05 Dec 2025, 03:04 [ UTC - 5; DST ]
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Post subject: Re: Cessna Conquest II project Posted: 14 Mar 2017, 14:37 |
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Joined: 06/09/09 Posts: 4438 Post Likes: +3306
Aircraft: C182P, Merlin IIIC
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Jason, do you see the temp limiters as a worthwhile safegaurd in the Merlin/Metro fleet?
These aircraft see a lot of pilots and a lot of new pilots. The engines on these airframes are setup close to max thermodynamic hp and as such you will run into temp limiting conditions.
MU2 is so far down on the potential hp of the engine that it is likely never temp limited so the benifit there is not as obvious.
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Post subject: Re: Cessna Conquest II project Posted: 14 Mar 2017, 15:32 |
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Joined: 12/03/14 Posts: 20797 Post Likes: +26310 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: The SRL system on the Merlin/Metro does not work the same as your MU-2. It only limits EGT and has no reference to torque. I don't have SRL, that is only Solitaire and Marquise. My plane had a temp torque limiter based on ITT. This has now been downgraded to just a torque limiter with the -10 conversion. I don't enable it. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Cessna Conquest II project Posted: 14 Mar 2017, 15:36 |
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Joined: 12/03/14 Posts: 20797 Post Likes: +26310 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: MU2 is so far down on the potential hp of the engine that it is likely never temp limited so the benifit there is not as obvious. We do get temp limited sometimes, but at 665 or 715 HP, we do have some margin. A Merlin will get limited a lot because you engines are not derated very much, 900 HP/side. You need that much power to get that much bulk of an airplane going. The only time I have been temp limited on takeoff is a very hot day in Denver. Even then, I got 90% torque, so not much of a factor. The Merlin would have been significantly temp limited, 67% torque, assuming equal -10 engines. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Cessna Conquest II project Posted: 14 Mar 2017, 21:18 |
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Joined: 06/09/09 Posts: 4438 Post Likes: +3306
Aircraft: C182P, Merlin IIIC
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30* C at KAPA with bleeds off I am at 74%, and load the aircraft accordingly.
Would have been nice if the Merlin was offered with -14 engines and RVSM.
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Post subject: Re: Cessna Conquest II project Posted: 14 Mar 2017, 21:41 |
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Joined: 12/03/14 Posts: 20797 Post Likes: +26310 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Would have been nice if the Merlin was offered with -14 engines Until you have to pay the fuel bill and the overhaul costs. -14 is easily twice the cost of the smaller engines. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Cessna Conquest II project Posted: 14 Mar 2017, 21:42 |
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Joined: 12/03/14 Posts: 20797 Post Likes: +26310 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: 30* C at KAPA with bleeds off I am at 74%, and load the aircraft accordingly. 30C at KAPA and I am 100%. The Merlin is relatively underpowered for its size/weight. Mike C.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Cessna Conquest II project Posted: 14 Mar 2017, 22:10 |
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Joined: 06/09/09 Posts: 4438 Post Likes: +3306
Aircraft: C182P, Merlin IIIC
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Username Protected wrote: 30* C at KAPA with bleeds off I am at 74%, and load the aircraft accordingly. 30C at KAPA and I am 100%. The Merlin is relatively underpowered for its size/weight. Mike C.
MU2 M 10520#/1330hp = 7.9 lb/hp
Merlin IIIC 13,230#/1800hp= 7.35 lb/hp
Merlin IIIC 12,500#/1800hp= 6.9 lb/hp
At the majority of my takeoff locations it looks like the MU2 would be more underpowered than my Merlin. This scenario would reverse as the takeoff field elevation and temps climb.
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Post subject: Re: Cessna Conquest II project Posted: 16 Mar 2017, 01:58 |
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Joined: 02/09/09 Posts: 6541 Post Likes: +3243 Company: RNP Aviation Services Location: Owosso, MI (KRNP)
Aircraft: 1969 Bonanza V35A
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Username Protected wrote: Jason, do you see the temp limiters as a worthwhile safegaurd in the Merlin/Metro fleet?
These aircraft see a lot of pilots and a lot of new pilots. The engines on these airframes are setup close to max thermodynamic hp and as such you will run into temp limiting conditions.
MU2 is so far down on the potential hp of the engine that it is likely never temp limited so the benifit there is not as obvious. It depends on the pilot(s). If it's only flown by one or two careful pilots, I could go either way. However, we operated them in a 135 cargo operation with many pilots and I feel that it was a benefit. I rarely seen it as it didn't bypass until 650 (fake) degrees, which I rarely ever attempted to exceed other than when demonstrating what would occur during training. Jason
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Post subject: Re: Cessna Conquest II project Posted: 16 Mar 2017, 02:00 |
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Joined: 02/09/09 Posts: 6541 Post Likes: +3243 Company: RNP Aviation Services Location: Owosso, MI (KRNP)
Aircraft: 1969 Bonanza V35A
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Username Protected wrote: 30* C at KAPA with bleeds off I am at 74%, and load the aircraft accordingly. 30C at KAPA and I am 100%. The Merlin is relatively underpowered for its size/weight. Mike C.
Does Mitsubishi publish a Takeoff Power Check Chart, or are your numbers just from experience?
Jason
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Post subject: Re: Cessna Conquest II project Posted: 16 Mar 2017, 09:43 |
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Joined: 12/03/14 Posts: 20797 Post Likes: +26310 Company: Ciholas, Inc Location: KEHR
Aircraft: C560V
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Username Protected wrote: Does Mitsubishi publish a Takeoff Power Check Chart, or are your numbers just from experience? The answer to your question is yes. Both. The AFM has a power assurance chart. But it was for the -6 engine. With -10, I obviously meet that chart with room to spare. I also have experience with KAPA and 30C days. Made 100% power. We can "cheat" and use the Marquise power assurance chart since it has a -10 engine. It says the Marquise will make 94% torque (672 HP) at KAPA on a 30C day. That is 101% of my torque (100% is 665 HP). Attachment: marquise-pac.png It should also be noted the power assurance chart is for zero airspeed. Once you get moving, the ram air effect gives you more power. This means at liftoff, even the Marquise is easily making 100% torque even if it was limited to 94% on a static runup. The ram air effect is why the normal procedure is to set power at 90% at the start of the takeoff roll. It will be at 100% by liftoff. Mike C.
Please login or Register for a free account via the link in the red bar above to download files.
_________________ Email mikec (at) ciholas.com
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Post subject: Re: Cessna Conquest II project Posted: 22 Mar 2017, 19:23 |
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Joined: 06/13/08 Posts: 18 Post Likes: +2
Aircraft: C-441 Pitts S-2b 172
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Good luck with your 441. I am looking forward to learning of the path that you take with regard to getting her all set up.
I have had my C441 25 months and think the world of her. RVSM was important to me for topping weather, more so than increasing range, and I am glad that i have the flexibility to fly high.
I think the world of Bruce Rayner and his team.
Enjoy the plane and feel free to email any questions that you think i could answer.
Best, Michael
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Post subject: Re: Cessna Conquest II project Posted: 22 Mar 2017, 20:01 |
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Joined: 01/16/12 Posts: 610 Post Likes: +279 Location: London
Aircraft: TC690A
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Username Protected wrote: Good luck with your 441. I am looking forward to learning of the path that you take with regard to getting her all set up.
I have had my C441 25 months and think the world of her. RVSM was important to me for topping weather, more so than increasing range, and I am glad that i have the flexibility to fly high.
I think the world of Bruce Rayner and his team.
Enjoy the plane and feel free to email any questions that you think i could answer.
Best, Michael Michael, Pretty sure he opted to part it out a few pages ago.
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Post subject: Re: Cessna Conquest II project Posted: 22 Mar 2017, 23:01 |
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Joined: 11/04/13 Posts: 211 Post Likes: +173 Company: USMCR Location: Ardmore, OK
Aircraft: PA-46T, B100, Tiger
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Thanks for the support but I did throw in the towel.
This thread has been all over the place in the past 50 days.
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