,

Barry





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barry.collman(at)air-brit
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PostPosted: Sat Aug 18, 2007 7:07 am    Post subject: 500A IO-550 Conversion Reply with quote

Hi Nico,

Permission granted - no problem!

Best Regards,
Barry
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KenWHyde(at)aol.com
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PostPosted: Thu Aug 23, 2007 5:32 pm    Post subject: 500A IO-550 Conversion Reply with quote

Guys,

When I saw this e-mail regarding the IO-550 conversion, I thought this is great...then I called a friend who bought a NEW Beech A36 with all the horns and whistles about 5 years ago and I ask him about the IO-550. The man knows engines...and he says "I It is the most disgusting, badly engineered piece of machinery that I can remember buying. I have had to replace at least three cylinders in 1000 hours and I am now having to replace the whole engine because corrosion has ruined the cylinders, camshafts and followers. All of this in spite of following Continental's book recommendations, Flight Safety's cooling rec's. and changing the oil every 25 hours. It is the worst aircraft engine I have ever owned and is the first that I've owned since new."
"Can you believe corrosion on an engine that averages more than 150 hrs a year. (always hanger kept)
It never actually broke down in flight!" A friend of his has a A36 plus a Baron...same engine..lots of problems, Baron making metal both engines. New airplanes guys. I'm sure others have heard the war stories. Hey, don't shoot me....I am just relaying the message.

AOL.com.
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brcamp(at)windows.microso
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PostPosted: Fri Aug 24, 2007 8:52 am    Post subject: 500A IO-550 Conversion Reply with quote

The IO-550 had a recall just after I bought mine. They had a number of poorly nickelled cylinders and wanted everyone who bought one to get an inspection, then the bad cylinders would be replaced. I never thought that would work, since they didn’t keep track of the serial numbers of the bad cylinders, or what engines they went on. I was, BTW, highly less than thrilled to be exposed to having my factory new engine turn into a field overhaul to new specs at 10 hours operation time. Continental was very clear they really didn’t see that as their problem. The actual words of the TCM rep at Oshkosh were a very snarky “If you don’t like it, sue us.” It didn’t come to that because the inspection showed no problem.

I suspect he got some of those bad cylinders, and they didn’t find them in the inspection, or something similar.

Just to be clear, I don’t personally recommend TCM engines, period. I think their customer orientation and business practices are very poor indeed. I *do* think that if you are using IO 520s that the IO 550 is a better deal from a number of directions, for essentially the same price. But, if you can upgrade from IO520s to current production Lycomings (500A to 500B conversion+STC(?)) that would be better still.

  Bruce

From: owner-commander-list-server(at)matronics.com [mailto:owner-commander-list-server(at)matronics.com] On Behalf Of KenWHyde(at)aol.com
Sent: Thursday, August 23, 2007 6:32 PM
To: commander-list(at)matronics.com
Subject: Re: 500A IO-550 Conversion



Guys,



When I saw this e-mail regarding the IO-550 conversion, I thought this is great...then I called a friend who bought a NEW Beech A36 with all the horns and whistles about 5 years ago and I ask him about the IO-550. The man knows engines...and he says "I It is the most disgusting, badly engineered piece of machinery that I can remember buying. I have had to replace at least three cylinders in 1000 hours and I am now having to replace the whole engine because corrosion has ruined the cylinders, camshafts and followers. All of this in spite of following Continental's book recommendations, Flight Safety's cooling rec's. and changing the oil every 25 hours. It is the worst aircraft engine I have ever owned and is the first that I've owned since new."

"Can you believe corrosion on an engine that averages more than 150 hrs a year. (always hanger kept)

It never actually broke down in flight!" A friend of his has a A36 plus a Baron...same engine..lots of problems, Baron making metal both engines. New airplanes guys. I'm sure others have heard the war stories. Hey, don't shoot me....I am just relaying the message.





AOL.com.
Quote:
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Quote:
1
Quote:
2
Quote:
3
Quote:
4
[quote][b]


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asgroup(at)tampabay.rr.co
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PostPosted: Fri Aug 24, 2007 10:37 am    Post subject: 500A IO-550 Conversion Reply with quote

All,

First, I must have missed it, but what airframes is the IO550
conversion for, and who offers the STC? Thx.

Now, I must comment on the Continental vs. Lyc debate, and we could
run this forever. But, I'm running a pair of IO550Cs in our Baron
that have performed flawlessly over the last 800 hours since new.
I've also got 1000s of hours behind the 520s and the Lyc TSIO 540s.
They both have their goods and bads and issues. I've had fairly good
luck with all of them. I did have to top the Lycs but I haven't had
but a few cylinders of of the Continental 520 and 470s over ~5000
hours of operation, and most go beyond TBO. The Continentals seem to
be more fuel efficient but the Lycs seems to be stronger. Just a
feeling.... no data.

Food for thought.

Larry Olson
St. Pete
On Aug 24, 2007, at 12:51 PM, Bruce Campbell wrote:

Quote:
The IO-550 had a recall just after I bought mine. They had a
number of poorly nickelled cylinders and wanted everyone who bought
one to get an inspection, then the bad cylinders would be
replaced. I never thought that would work, since they didn’t keep
track of the serial numbers of the bad cylinders, or what engines
they went on. I was, BTW, highly less than thrilled to be exposed
to having my factory new engine turn into a field overhaul to new
specs at 10 hours operation time. Continental was very clear they
really didn’t see that as their problem. The actual words of the
TCM rep at Oshkosh were a very snarky “If you don’t like it, sue
us.” It didn’t come to that because the inspection showed no
problem.

I suspect he got some of those bad cylinders, and they didn’t find
them in the inspection, or something similar.

Just to be clear, I don’t personally recommend TCM engines,
period. I think their customer orientation and business practices
are very poor indeed. I *do* think that if you are using IO 520s
that the IO 550 is a better deal from a number of directions, for
essentially the same price. But, if you can upgrade from IO520s to
current production Lycomings (500A to 500B conversion+STC(?)) that
would be better still.

Bruce

From: owner-commander-list-server(at)matronics.com [mailto:owner-
commander-list-server(at)matronics.com] On Behalf Of KenWHyde(at)aol.com
Sent: Thursday, August 23, 2007 6:32 PM
To: commander-list(at)matronics.com
Subject: Re: 500A IO-550 Conversion

Guys,

When I saw this e-mail regarding the IO-550 conversion, I thought
this is great...then I called a friend who bought a NEW Beech A36
with all the horns and whistles about 5 years ago and I ask him
about the IO-550. The man knows engines...and he says "I It is the
most disgusting, badly engineered piece of machinery that I can
remember buying. I have had to replace at least three cylinders in
1000 hours and I am now having to replace the whole engine because
corrosion has ruined the cylinders, camshafts and followers. All of
this in spite of following Continental's book recommendations,
Flight Safety's cooling rec's. and changing the oil every 25 hours.
It is the worst aircraft engine I have ever owned and is the first
that I've owned since new."

"Can you believe corrosion on an engine that averages more than 150
hrs a year. (always hanger kept)

It never actually broke down in flight!" A friend of his has a A36
plus a Baron...same engine..lots of problems, Baron making metal
both engines. New airplanes guys. I'm sure others have heard the
war stories. Hey, don't shoot me....I am just relaying the message.


AOL.com.

http://www.matronics.com/Navigator?Commander-Listhttp://
forums.matronics.com
http://www.matronics.com/Navigator?Commander-List_-
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BobsV35B(at)aol.com
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PostPosted: Sat Aug 25, 2007 8:41 pm    Post subject: 500A IO-550 Conversion Reply with quote

Quote:
Good Evening Ken,
Please do not consider this as being any effort to shoot the messenger!

However, I very respectfully disagree with the gentleman's impression of the engine. I think it is far and away the best effort Continental has produced in the last fifty years.

Having said that, I also feel Continental has suffered greatly from poor quality control of their products during the past fifteen years or so. The move from Michigan to Mobile resulted in the loss of a dedicated work force that has been hard to replace.

If you have a chance to discuss this with the Continental management, they will agree that there have been some problems, but they are confident those bad times are behind them.

There was a rash of cylinder problems in the nineties that most folks will agree was due to a practice of running the engine not rich enough when at high power settings.

The 550 is capable of putting out a lot of power and it takes a lot of fuel to keep it cool at those high power settings.

I like to set up a freshly majored 550 at around thirty-one to thirty-two GPH for the initial takeoff until such time as the fuel balance can be determined. Once it has been assured that the distribution between the cylinders is reasonable, I like to see about twenty-nine GPH for a sea level, standard conditions, takeoff.

Unfortunately, most mechanics seem hesitant to push that much fuel through the engine.

Rather than get into an argument as to how much fuel is needed to develop that sort of power, may I tell of my experience with the engine? I had one installed in my Bonanza at the height of Continental's problem time frame. It was in 1996.

It was without doubt the best money I have ever spent on any airplane. The increase in performance was a LOT more than I had anticipated. That engine currently is ready to be replaced and it has never had any jug removed. It has suffered from the Continental valve leakage problems during it's regular compression check, but by following the Continental recommendations on using a calibrated orifice and checking low cylinders with a borescope, the engine has easily made it to TBO. I currently have another 550 being built up by a boutique engine shop to replace the factory remanufactured one that I first had installed.

Since that time, two of our sons have purchased 550s that were rebuilt by a custom overhaul shop and both those engines have performed marvelously without suffering the low compression readings common with those 1990 through 1999 factory cylinders. It is my understanding that Continental had gone to the practice of using pre fit valves instead of seating them individually as had been done in the past. While that led to bad compression checks, it did not seem to cause any serious leakage under actual operating conditions. That is why Continental developed their special Service Bulletin which includes using the calibrated orifice and the borescope to ascertain the suitability of continued operation of the cylinders.

There is no doubt that I can find you plenty of folks who will tell you that the 550 is no good. I can easily find you another couple of hundred users who think as I do.

There is also no doubt that the engine does need to be set up properly.

Most of the earlier Bonanza installations used an Altitude Compensating Fuel Pump. That system works great, but it takes a bit more care to be set up properly. Beech has quit using it.

A few old line mechanics don't care to learn how to do the setup and that can cause problems. Continental has a very complete set of instructions and if they are followed by the operator, the Altitude Compensating Pump works great. No need to lean on takeoff at higher elevations and altitude changes can be made without the necessity of constant adjustment.

We who have those pumps and have had then set up as Continental has advised have had great results.

This has been a bit if a rambling discourse and for that I am sorry, but as in so many cases of opinions, it is hard to know where to start. As I said earlier, I consider it to be a great engine. It is light and powerful. When the fuel control is setup the way the manufacturer suggests, it works wonderfully. Those folks who chose to run high powers with lean mixtures have encountered problems, but those of us who have chosen to operate them within the design parameters have had excellent performance. In fact, we who operate them at lower powers on the lean side of peak EGT have had exceptional service from the engines. I would be happy to discuss specifics with anyone who has the time and the data to share.

The IO-550-B is a marvelous engine!

Happy Skies,

Old Bob
AKA
Bob Siegfried
Ancient Aviator
Stearman N3977A
Brookeridge Air Park LL22
Downers Grove, IL 60516
630 985-8503


In a message dated 8/23/2007 8:33:32 P.M. Central Daylight Time, KenWHyde(at)aol.com writes:


Guys,

When I saw this e-mail regarding the IO-550 conversion, I thought this is great...then I called a friend who bought a NEW Beech A36 with all the horns and whistles about 5 years ago and I ask him about the IO-550. The man knows engines...and he says "I It is the most disgusting, badly engineered piece of machinery that I can remember buying. I have had to replace at least three cylinders in 1000 hours and I am now having to replace the whole engine because corrosion has ruined the cylinders, camshafts and followers. All of this in spite of following Continental's book recommendations, Flight Safety's cooling rec's. and changing the oil every 25 hours. It is the worst aircraft engine I have ever owned and is the first that I've owned since new."
"Can you believe corrosion on an engine that averages more than 150 hrs a year. (always hanger kept)
It never actually broke down in flight!" A friend of his has a A36 plus a Baron...same engine..lots of problems, Baron making metal both engines. New airplanes guys. I'm sure others have heard the war stories. Hey, don't shoot me....I am just relaying the message.





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