31 Jan 2026, 13:34 [ UTC - 5; DST ]
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Post subject: Re: Legacy Citation vs Turboprop Posted: 09 Nov 2023, 18:16 |
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Joined: 12/03/14 Posts: 21202 Post Likes: +26703 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Maybe I am missing something here, but a 510 and a 525 are two completely different type ratings M2 is on a CE-525 type rating. It is a CJ1 underneath with various minor changes. In fact, it is on the CJ type certificate A1WI and the aircraft all have serial numbers 525-xxxx. The M2 name is a marketing trick to replace the Mustang (CE-510 type rating) as the bottom of the product line. The Mustang costs more to build than the CJ due to uniqueness of parts and process that doesn't take advantage of the CJ product line. Maybe the insurance is confused by that and thinks the M2 is not a 525? They don't always catch those details. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Legacy Citation vs Turboprop Posted: 09 Nov 2023, 18:36 |
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Joined: 05/23/13 Posts: 8882 Post Likes: +11635 Company: Jet Acquisitions Location: Franklin, TN 615-739-9091 chip@jetacq.com
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Username Protected wrote: No big deal because it doesn't have vastly different systems integrated into the avionics and it doesn't have a $3+ Million dollar hull value. Mike C.
_________________ Be kind. You never know what someone is going through.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 09 Nov 2023, 18:42 |
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Joined: 05/23/13 Posts: 8882 Post Likes: +11635 Company: Jet Acquisitions Location: Franklin, TN 615-739-9091 chip@jetacq.com
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Username Protected wrote: This argument about insurance is meaningless without addressing how Hull and Liability limits affect the policy. Exactly. I think this is the part Mike is missing, except when it suits him to sell the value of his $900k hull value aircraft. When you go over $3M hull value the insurance companies get real testy. When you hit about $5M - $6M it gets worse and when you get over about $8M it seems to get really bad! I have been told by numerous sources that The $8M - $9M PLUS range is bad because the value is too great for a single insurer and they have to bring in a second company. As always, I just want to get good and correct info out there so that aircraft buyers, owners and operators don't get caught with their pants down. If I make a mistake or say something that is inaccurate, please call me out on it. I will quickly admit I was wrong and will be glad the record is corrected.
_________________ Be kind. You never know what someone is going through.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 09 Nov 2023, 18:56 |
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Joined: 05/23/13 Posts: 8882 Post Likes: +11635 Company: Jet Acquisitions Location: Franklin, TN 615-739-9091 chip@jetacq.com
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Username Protected wrote: Quote: FAA says a CJ4 / PC-24 / Phenom 300E is single pilot, insurance company says HOLD MY BEER! You’re going to love this quote! Another reason for ME. MIKE C., to avoid those high priced newer planes that everybody thinks will cost less to own. The owner flown buyers of those just have lots of money and won't balk at 6 figure insurance premiums. They are already into about $800K/year just in cost of money, so that's no big deal. High hull value is a major driver off the total cost of ownership. I currently carry $3M/$250K liability, $900K hull, $14,785/year. My insurance costs went down as compared to my MU2 with the C560V. I'm single pilot. Mike C. There, I fixed it for you!  And $3M in liability? You are kidding right? You said you fly employees on your aircraft... $3M?
_________________ Be kind. You never know what someone is going through.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 09 Nov 2023, 19:28 |
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Joined: 08/15/11 Posts: 2631 Post Likes: +1236 Location: Mandan, ND
Aircraft: None currently
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Thread drift in full mode…we got new insurance quote on Bonanza. They wanted to know how many hours I had in a V35. NOT P35, S35, V35A or V35B. Just V. Insurance is getting extremely picky for model to mean just that, a model. Even though that does not match FAAs description. Conversely, here is something even dumber. FAA requires under 135 higher mins until 100 hours time in type. TYPE. C90 and 200/B200 different types, so 100 hrs each. But 200/B200/300//B300/A200/1900 are all one TYPE (A24CE). So, that’s OK. 
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Post subject: Re: Legacy Citation vs Turboprop Posted: 09 Nov 2023, 20:35 |
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Joined: 08/05/16 Posts: 3151 Post Likes: +2295 Company: Tack Mobile Location: KBJC
Aircraft: C441
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Username Protected wrote: Thread drift in full mode…we got new insurance quote on Bonanza. They wanted to know how many hours I had in a V35. NOT P35, S35, V35A or V35B. Just V. Insurance is getting extremely picky for model to mean just that, a model. Even though that does not match FAAs description. Conversely, here is something even dumber. FAA requires under 135 higher mins until 100 hours time in type. TYPE. C90 and 200/B200 different types, so 100 hrs each. But 200/B200/300//B300/A200/1900 are all one TYPE (A24CE). So, that’s OK.  I've become less confused about FAA rules now that I understand they exist primarily to prevent the FAA from being blamed for anything, not for our safety.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 10 Nov 2023, 00:07 |
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Joined: 03/09/13 Posts: 938 Post Likes: +479 Location: Byron Bay,NSW Australia
Aircraft: C525,C25A,C25C,CL605
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Username Protected wrote: the M2 is basically a re-imagined CJ and is a 525. I did my initial 525 rating which gave me CJ,CJ1 and CJ2. I did differences training for M2, which didn’t include a flight test. Also did the same for CJ4, and another seperate for CJ1+, CJ2+ Andrew
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Post subject: Re: Legacy Citation vs Turboprop Posted: 10 Nov 2023, 00:34 |
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Joined: 08/16/15 Posts: 3838 Post Likes: +5705 Location: Ogden UT
Aircraft: Piper M600
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Username Protected wrote: One that can flub the best of them, is when ATC gives you crossing restriction say 20 miles from a fix in your flight plan, but there happens to be another waypoint in your flight plan between the along track offset waypoint and the crossing restriction. It can be done, but you won't get that situation often, maybe once in hundreds of hours, and I don't believe it is in the book. Uh, that's simple. Go to the referenced waypoint, hit VNAV, say 20 miles prior, enter altitude, activate. It will create a waypoint 20 miles prior to the reference waypoint even if there is a flight plan waypoint between that and the reference one. It works the same regardless of the intermediate waypoint or not. It then gives you vertical guidance so you reach the crossing altitude at the right spot. I get this a lot from ATC, like every third flight, very common for jets apparently. Not difficult with my setup (GTN 750 Xi). Quote: It can be done, but your first time you will be heads-down headscratching melting your brain with WTH???? Prob hand fly it the first time using an E6B.  Not that hard, you can always go heading and pitch pointed in roughly the right direction, then sort it out. Every pilot needs to know how to revert to basic modes while resolving complex situations. This was dealt with in the famous Children of Magenta video. [youtube]https://youtu.be/5ESJH1NLMLs[/youtube] Quote: There are a lot of these low occurrence, high workload situations that are avionics specific. I think the logic is pretty similar to my GTN on the high end G systems. Mike C.
You guys are making my point or not reading my post, or maybe me not writing well. The G3000 will not insert an along track waypoint that is before the previous waypoint in the flightplan. No matter how hard you try. Now find that out on a descent at a few hundred knots with an altitude restriction and speed assignment. Might want that E6B
_________________ Chuck Ivester Piper M600 Ogden UT
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Post subject: Re: Legacy Citation vs Turboprop Posted: 10 Nov 2023, 00:37 |
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Joined: 12/24/17 Posts: 1502 Post Likes: +1352
Aircraft: A36
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Username Protected wrote: You guys are making my point or not reading my post, or maybe me not writing well. The G3000 will not insert an along track waypoint that is before the previous waypoint in the flightplan. No matter how hard you try. Now find that out on a descent at a few hundred knots with an altitude restriction and speed assignment. Might want that E6B I agree that some of that UX logic isn't great. But why should this be a problem for any reasonably proficient pilot? I get that some of these "pro" pilots get lost if they have to actual fly the plane, but if we expect pilots to actually be able to fly - and in this case, it's as easy as managing a descent and speed without automation - this should be simple.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 10 Nov 2023, 00:53 |
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Joined: 11/30/12 Posts: 4952 Post Likes: +5635 Location: Santa Fe, NM (KSAF)
Aircraft: B200, 500B
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Username Protected wrote: You guys are making my point or not reading my post, or maybe me not writing well. The G3000 will not insert an along track waypoint that is before the previous waypoint in the flightplan. No matter how hard you try. Now find that out on a descent at a few hundred knots with an altitude restriction and speed assignment. Might want that E6B
I’m definitely confused. “…before the previous waypoint…”? As in, before the waypoint that is behind you? Why would you want to do that? Or did I misunderstand?
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Post subject: Re: Legacy Citation vs Turboprop Posted: 10 Nov 2023, 03:47 |
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Joined: 04/24/18 Posts: 736 Post Likes: +359 Location: NYC
Aircraft: ISP Eagle II SR22 g2
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Username Protected wrote: You guys are making my point or not reading my post, or maybe me not writing well. The G3000 will not insert an along track waypoint that is before the previous waypoint in the flightplan. No matter how hard you try. Now find that out on a descent at a few hundred knots with an altitude restriction and speed assignment. Might want that E6B
I’m definitely confused. “…before the previous waypoint…”? As in, before the waypoint that is behind you? Why would you want to do that? Or did I misunderstand?
Pretty sure he means after the next waypoint.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 10 Nov 2023, 04:16 |
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Joined: 05/23/13 Posts: 8882 Post Likes: +11635 Company: Jet Acquisitions Location: Franklin, TN 615-739-9091 chip@jetacq.com
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Username Protected wrote: the M2 is basically a re-imagined CJ and is a 525. I did my initial 525 rating which gave me CJ,CJ1 and CJ2. I did differences training for M2, which didn’t include a flight test. Also did the same for CJ4, and another seperate for CJ1+, CJ2+ Andrew
And that made you perfectly legal to fly all of those per the FAA.
The next step is to satisfy whatever insurance requirements an underwriter deems necessary, and those requirements vary from one situation to another.
_________________ Be kind. You never know what someone is going through.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 10 Nov 2023, 04:23 |
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Joined: 05/23/13 Posts: 8882 Post Likes: +11635 Company: Jet Acquisitions Location: Franklin, TN 615-739-9091 chip@jetacq.com
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Username Protected wrote: Should be, yet many NTSB reporte begin with pilots “pro” or not wrestling with automation and losing, bringing a perfectly good aircraft to its demise. Don’t dismiss the seriousness of having unfamiliar avionics in the cockpit. Back to my prior post. I would not want a pilot new to the G3000 no matter how many hours in c525’s piloting my M2 with me in the back. The insurance companies now agree with you and that fact is in part because of the King Air 350i accident in Addison, two pro pilots, Collins Fusion panel, ten dead bodies and a major loss for the insurance industry. I spoke with Tom Clements shortly after it happened, Tom with frustration and pain in his voice, said “I don’t understand, why didn’t they just fly the airplane?” My reply “because they were both looking at those three big tv screens in front of them, trying to figure out what the hell was going on” Prior to this accident the King Air 350 had a near perfect accident history.
_________________ Be kind. You never know what someone is going through.
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Post subject: Re: Legacy Citation vs Turboprop Posted: 10 Nov 2023, 06:50 |
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Joined: 05/05/09 Posts: 5346 Post Likes: +5405
Aircraft: C501, R66, A36
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I just processed payroll so I have same insight on this week's Phase 1-5:
We do about 12 of these a year. It's not a rocket science inspection but that's ALL my guys work on so the entire shop is geared specifically for these inspections. Standard parts are pre-ordered in bins, random spares are in a 1,500 sq foot air conditioned parts room, airframe parts planes are immediately behind the hangar and all checklists are pre-printed and ready to go. Highly efficient.
A relatively squawk free inspection with normal consumable parts takes 100 man hours. Basic parts are fuel filters, periseals, gaskets and hydraulic filters that add up to about $1,200 (unfortunately you must buy this stuff new from Textron)
So unless your airplane is incredibly jacked up OR you are buying grossly overpriced parts, you're going to have to really try to get the bill up beyond 25K.
So, if you are getting a $75K bill for a Phase 1-5, your plane is highly neglected and this is not NORMAL by any stretch. Another rationalization for this is that you are getting ripped off OR the shop/guys working on the airplane don't know what they are doing and are fumbling their way through the procedures.
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