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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 02:22 
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I’d think the LOA from the administrator supersedes any need for another one from the local FSDO.

I thought all LOAs were by definition issued to a specific operator. While what you’re saying would be hugely useful and basically one LOA could (should!) be used for every turbine (i.e. allow the MMEL to always be usable without another specific LOA), I would think there is no such thing as a “blanket LOA”. But… ?

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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 02:34 
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Username Protected wrote:

I’d think the LOA from the administrator supersedes any need for another one from the local FSDO.

I thought all LOAs were by definition issued to a specific operator. While what you’re saying would be hugely useful and basically one LOA could (should!) be used for every turbine (i.e. allow the MMEL to always be usable without another specific LOA), I would think there is no such thing as a “blanket LOA”. But… ?


yeah this kind of bureaucracy is infuriating but I suppose it keeps some folks employed. If it's not a blanket LOA its certainly a form sent out to everyone who asks, but I'll confirm when I'm at the hangar next time. I recall looking at this recently.
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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 08:31 
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One thing to note is that the MMEL from the OEM is for the standard equipment. Those of us with highly Garminized panels will need to modify that MMEL to match our panels.


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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 08:52 
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Go to you tube and watch some famous Jet pilot Vlogs. Many are flying solo and at or above 40K with no masks on. Seems the reg is regularly ignored.


I’ve actually never seen a jet pilot wear a mask, not once. As Mike C. said earlier a sudden decompression event seems exceedingly rare.

Many a flight attendant saw me wearing one when in 121 operations while she was standing in the cockpit because the Capt was using the lav.
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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 08:56 
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That's not how I read reg, Mike. It says "equipment installed". All aircraft have equipment installed. But even if you're right, that means that any equipment failure, however small, grounds you without an MEL. How many of the aircraft we fly have 0 items inop or failed? I would argue no such aircraft exists.


Mike is right, you are wrong. The reg refers to flying with inop equipment. If you don't have anything inop it doesn't apply.

In 5 years of flying my TBM ALL the equipment has worked. I would get rid of it if something was always breaking.


this is correct and this is how Daher treats it. They do not include an MEL, but there are companies that will build it for a TBM owner if desired (IIRC it is around $2,500).

without that, if anything breaks in the plane, technically, it isn't operational. thankfully this rarely happens.
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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 10:20 
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Why it's tied to the operator and not the serial number is beyond me.

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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 11:24 
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Socata provides/provided an MMEL online, as Mike said you can use that as a template. We simply downloaded that for our TBM 700, submitted it with a letter to the FSDO, then waited 5 annoying months to get the LOA back.

We needed the MMEL LOA to remove an air conditioning component to send out to service and legally keep flying. By the time the LOA arrived the backordered exchange part became available.

And this folks is why I'll never own a Part 135 company - the downtime waiting on the FAA and headaches just aren't worth it to me.

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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 12:17 
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Username Protected wrote:
One thing to note is that the MMEL from the OEM is for the standard equipment. Those of us with highly Garminized panels will need to modify that MMEL to match our panels.

Well, technically, you don't have to.

In my case, I just sent in the stock MMEL for approval despite being fully Garminized.

What does that mean legally? FAR 91.213 only applies to installed equipment, so if my MEL lists something that is NOT installed, it no longer becomes part of my dispatch check against the MEL. The MMEL lists a bunch of stuff I don't have even before the mod, so this is normal.

In terms of the Garmin equipment, none of which is in the MMEL (and thus my MEL), all of it must work per FAR 91.213. If I want to get relief for some of it (say one transponder can be out), then I need to amend my MEL and get a new LOA. I chose not to do that because I inferred that any deviation from the MMEL requires more approval effort at the FSDO and thus would delay things. I just didn't want to open that can of worms for what is likely to be something I don't need.

I have attached the MMEL I used for my plane. Note that it covers all the legacy models, from 500 to 560, so it naturally contains a bunch of stuff that is not applicable to my plane even in the stock configuration.

Mike C.


Please login or Register for a free account via the link in the red bar above to download files.

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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 13:11 
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Here’s a couple of interior photos that show both more clearance between the seats and more distance between the sidewalls.

These are the types of improvements that may not impress the guy flying and buying, but they do impress the ladies who are accustomed to finer things in the transportation sector.

I once told a broker trying to convince my client to buy an older Pilatus, that he wasn’t competing with a King Air, he was competing with BMW!

A few years later Pilatus announced a new interior designed by BMW.


You're comparing aircraft interiors not types. Ask anyone who isn't a pilot to sit in both and they will tell you they like the one with the nicer carpet and leather better. If you pull out a ruler and say this one has an extra inch can't you see? They'll shrug. Few legacy citations have the original interior, so the question is which V vs which CJ? A non-pilot passenger was asked how much bigger the 441 was than the 340 and they asked me "I think it's just a little longer, right?" (441 has to be twice the size of a 340).

The Nextant Beechjet conversions added a significant amount of room by changing the insulation, headliner, etc. and two Beechjets could therefore have significantly more or less interior room. This isn't related to the aircraft type just who did the interior. You could argue a Nextant Beechjet is a different type, similar to V/CJ, as it has different engines, but then this becomes a semantic argument. At the end of the day it's still a discussion about the interior not the type.


I think you kinda missed the point of the argument, the tubes are roughly the same, so my point was that on the newer airplanes like the M2 and CJ3+, Textron has gone to great lengths to soften corners, tuck the tray tables in closer to the sidewall and redesign the drink rails to make the cabin roomier. Is it even an inch wider? I don't know, I actually measured a CJ3+ and was going to measure the V we had in prebuy at a gold plated shop, but when I went out Thursday they still didn't have the interior back in, I was with the airplane yesterday, but was so focused on getting it ready for the test flight and delivery that I didn't think to measure it.

Mike C's argument was there is no physical difference and this is roomier feel I spoke of is just an optical illusion based on colors. He's flat wrong, as he often is these days, he has fallen in to the trap he use to warn others about which is arguing about that which you have no direct experience. I've pointed out that Mike hasn't actually seen a Mustang, M2 or CJ3+, but continues to criticize them. Mike also refuses to ever admit when he is wrong, which bugs me... but it is what it is.

So, yes it is an argument about the interior, not types, and no you can't do the new style interior in legacy Citations, at least not yet.

So, the new airplanes have a roomier interior than the old ones. See photos I posted earlier for all the proof one needs... or just go sit in a new one, they're everywhere.

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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 15:57 
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Username Protected wrote:
...and no you can't do the new style interior in legacy Citations, at least not yet...



can you expand on this? what limitations are there on updating the interior on, say, a 501? seems like trimmer seats and lighter colors would add a lot of "open feel."

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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 19:16 
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Username Protected wrote:
...and no you can't do the new style interior in legacy Citations, at least not yet...



can you expand on this? what limitations are there on updating the interior on, say, a 501? seems like trimmer seats and lighter colors would add a lot of "open feel."


Yes, it requires an STC to make major changes to the interior components, things that seem benign like drink rails, tray tables and armrest all require an STC (and potentially a lot more) to have a plug and play replacement.

You can change finishes, leathers, colors... you can even change the foam and shape of the seats (within reason) but you can't change the armrest or install different tray tables or drink rails.

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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 04 Dec 2023, 23:39 
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I think you can do whatever you wanted to do to a 501; it's a part 23 airplane just like a Beech Baron. Is the Tim Hallack (or however his name is spelled) mod to the Beech line sidewalls STCd? I don't think it is. It's a minor modification and doesn't require an STC or a 337 IMO. You definitely can't mess with the seat rails but you could absolutely move things around, change tray tables, or get rid of a galley. Moving the seating arrangement such as the Sierra mod would definitely be an STC. But, modifying the arm rests...go right ahead.

Best looking mods I've seen are Ultra seats and Ultra side window shades. This really gives the interior a great look.

But, I think this is a silly conversation. There's NOTHING wrong with the legacy Citation interior. It's very comfortable and can be extremely modern and beautiful with nice materials.

Unfortunately, I never get to sit in the back so there's not much of a difference in a 1972 500 and a brand new CJ up in the cockpit other than the avionics.

Enjoy your old jet, don't try to make it something it's not, and enjoy the fact that it does 90+% of what a new one does for 10% the cost.


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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 05 Dec 2023, 00:56 
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Username Protected wrote:
.
I guess if you can train yourself not to take a breath after explosive decompression (aside of what’s blown out of your lungs forcibly), your TUC will be whatever it normally is holding your breath instead of just a couple seconds if you inhale.
If you’re a trained free diver, you might be well on your way through the emergency descent before your need to get your mask on. ;-)


Doesn't work that way. The percentage of oxygen molecules per unit air stays the same, but the molecules are now much farther apart. In essence, there are far less oxygen molecules in your lungs after your lungs involuntary empty themselves with the large pressure gradient. So you pass out all the same within seconds at FL450. You need pressurized oxygen.

Edit: reading backwards, looks like that was addressed, but the pressure delta generated by depressurization in a jet would result in death if you tried to hold your breath. That pressure differential is about 4-8 times the maximum pressure that an athletic and a normal young man can generate blowing into a closed tube.


This is a very complex physiologic subject that requires "going into the weeds" a bit and is probably not of interest to many reading about turboprops vs jets.

First I need to mention that I'm not advocating attempting to hold your breath in lieu of wearing a mask at high altitude. That much said, my post comes from this very question asked of the FAA Aeromedical officer at an AOPA fly-in at Colorado Springs after a lecture on the subject a few years ago.
Pulmonary barotrauma due to rapid decompression is actually a very rare event for those exposed in aviation, not so in diving and submarine escape. This is because the pressure differentials are huge in diving compared to aviation. The differential from 100m to the surface is about 7000mm Hg in water. Sea level to 35,000 feet in air is only about 500mm Hg. But in planes, the decompression happens faster than in ascent from depth. Still, injuries in aviation are very rare and in diving are common.
Air Force studies arbitrarily seem to set "explosive decompression" at <1sec and "rapid decompression" at >1sec. The speed has a huge effect on potential damage. But even with relatively rapid (0.1sec) decompressions from 8,000 feet to 35,000 feet in human studies of over 100 test subjects, no ill effects were noted. Above 63,000 feet, it's a kill zone due to water in the lungs vaporizing and explosive expansion causing air embolism.
If you are high enough and cabin pressure drops fast enough that you are truly exposed to explosive decompression, the pulmonary barotrauma due to dynamic pressure spike happens in the static and dynamic chest expansion phases which last fractions of a second. It doesn't matter if you are trying to hold your breath or not. Tightening your chest muscles or a tight garment will provide quite a bit of protection and can double the pressure you can tolerate before damage, but whatever happens, it will happen so fast that you won't even be able to think about it.
Around the 1 or 2 second mark as gas is escaping from your lungs, if you have not already torn your alveoli and veins apart or blown a big air embolus into your aorta (unlikely) then you are past the typical window of damage. If you then consciously retain pressure in your lungs by holding your breath, you will extend TUC. It might only be a 2psi difference, but as you know, the effect of altitude on TUC is somewhat logarithmic, not linear so every little bit can help. British studies on human subjects exposed to as much as a 5.8psi differential drop in 0.1sec showed no ill effect. Once you take that first breath, pressures equalize and as Mr. Long notes (and as I stated in my post) the lung works in reverse following the pressure gradient, deoxygenated blood hits the brain and things go dark.
Do I think this is a viable survival method for high altitudes that eliminates the need for masks? No, wear a mask if you want to maximize chances of survival in the VERY rare case of explosive decompression.
Do I think holding breath (to the degree that you can) to retain pressure in your lungs will make a difference in TUC? Yes, the same way pursed-lip-breathing can help mountain climbers at altitude suffering from HAPE when no supplemental oxygen is available.
Most loss of consciousness events in flying are due to slow, unrecognized loss of pressure, thus the advantage of the Icarus and similar systems that I mentioned if your primary warning system fails.
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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 05 Dec 2023, 01:32 
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Yes, it requires an STC to make major changes to the interior components, things that seem benign like drink rails, tray tables and armrest all require an STC (and potentially a lot more) to have a plug and play replacement.

This is incorrect.

An STC is required when you make a major alteration. Part 43 Appendix A paragraph (a) defines what are major alterations. Interior furnishings are not among them.

That hasn't stopped people from getting STCs for interior things, however. The gratuitous STC market has grown as a sort of assurance the item is suitable for installing in an airplane. Things like window shades have STCs for them. The proliferation of gratuitous STCs has created the impression they are required. Obviously the company who has an STC thingy wants to imply theirs is better. Major shops will also promote the STC packages, too, since they make money on that.

But the STC is not required for interior furnishings. It isn't a major alteration. The furnishings do need to meet certain requirements, like burn ratings and the like, but they don't need an STC. A mechanic can sign them off as a minor alteration.

Mike C.

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 Post subject: Re: Legacy Citation vs Turboprop
PostPosted: 05 Dec 2023, 01:38 
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Username Protected wrote:
Yes, it requires an STC to make major changes to the interior components, things that seem benign like drink rails, tray tables and armrest all require an STC (and potentially a lot more) to have a plug and play replacement.

This is incorrect.

An STC is required when you make a major alteration. Part 43 Appendix A paragraph (a) defines what are major alterations. Interior furnishings are not among them.

That hasn't stopped people from getting STCs for interior things, however. The gratuitous STC market has grown as a sort of assurance the item is suitable for installing in an airplane. Things like window shades have STCs for them. The proliferation of gratuitous STCs has created the impression they are required. Obviously the company who has an STC thingy wants to imply theirs is better. Major shops will also promote the STC packages, too, since they make money on that.

But the STC is not required for interior furnishings. It isn't a major alteration. The furnishings do need to meet certain requirements, like burn ratings and the like, but they don't need an STC. A mechanic can sign them off as a minor alteration.

Mike C.


I think you might want to check your facts, if you want to put M2 armrest in your 560, it’s going to require an STC.

I’m certainly no expert in regards to what you can and cannot do to an interior, but I know that seats are a safety item so you can’t just modify them. I’m not sure what’s involved in changing out tray tables and drink rails but I have never seen it done, so I’m assuming it’s more complicated than taking the old ones out and installing the ones from a 525.

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