• Welcome to the new Commander Owners Group Forums. Please bear with us as the kinks are worked out and things are tweaked. If you have any questions or issues with the new platform, please post them here.

New Cowling Update

carllee

Sponsor
Supporting Member
Sponsor
Aircraft Year
1974
Aircraft Type
112 Hot Shot
Reg Number
N1144J
Serial Number
186
The third new cowling is being fitted. This time on a 114. These are a huge step forward in strength, weight savings, and quality.
 

Attachments

  • 114 fit.jpg
    114 fit.jpg
    191.9 KB · Views: 0
Loaded question - how close are you going public?

I just received an estimate for 1K$ for cosmetic work for my (serviceable) upper cowling. (spider cracks in the finish + numerous nicks and dings)

Sure like to put that toward a more permanent fix. And with the Scimitar up front 'any' weight reduction is appreciated.

Q: Will the cowl include the oil and gasolator access panels? Duze and Latches?
 
Loaded question - how close are you going public?

I just received an estimate for 1K$ for cosmetic work for my (serviceable) upper cowling. (spider cracks in the finish + numerous nicks and dings)

Sure like to put that toward a more permanent fix. And with the Scimitar up front 'any' weight reduction is appreciated.

Q: Will the cowl include the oil and gasolator access panels? Duze and Latches?

Hi John,

The original cowlings really cant be "fixed". When the factory layed up the original cowls they didn't properly impregnate the fiberglass with resin. There's a couple of dry layers in the middle, so there's an inner shell and and outer shell. When there's heat on the inside and cold on the outside the inner and outer shells work against each other. Fixing cracks is just adding layers to the outer shell. Many of our planes have had their cowls repaired over and over - adding layer after layer to the outer shell. That's why they weigh 40+lbs, and continue to crack again and again.

The new cowls are owner produced parts, so you would need to ask your IA if he will accept it if you produce it. It works like this:

$2,500 for the material, and to rent the mold from RCM
$1,500 to pay RCM's labor
$500 custom latch system (optional)
Shipping depends on your region $300 - $500 in the US - estimated.

These are universal parts. They fit: 112,112A,112B,114,114A

They do not include: latches, side scoops, oil doors, landing light nacelles, cowl flaps. All of these parts need to be transferred over from the original cowl.
 
Bless You Sir for the quick response,

My IA is 'very level-headed' and I'm sure he'd go for it. Will see him this week and will discuss.

Q: Are you in Tyler or CA? If Tyler I could get my friend from MS to use his King Air and deliver the new cowl . . .:p

I'm authorized one dumb question a day at work, so I'll burn it here / now. Prices you describe above is for the 'upper and lower' cowl set?

You probably shared with us at the Fly-In's but is there any literature / flyers describing the new cowl?

Custom latch??
 
Carl

​​​​​​Can the top cowl be used with an original bottom.?
I know the TCA is not on the list due to the larger cooling opening but isn't the top cowling pretty close?
 
Carl

​​​​​​Can the top cowl be used with an original bottom.?
I know the TCA is not on the list due to the larger cooling opening but isn't the top cowling pretty close?

Not without modification, but I believe it could be done, and would probably/maybe be easier than trying to rebuild an original.
 
Where do I send the check?
 
Hi Mark,
I'm in California right now. Call when you get a chance

805-215-2982
 
What material is the new cowling made from? How would we attach the oem air inlets, oil doors and headlight to the new part?
 
Not without modification, but I believe it could be done, and would probably/maybe be easier than trying to rebuild an original.

I would go in with Joel if we did end up pursuing a mod for the TCs.
 
What material is the new cowling made from? How would we attach the oem air inlets, oil doors and headlight to the new part?

The pricing above is for carbon fiber. If you want fiberglass it's $500 cheaper, but 8-10 lbs heavier.
Around 27-29 lbs instead of 19.

If you know of someone in your area that does fiberglass work doing the scoops, landing light, and oil doors is easy.
 
I would go in with Joel if we did end up pursuing a mod for the TCs.

I'd be willing to work with you on this, if a couple of TC/TCA owners want to commit to orders. I think I could come up with a forward lower section that could be spliced into the new lower cowl.
 
I'd be willing to work with you on this, if a couple of TC/TCA owners want to commit to orders. I think I could come up with a forward lower section that could be spliced into the new lower cowl.


The TC does have heat/heat shield requirements that we'll have to figure in.
However we're nose heavy to begin with - this helps and also a new part.

We should discuss.

Not many moving parts on the upper cowl - access door for the oil/gascolator ; latches and the screw points to the lower cowling in the front.

i'd be interested.
 
The TC does have heat/heat shield requirements that we'll have to figure in.
However we're nose heavy to begin with - this helps and also a new part.

We should discuss.

Not many moving parts on the upper cowl - access door for the oil/gascolator ; latches and the screw points to the lower cowling in the front.

i'd be interested.

Me too!!
 
My understand is the cowl being presented is for a 114. My 114 1976 does not have screws for securing the top cowl as it has 2 latches on each side.
 
My understand is the cowl being presented is for a 114. My 114 1976 does not have screws for securing the top cowl as it has 2 latches on each side.

From post #4


These are universal parts. They fit: 112,112A,112B,114,114A

"They do not include: latches, side scoops, oil doors, landing light nacelles, cowl flaps. All of these parts need to be transferred over from the original cowl."
 
The TC does have heat/heat shield requirements that we'll have to figure in.
However we're nose heavy to begin with - this helps and also a new part.

We should discuss.

Not many moving parts on the upper cowl - access door for the oil/gascolator ; latches and the screw points to the lower cowling in the front.

i'd be interested.

I took out my metal shield years ago. Jim has a blanket that is light, oil resistant, and I never see my cowl temp probe over 80 deg (it's placed above the turbo between the blanket & the fiberglass). Haven't cracked the fiberglass since I installed it. I'm ok right now but would be onboard if something breaks.

I think Sherman has a blanket too. k
 
Last edited:
From post #4


These are universal parts. They fit:

"They do not include: latches, side scoops, oil doors, landing light nacelles, cowl flaps. All of these parts need to be transferred over from the original cowl."

The first post says it is for a 114 and #4 post is universal parts that are on 112,112A,112B,114,114A. The cowl, if I am reading it right, is not for a 112.
 
My understanding, years ago from Sid. Is that the 114 being a 6 cyl is much heavier up front than the 112 or TC. Also he shared flying with me. That the TC cowl is MUCH shorter than the 114 cowl and my 'over the nose visibility' is much better. Especially during landings. He also said our over the nose 'slope ', increasing visibility is 'somewhat steeper'. So many details to explore!

Right Kelly, I have Aerodymes heat shield blanket which I believe cut 2# weight from the steel shield ( which did get hot too) under the top cowl.

Not home so don't have my W&B sheets
handy.

So right, these issues would have to be addressed with a new cowling. The TC also uses an extended prop hub.

So in addition to all the other misc 'Owner Produced Parts' that would have to transfer, we TC owners need to concern ourselves with how the new cowl would align (length) with the lower cowl AND the extended hub.
 
As stated in the original post it is a universal part that fits the following: 112,112A,112B,114,114A. It's already been fitted to both a 112, and a 114.

It would fit perfectly onto the 112TC/TCA airframe, but wouldn't work because the inlets are different. The 112TC/TCA's engine is cooled by air being forced from bottom-to-top rather than, the traditional, top-to-bottom. As Joel stated above the new upper cowling would work fine, as it is, I would just need to crate a mold for a new 112TC/TCA lower cowl that would match up with the new upper.

The 114B, 114TC, 115, and 115TC's are different. The propellers have a 3" extension on them, so the cowlings are longer. These models are obviously not included in this program.
 
Last edited:
Back
Top