Jump to content

Recommended Posts

Posted
5 hours ago, MooneyAcolyte said:

I'm in the process of making replacement covers from carbon fibre as owner-produced parts as per FAA (see FAR 21.9 (a)(5)) and EASA (CS-STAN for standard changes according to 21.A.307(b)4). I'll report here on my prototypes and whether or not I get them approved by my A&P/IA (due end of February '25). Perhaps we can make a co-op effort to get enough wheel covers for everyone. I know Lasar is selling them for 1,4 k$ each here: https://lasar.com/doors/inner-main-gear-door-550060-001?rq=gear door

Be a little more careful, An OPP requires same material choice. I would suggest a “repaired part” with the carbon fiber being used. Since it is a minor repair by definition, no 337 required. 
-Matt

  • Like 1
Posted
Be a little more careful, An OPP requires same material choice. I would suggest a “repaired part” with the carbon fiber being used. Since it is a minor repair by definition, no 337 required. 
-Matt

I’ll try the EASA avenue first. Here in Europe, we have the freedom of “standard change” that allows us to make minor changes to certificated, non-complex (Part-M) aircraft.
Any chance you can point me to the applicable FAR on material equivalency, as I seem to be unable to find it?


Sent from my iPhone using Tapatalk
  • Like 1
Posted
19 minutes ago, Oscar Avalle said:

I was about to ask the same can these inner doors be added to a M20C?

I don't know what would be required but Don Maxwell told me he put them on some J-bar airplane (maybe an F, don't remember) and the air loads were so great it was really hard to raise the gear.

Posted
45 minutes ago, Oscar Avalle said:

I was about to ask the same can these inner doors be added to a M20C?

One of my hangar neighbors that has an M20A said there was a local with an M20C that put the lower doors on.   They did the engineering to resize the helper springs due to the increases aero load and had new springs wound.   Apparently that worked well.   I've no idea where that airplane is now, though, as I don't think it's around here any more.

Might make it exciting to take the doors back off again, too.  ;)

In any case, like anything it can be done, but it isn't as straightforward as just attaching them to the gear.

  • Like 1
Posted
56 minutes ago, EricJ said:

One of my hangar neighbors that has an M20A said there was a local with an M20C that put the lower doors on.   They did the engineering to resize the helper springs due to the increases aero load and had new springs wound.   Apparently that worked well.   I've no idea where that airplane is now, though, as I don't think it's around here any more.

Might make it exciting to take the doors back off again, too.  ;)

In any case, like anything it can be done, but it isn't as straightforward as just attaching them to the gear.

But, it sounds like he did it correctly. Not sure it's worth the work for 5 kts, but what the heck.

  • Like 1
Posted
16 hours ago, PT20J said:

But, it sounds like he did it correctly. Not sure it's worth the work for 5 kts, but what the heck.

I'm not sure it's worth 5 kts.    ;)

Posted (edited)
23 hours ago, MooneyAcolyte said:

Any chance you can point me to the applicable FAR on material equivalency, as I seem to be unable to find it?

There is no equivalent for EASA CS-STAN ("standard change") in US rules, however, the FAA has two routes for "minor change" and "major change", these are done with logbook signature and 337 forms (with an IA) 

You can argue that FAA "minor change" route is equivalent to EASA "standard change" route (CS-STAN), however, these things gets highly mixed up and there is no one-to-one (in EASA, you can use some ASTM UL fuels with CS-STAN as long as they are approved for engine, all you need is logbook signature while in FAA rules this require an airframe STC)

For major changes, if you see them in a given N registration, you can request all 337s in CD-ROM from FAA for that registration (these should include all 337s major mods that are done via field approvals as well as STCs, even those associated with serial numbers) 

In EASA land, you can look at similar "well trodden" paths...

https://www.easa.europa.eu/download/stc/MajCh-Digital-Certificate-Publication-Report.pdf

 

 

 

Edited by Ibra
  • Like 1
Posted (edited)

On the topic, how does one go about getting these approved? something looks fishy !

FB_IMG_1734902913184.jpg

Edited by Ibra
  • Like 3
  • Haha 3
  • 2 weeks later...
Posted
40 minutes ago, MooneyAcolyte said:

I have started making the moulds.

IMG_8019.jpg

The Mooney part is made from two pieces of aluminum sheet metal riveted together. Are you going to make a mould for each piece and then bond them together, or are you planning on making one thick piece of fiberglass? That will be quite a bit heavier if you do that.

  • Like 1
Posted (edited)
13 minutes ago, N201MKTurbo said:

The Mooney part is made from two pieces of aluminum sheet metal riveted together. Are you going to make a mould for each piece and then bond them together, or are you planning on making one thick piece of fiberglass? That will be quite a bit heavier if you do that.

Making two a side is exactly the plan. I plan 4 carbon fibre layers for each "side" to get the thickness right. Then, I trim the inside and bond it  - for a total of 8 layers - at exactly the same surfaces as where the original part is riveted. I still have to decide on the vacuum bagging approach (low or high vacuum). In my experience, 70 - 80% of the work is in making the moulds. Since I have to make 4 (inside, outside times left and right), that mike take a while. I have experimented with a prototype (car fuel port lid) that was very similar and that worked splendidly.

 

 I'll keep you posted. 

Edited by MooneyAcolyte
correction
  • Like 3

Join the conversation

You can post now and register later. If you have an account, sign in now to post with your account.

Guest
Reply to this topic...

×   Pasted as rich text.   Paste as plain text instead

  Only 75 emoji are allowed.

×   Your link has been automatically embedded.   Display as a link instead

×   Your previous content has been restored.   Clear editor

×   You cannot paste images directly. Upload or insert images from URL.

×
×
  • Create New...

Important Information

We have placed cookies on your device to help make this website better. You can adjust your cookie settings, otherwise we'll assume you're okay to continue.