06 May 2025, 06:34 [ UTC - 5; DST ]
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 10:10 |
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Joined: 08/07/08 Posts: 5576 Post Likes: +4213 Location: Fort Worth, TX (KFTW)
Aircraft: B200, ex 58P
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Username Protected wrote: What is the ceiling on the 200? Any of the legacy 200s equipped with RVSM? Is it worth it? I think all the G1000Nxi are RVSM, no? With the -52/-61 engines it will happily go to 350 if need be. Cabin is pretty high though, so I only do that to take advantage of raging tailwinds. My most common altitude is 280 - 300.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 10:40 |
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Joined: 08/15/11 Posts: 2574 Post Likes: +1178 Location: Mandan, ND
Aircraft: V35
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Username Protected wrote: What is the ceiling on the 200? Any of the legacy 200s equipped with RVSM? Is it worth it? Diff on a 200 is 6.1 and diff on a B200 is 6.5. The extra 0.4 psi makes a difference. -42s run out of steam at FL280, so marginally worth it to go higher. -61s or -52s make more power at altitude, so it is worth it. Probably why you don't see many 200s with anything bigger than a -42. -52s on a B200 is the real business, but -61s are really good also!
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 10:48 |
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Joined: 11/30/12 Posts: 4702 Post Likes: +5297 Location: Santa Fe, NM (KSAF)
Aircraft: B200, 500B
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Username Protected wrote: It’s not that low; he’s just high. The MMO of Mach 0.52 (Vmo 259 KIAS @ 15,000 ft) is higher than the Vmo on an M600, the MU-2, the 441, the Commander….
They’re all within a few knots of each other but the King Air is highest.
Going to leave this here Interesting. I knew the Vmo was lower, so I assumed Mmo was lower. It’s not the case.
To summarize: B200 Vmo 259 KIAS, Mmo 0.52 MU-2 Vmo 250 KIAS, Mmo 0.57
Does anyone know the physics behind one plane having a higher Vmo and the other having a higher Mmo?
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 10:58 |
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Joined: 08/24/13 Posts: 9625 Post Likes: +4470 Company: Aviation Tools / CCX Location: KSMQ New Jersey
Aircraft: TBM700C2
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Username Protected wrote: I have no idea!
You're not a "if I can't find it on the internet, it didn't happen" guy are you? No, I'm the "some guy on the internet claims something I've never heard of so I'm not believing it until there is a reference". You say a lot of things. I've learned from past experience some of them are apocryphal. Really, it is an interesting story, I would love to see the accident reports and AD. I can't find any AD that is remotely close to this, and the entire Commander SB list doesn't mention anything close to this....
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 11:01 |
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Joined: 11/30/12 Posts: 4702 Post Likes: +5297 Location: Santa Fe, NM (KSAF)
Aircraft: B200, 500B
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Username Protected wrote: What is the ceiling on the 200? Any of the legacy 200s equipped with RVSM? Is it worth it? Diff on a 200 is 6.1 and diff on a B200 is 6.5. The extra 0.4 psi makes a difference. -42s run out of steam at FL280, so marginally worth it to go higher. -61s or -52s make more power at altitude, so it is worth it. Probably why you don't see many 200s with anything bigger than a -42. -52s on a B200 is the real business, but -61s are really good also! B200s can be flown RVSM through section 9 if properly equipped, tested and managed. The ceiling is FL350.
B200s with the Raisbeck strakes and BLR winglets do just fine in the RVSM levels. The winglets give you the lift you need and the strakes give you the stability. I’m still climbing right around 1000 fpm with old -42 engines when I get to FL280 on most days. They are a slight speed penalty down low and are a fantastic improvement up high. Spending the day at 8, 9 or 10,000 feet doesn’t bother me as much as other people. I really don’t notice it.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 11:08 |
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Joined: 11/08/12 Posts: 7274 Post Likes: +4775 Location: Live in San Carlos, CA - based Hayward, CA KHWD
Aircraft: Piaggio Avanti
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Username Protected wrote: No, I'm the "some guy on the internet claims something I've never heard of so I'm not believing it until there is a reference". We should all aspire to be that guy! Quote: You say a lot of things. I've learned from past experience some of them are apocryphal. There is a long, rich history of oral story telling and information sharing in aviation. A lot of it is complete BS.
_________________ -Jon C.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 11:14 |
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Joined: 05/23/13 Posts: 7814 Post Likes: +10198 Company: Jet Acquisitions Location: Franklin, TN 615-739-9091 chip@jetacq.com
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Username Protected wrote: I have no idea!
You're not a "if I can't find it on the internet, it didn't happen" guy are you? No, I'm the "some guy on the internet claims something I've never heard of so I'm not believing it until there is a reference". You say a lot of things. I've learned from past experience some of them are apocryphal. Really, it is an interesting story, I would love to see the accident reports and AD. I can't find any AD that is remotely close to this, and the entire Commander SB list doesn't mention anything close to this....
Well, sorry... don't have any references for you.
If you don't believe me just call Dave Amis who owned Downtown Airpark - Commander Service Center (I called him yesterday to make sure I wasn't misremembering the story) or call Bruce Byerly, who will probably chime in at some point, you may know that Byerly Aviation is also a Commander Service Center and Bruce probably knows more about Turbo Commanders than anyone in the world. You could call Ron Farish, a Commander expert in his own right, that's who I worked for, buying and selling Commanders back in that time period. If that's not good enough, you can call the guys at Eagle Creek or RJ at the Service Center... shall I go on.
There's always a chance all of us Commander guys dreamed this happened, some sort of mass-delusion... Lord knows we all drank a lot back then... or you could just accept that it happened before the internet was a thing and that there was an AD to replace the cap and I have no idea why it isn't showing up.
Good job on using the word "apocryphal" I had to look it up, please give reference to what claims I have made that are false.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 11:42 |
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Joined: 11/30/12 Posts: 4702 Post Likes: +5297 Location: Santa Fe, NM (KSAF)
Aircraft: B200, 500B
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Username Protected wrote: Really didn’t understand the ATC restrictions. Storm tops were 300 or lower. Not sure how it clogs up there arrival machine. https://www.flightaware.com/live/flight ... A/tracklogFlying into or out of S Florida on a weather day requires a special skill, and I don’t have it. I always seem to get screwed and never know the magic altitude or route to request. Sounds like you did a nice job using the capabilities of a versatile plane to manage it.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 12:51 |
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Joined: 08/24/13 Posts: 9625 Post Likes: +4470 Company: Aviation Tools / CCX Location: KSMQ New Jersey
Aircraft: TBM700C2
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Username Protected wrote: Well, sorry... don't have any references for you.
If you don't believe me just call Dave Amis who owned Downtown Airpark - Commander Service Center (I called him yesterday to make sure I wasn't misremembering the story) or call Bruce Byerly, who will probably chime in at some point, you may know that Byerly Aviation is also a Commander Service Center and Bruce probably knows more about Turbo Commanders than anyone in the world. You could call Ron Farish, a Commander expert in his own right, that's who I worked for, buying and selling Commanders back in that time period. If that's not good enough, you can call the guys at Eagle Creek or RJ at the Service Center... shall I go on.
There's always a chance all of us Commander guys dreamed this happened, some sort of mass-delusion... Lord knows we all drank a lot back then... or you could just accept that it happened before the internet was a thing and that there was an AD to replace the cap and I have no idea why it isn't showing up.
Good job on using the word "apocryphal" I had to look it up, please give reference to what claims I have made that are false. I didn't start out not believing you, just wanted to see where I could find out more. But you got so defensive you started accusing me.... There is nothing wrong with being wrong. I shoot from the hip sometimes myself and often end up admitting I was wrong. I really do want to hear more about this failure mode.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 14:53 |
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Joined: 12/03/14 Posts: 19944 Post Likes: +25013 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Does anyone know the physics behind one plane having a higher Vmo and the other having a higher Mmo? Vmo can be set by a number of things that aren't basic aerodynamics like windshields, props, gear doors, etc. Mmo is set mostly by aerodynamics such as airfoil shape and control surface behaviors. Flutter margins might be the primary reason in turboprops. Nobody really knows exactly how the numbers are set outside of the design team unless they specify it which is rare. It could be as simple as the equipment they had to test the windshield only went up to 250 KIAS, so that's what they set Vmo to. Typically, the thinner the wing and the more stout the control surfaces, the higher Mmo. The MU2 has really stout wings and no ailerons, so it isn't surprising it can go to a higher Mmo. Odd fact: If the MU2 Vmo had been lowered 1 knot, to 249 KIAS, it would not need a type rating in Canada. In Canada, type ratings are required for any plane capable of 250 KIAS or higher. My Citation V numbers: Stock: (11,200 lbs ZFW) Vmo 261 KIAS below 8000 ft, 292 KIAS above 8000 ft Mmo 0.755 Mach Modified: (12,200 lbs ZFW) Vmo 261 KIAS below 8000 ft, 276 KIAS above 8000 ft Mmo 0.755 Mach I have the ZFW increase mod (allows ~3000 lbs cabin load, more than I can ever use). Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 16:58 |
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Joined: 05/23/13 Posts: 7814 Post Likes: +10198 Company: Jet Acquisitions Location: Franklin, TN 615-739-9091 chip@jetacq.com
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Username Protected wrote: I didn't start out not believing you, just wanted to see where I could find out more. But you got so defensive you started accusing me....
There is nothing wrong with being wrong. I shoot from the hip sometimes myself and often end up admitting I was wrong.
I really do want to hear more about this failure mode. I didn't accuse you at all, I just asked if you were a if you can't find it on the internet it isn't true guy... that was actually a reference to Mike, who I expected to accuse me of sharing false info. So I apologize if I was defensive, you have to admit that much of what I post gets assailed and usually with demands to back it up with internet proof! I've googled this before and I've never found anything of any substance, so that's why I expected backlash. I wasn't wrong and wasn't shooting from the hip, that's not why I was defensive, I was defensive because of the environment BT has become. I've asked Dave Amis to get involved in Beechtalk, and maybe Bruce can share as well.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 17:09 |
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Joined: 08/24/13 Posts: 9625 Post Likes: +4470 Company: Aviation Tools / CCX Location: KSMQ New Jersey
Aircraft: TBM700C2
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Username Protected wrote: I've googled this before and I've never found anything of any substance, so that's why I expected backlash. I wasn't wrong and wasn't shooting from the hip, that's not why I was defensive, I was defensive because of the environment BT has become.
I've asked Dave Amis to get involved in Beechtalk, and maybe Bruce can share as well. I'm skeptical because there does not seem to be any AD record or Service Bulletin record of this. I don't use Google for those. Next would be to search the NTSB records...
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Post subject: Re: Legacy Citation vs Turboprop Posted: 11 Dec 2023, 17:41 |
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Joined: 08/16/15 Posts: 3349 Post Likes: +4810 Location: Ogden UT
Aircraft: Piper M600
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Username Protected wrote: I didn’t realize the Vmo was that low on a King Air. Do you have to pull power to descend? Why so low? What is Va? It’s not that low; he’s just high. The MMO of Mach 0.52 (Vmo 259 KIAS @ 15,000 ft) is higher than the Vmo on an M600, the MU-2, the 441, the Commander…. They’re all within a few knots of each other but the King Air is highest.
The Vmo on the M600 is 251, and the Mmo is Mach 0.55
_________________ Chuck Ivester Piper M600 Ogden UT
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