04 Jul 2025, 00:04 [ UTC - 5; DST ]
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Post subject: Re: Cessna announces new twin turboprop - skycourier Posted: 30 Nov 2017, 21:30 |
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Joined: 01/06/08 Posts: 6405 Post Likes: +3199 Location: Pottstown, PA (KPTW)
Aircraft: 1965 Debonair C33
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Username Protected wrote: Reminds me of Short Bros. Skyvan, but with a ramp-friendly tail. I recall a photo of a VW Microbus inside a Skyvan. I have lots of skydives from a Shorts Skyvan. Great platform for that.
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Post subject: Re: Cessna announces new twin turboprop - skycourier Posted: 01 Dec 2017, 23:12 |
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Joined: 07/04/11 Posts: 1709 Post Likes: +244 Company: W. John Gadd, Esq. Location: Florida
Aircraft: C55 Baron
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Username Protected wrote: Reminds me of Short Bros. Skyvan, but with a ramp-friendly tail. I recall a photo of a VW Microbus inside a Skyvan. Ugly , but way cool.
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Post subject: Re: Cessna announces new twin turboprop - skycourier Posted: 02 Dec 2017, 15:32 |
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Joined: 08/26/15 Posts: 9937 Post Likes: +9839 Company: airlines (*CRJ,A320) Location: Florida panhandle
Aircraft: Travel Air,T-6B,etc*
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Username Protected wrote: Powering it with a twin gas turbine engine and transmission adapted from a helicopter is just nuts. I can't even imagine why anyone would go down that route, Not sure myself either, although mechanically it works fine in helicopters. You don't have the maintain control/V MC problems when one rolls back (but you can still pull off the "good" engine by mistake, and identifying the "bad" engine is not always straightforward, especially if the computers are having crosstalk problems). Quote: when there's really no reason to just hang two engines on the wings. Yeah, not sure why they put so much R&D into an unconventional two-engines-into-one concept. Obviously they thought it was a good bet. There might have been some cycle time advantage to feathering the prop while loading/offloading cargo. The prop is that much farther away from the cargo door than wing mounted engines. You can see how a truck fits easily under the wing- no struts or anything else close to the cargo door access. How many hangar rash "events" would that save over 10-20 years, and how many seconds and minutes could the company shave (safely) by not having to work extra slow when maneuvering ground vehicles up to the cargo door? Time is money... On the other hand, aviation history has just a handful of similar attempts, mostly obscure and never wild successes:    Picture credits: Wikipedia
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Post subject: Re: Cessna announces new twin turboprop - skycourier Posted: 29 Oct 2021, 15:24 |
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Joined: 09/28/15 Posts: 42 Post Likes: +28
Aircraft: Cessna 208B
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The new Skycourier sim is about ready in ICT. We should get the first aircraft by the end of the year. Be a while before they show up on the line though. Max take off weight is around 18000 lbs.
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Post subject: Re: Cessna announces new twin turboprop - skycourier Posted: 29 Oct 2021, 16:19 |
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Joined: 11/15/17 Posts: 1125 Post Likes: +582 Company: Cessna (retired)
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Any online references to the tons of problems for the Ayres Loadmaster?
The reason that this has been tried is to obtain (most) of the redundancy benefits of a twin without the VMC issue and nacelle drag of a conventional twin. Also there are, or were, advantages in Part 135 IFR operations if it qualifies as a twin.
The main disadvantage is that the FAA has imposed pretty strict special conditions (on Learfan and Soloy twin Caravan) regarding power transmission reliability. I don't know if those would qualify it as a "real" twin for Part 135.
Not really a helicopter gearbox either, when you start considering prop loads. Prop control system is also a reliability/redundancy issue.
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Post subject: Re: Cessna announces new twin turboprop - skycourier Posted: 29 Oct 2021, 16:20 |
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Joined: 11/15/17 Posts: 1125 Post Likes: +582 Company: Cessna (retired)
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Any online references to the tons of problems for the Ayres Loadmaster?
The reason that this has been tried is to obtain (most) of the redundancy benefits of a twin without the VMC issue and nacelle drag of a conventional twin. Also there are, or were, advantages in Part 135 IFR operations if it qualifies as a twin.
The main disadvantage is that the FAA has imposed pretty strict special conditions (on Learfan and Soloy twin Caravan) regarding power transmission reliability. I don't know if those would qualify it as a "real" twin for Part 135.
Not really a helicopter gearbox either, when you start considering prop loads. Prop control system is also a reliability/redundancy issue.
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