I assume you provide counsel on not just the purchase but also the prospects of a future resale. If the marketplace is replacing the King Air with the Denali, how do you expect that to influence resale values?
Post subject: Re: A tale of two workhorses Citation V vs King Air 350
Posted: 27 May 2025, 12:32
Joined: 11/30/12 Posts: 4892 Post Likes: +5569 Location: Santa Fe, NM (KSAF)
Aircraft: B200, 500B
Username Protected wrote:
Nah, King Air 350 wins.
Current score: 1467 to 251
Total fatal accidents in King Airs since 1990.... 112
Total fatal accidents in Piaggios since 1990 ... 1
Tell me again who wins?
What do those numbers look like if you divide by the number of flight hours and account for inherently unsafe flight environments (Africa, South America, etc)?
Post subject: Re: A tale of two workhorses Citation V vs King Air 350
Posted: 27 May 2025, 12:38
Joined: 11/08/12 Posts: 7620 Post Likes: +5022 Location: Live in San Carlos, CA - based Hayward, CA KHWD
Aircraft: Piaggio Avanti
Username Protected wrote:
That subtle nuance of an engine failure versus a throttle slipping back to idle is silly. The end result is the same.
100% not the same because the throttle moving back disables the auto-feather - the auto feather mechanism is in part tied to the position of the throttle handle. Engine failure without the throttle moving activates auto-feather.
Most turboprops are not controllable on one engine without the autofeather.
Now, now Mark... don't be sneaky. We are comparing King Air 350's with V's and then you brought up the Piaggio so I compared the numbers of 350's sold since 1990. Then when you listed fatalities you included a number for ALL King Airs.
How many fatalities in just the 350?
Well I can assure you it's far more than one.
The one Mike sent happened less than 100 yards from my hangar.
And that was a tragic, shocking event. It hit close to home for many of us.
Those were the first fatalities (to my knowledge) in a US based King Air 350!
Ten people.
If you include the foreign accidents, it's a total of 44 people.
The four foreign accidents were all interesting.
Philippines - Medivac Pakistan - Military Nigeria - Military China - Cloud seeding
It seems to me that there was one more, in the Middle East, but I can't find a record of it.
If you consider the nearly 1500 airframes flying and the number of flight hours, the King Air 350 has a very good safety record.
_________________ We ONLY represent buyers!
It’s a small data point, but my passengers have preferred the King Air’s cabin over the Citation’s. It’s taller and just overall more comfortable. The tube in the Citation is small and cramped for taller passengers.
Robert
King Airs literally and figuratively have BIG ramp presence. A KA350 is a large airplane with a large cabin. It's surprisingly important to the non-flying public, most of whom still assume that all private jets are Gulfstream sized inside with a stand up cabin and a private washroom.
I would love the cabin of a King Air with the performance of a Citation but that requires more money than I currently have.
That subtle nuance of an engine failure versus a throttle slipping back to idle is silly. The end result is the same.
100% not the same because the throttle moving back disables the auto-feather - the auto feather mechanism is in part tied to the position of the throttle handle. Engine failure without the throttle moving activates auto-feather.
Most turboprops are not controllable on one engine without the autofeather.
HUGE DIFFERENCE.
You’re all hanging up on this auto feather thing. Yes I know how it works. I agree that turboprops are not controllable on one engine without auto-feather. It doesn’t matter to me if the auto feather was working or not working. They rotated and VMC’d into the ground. Those airplanes all crashed. They are dead and gone. Their estates are up for grabs.
Give me an example of a VMC roll in a Citation. This thread is Citation V versus KA 350.
The only thing this thread has indicated thus far is pointing out the serious airframe design flaw in the KA throttle. I genuinely wonder if the people choosing KA over jet aircraft because of the optics truly understand the implications and risk of that decision.
Earlier Chip mentioned the Citation V is marginally more expensive to operate than the KA350. I am still interested in seeing those numbers and a definition of “marginally.”
In my eyes, the Citation is a simpler airframe and simpler engine. Simple to me is less money to maintain.
Post subject: Re: A tale of two workhorses Citation V vs King Air 350
Posted: 27 May 2025, 13:23
Joined: 02/28/18 Posts: 89 Post Likes: +34
Aircraft: NA
Username Protected wrote:
None of them were engine failures.
This is some strange usage of the word "failure" I wasn't previously aware of.
Every single case was lack of thrust in one engine in such a critical regime of flight that the pilot(s) couldn't handle it. Some of the pilots were highly experienced, too.
Compare what happens in a V when an engine fails:
I doubt the passengers even notice. For the record, that was my first time doing a V1 cut in the actual airplane after several times in the sim. It was easy.
I hope no turboprop owner tries to make a similar video. Far too risky.
Mike C.
Hi Mike, (1) The King Air risks are real. However, the issue is specific to the King Air itself, not the engine, so I don't think you can extrapolate those risks to other turboprops. (2) I don't think there is a pilot in the world who would rather manage an engine failrue on the take off run in a turbprop instead of a jet, so you are absolutely correct. (3) ChatGPT estimates the incident rate of turbine take off run (V1-400' AGL) engine failures as 1 in 5 to 10 million take offs, so it's not a particularly high risk to focus on in the list of aircraft considerations, especially when you layer in the marginal compound risk of not managing the failure properly in a turboprop vs a jet, esp a TP with auto feather. The rate of pilot incapacitation, which you (I think correctly) poo poo, is 1 in 10 to 20 million flight hours, which would be the same rate if you assume a 2-hr average flight. And that includes incapacitation from all causes, including hypoxia.
Cheers, Ed
Last edited on 27 May 2025, 13:30, edited 2 times in total.
I assume you provide counsel on not just the purchase but also the prospects of a future resale. If the marketplace is replacing the King Air with the Denali, how do you expect that to influence resale values?
Nishant
We are already seeing extremely strong resale values in the later model King Airs because they just don't build that many.
When you look at the military and training aircraft contracts they have to fulfill it is clear that in the future fewer new King Airs will be delivered for civilian use.
I expect the production numbers for the Denali to be much higher, it is a new design that had producibility as one of it's goals. If I were to guess, I would say Textron can build 1 1/2 - 2 units on the Denali line with the effort required to build just one King Air.
When a new King Air 260 sells for more than $7M and a 360 for more than $8M... there's plenty of room for the Denali to slide nicely below the acquisition cost of either.
Earlier Chip mentioned the Citation V is marginally more expensive to operate than the KA350. I am still interested in seeing those numbers and a definition of “marginally.”
I publish my numbers on BT. So far, 2022, 2023, 2024, exactly what I spent. I'll add 2025 when known. It is strictly cash basis, what I spend.
Now you need to find a KA 350 private operator who isn't embarrassed to publish their numbers.
There will always be random variable involved. This year will be a high water mark for my maintenance, phase 1-5, but I only suffer that every 6 years. I don't know what the King Air program looks like, but suspect it is much worse.
KA 350 has almost 6 ft more wing span, has 5 tires, has 6 year gear overhaul, has props, and lastly, has a Beech defined maintenance program. Those drive up costs.
It also has a type rating, so basically the same training overhead as a Citation.
Quote:
In my eyes, the Citation is a simpler airframe and simpler engine. Simple to me is less money to maintain.
It seems so to me.
This thread came about because I saw four Blackhawk 350s each worth $5M or so and I wondered what the appeal was of that over my plane. My plane is worth maybe $1.5M as it sits, so the extra $3.5M to get a KA 350 has to be for something, right? The extra cost of money for the King Air exceeds my total operating budget.
Yes, they burn less fuel. But they burn more cash.
I assume you provide counsel on not just the purchase but also the prospects of a future resale. If the marketplace is replacing the King Air with the Denali, how do you expect that to influence resale values?
Nishant
We are already seeing extremely strong resale values in the later model King Airs because they just don't build that many.
When you look at the military and training aircraft contracts they have to fulfill it is clear that in the future fewer new King Airs will be delivered for civilian use.
I expect the production numbers for the Denali to be much higher, it is a new design that had producibility as one of it's goals. If I were to guess, I would say Textron can build 1 1/2 - 2 units on the Denali line with the effort required to build just one King Air.
When a new King Air 260 sells for more than $7M and a 360 for more than $8M... there's plenty of room for the Denali to slide nicely below the acquisition cost of either.
To your point with the Denali production (supply) and lower price point, why would anybody in the civilian resale market buy an old King Air when they could buy a new Denali for less? I struggle to see how the KA resale market stays strong.
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