banner
banner

05 Dec 2025, 03:04 [ UTC - 5; DST ]


Garmin International (Banner)



Reply to topic  [ 134 posts ]  Go to page Previous  1 ... 5, 6, 7, 8, 9
Username Protected Message
 Post subject: Re: Cessna Conquest II project
PostPosted: 14 Mar 2017, 14:37 
Offline


 Profile




Joined: 06/09/09
Posts: 4438
Post Likes: +3306
Aircraft: C182P, Merlin IIIC
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.


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 14 Mar 2017, 15:32 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20797
Post Likes: +26310
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
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


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 14 Mar 2017, 15:36 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20797
Post Likes: +26310
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
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


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 14 Mar 2017, 21:18 
Offline


 Profile




Joined: 06/09/09
Posts: 4438
Post Likes: +3306
Aircraft: C182P, Merlin IIIC
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.


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 14 Mar 2017, 21:41 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20797
Post Likes: +26310
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
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


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 14 Mar 2017, 21:42 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20797
Post Likes: +26310
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
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


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 14 Mar 2017, 22:10 
Offline


 Profile




Joined: 06/09/09
Posts: 4438
Post Likes: +3306
Aircraft: C182P, Merlin IIIC
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.

Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 16 Mar 2017, 01:58 
Offline




User avatar
 Profile




Joined: 02/09/09
Posts: 6541
Post Likes: +3243
Company: RNP Aviation Services
Location: Owosso, MI (KRNP)
Aircraft: 1969 Bonanza V35A
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


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 16 Mar 2017, 02:00 
Offline




User avatar
 Profile




Joined: 02/09/09
Posts: 6541
Post Likes: +3243
Company: RNP Aviation Services
Location: Owosso, MI (KRNP)
Aircraft: 1969 Bonanza V35A
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

Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 16 Mar 2017, 09:43 
Offline


 WWW  Profile




Joined: 12/03/14
Posts: 20797
Post Likes: +26310
Company: Ciholas, Inc
Location: KEHR
Aircraft: C560V
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


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 22 Mar 2017, 19:23 
Offline


 Profile




Joined: 06/13/08
Posts: 18
Post Likes: +2
Aircraft: C-441 Pitts S-2b 172
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


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 22 Mar 2017, 20:01 
Offline


User avatar
 Profile




Joined: 01/16/12
Posts: 610
Post Likes: +279
Location: London
Aircraft: TC690A
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.


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 22 Mar 2017, 23:01 
Offline


 Profile




Joined: 11/04/13
Posts: 211
Post Likes: +173
Company: USMCR
Location: Ardmore, OK
Aircraft: PA-46T, B100, Tiger
Thanks for the support but I did throw in the towel.

This thread has been all over the place in the past 50 days.


Top

 Post subject: Re: Cessna Conquest II project
PostPosted: 23 Mar 2017, 01:10 
Offline


 Profile




Joined: 06/13/08
Posts: 18
Post Likes: +2
Aircraft: C-441 Pitts S-2b 172
Sorry. Missed it.


Top

Display posts from previous:  Sort by  
Reply to topic  [ 134 posts ]  Go to page Previous  1 ... 5, 6, 7, 8, 9



Gallagher Aviation, LLC (Bottom Banner)

You cannot post new topics in this forum
You cannot reply to topics in this forum
You cannot edit your posts in this forum
You cannot delete your posts in this forum
You cannot post attachments in this forum

Jump to:  

Terms of Service | Forum FAQ | Contact Us

BeechTalk, LLC is the quintessential Beechcraft Owners & Pilots Group providing a forum for the discussion of technical, practical, and entertaining issues relating to all Beech aircraft. These include the Bonanza (both V-tail and straight-tail models), Baron, Debonair, Duke, Twin Bonanza, King Air, Sierra, Skipper, Sport, Sundowner, Musketeer, Travel Air, Starship, Queen Air, BeechJet, and Premier lines of airplanes, turboprops, and turbojets.

BeechTalk, LLC is not affiliated or endorsed by the Beechcraft Corporation, its subsidiaries, or affiliates. Beechcraft™, King Air™, and Travel Air™ are the registered trademarks of the Beechcraft Corporation.

Copyright© BeechTalk, LLC 2007-2025

.suttoncreativ85x50.jpg.
.planelogix-85x100-2015-04-15.jpg.
.sarasota.png.
.bullardaviation-85x50-2.jpg.
.Aircraft Associates.85x50.png.
.tempest.jpg.
.pdi-85x50.jpg.
.shortnnumbers-85x100.png.
.wat-85x50.jpg.
.traceaviation-85x150.png.
.8flight logo.jpeg.
.blackhawk-85x100-2019-09-25.jpg.
.camguard.jpg.
.stanmusikame-85x50.jpg.
.concorde.jpg.
.performanceaero-85x50.jpg.
.tat-85x100.png.
.boomerang-85x50-2023-12-17.png.
.rnp.85x50.png.
.dbm.jpg.
.AeroMach85x100.png.
.aviationdesigndouble.jpg.
.Wentworth_85x100.JPG.
.v2x.85x100.png.
.daytona.jpg.
.CiESVer2.jpg.
.Latitude.jpg.
.Elite-85x50.png.
.jandsaviation-85x50.jpg.
.KingAirMaint85_50.png.
.ssv-85x50-2023-12-17.jpg.
.BT Ad.png.
.aerox_85x100.png.
.jetacq-85x50.jpg.
.mcfarlane-85x50.png.
.MountainAirframe.jpg.
.temple-85x100-2015-02-23.jpg.
.KalAir_Black.jpg.
.SCA.jpg.
.saint-85x50.jpg.
.bpt-85x50-2019-07-27.jpg.
.LogAirLower85x50.png.
.kadex-85x50.jpg.
.b-kool-85x50.png.
.Wingman 85x50.png.
.holymicro-85x50.jpg.
.avnav.jpg.
.AAI.jpg.
.blackwell-85x50.png.
.Plane AC Tile.png.
.ocraviation-85x50.png.
.garmin-85x200-2021-11-22.jpg.
.sierratrax-85x50.png.
.headsetsetc_Small_85x50.jpg.
.midwest2.jpg.
.gallagher_85x50.jpg.
.geebee-85x50.jpg.
.puremedical-85x200.jpg.
.ABS-85x100.jpg.
.airmart-85x150.png.
.kingairnation-85x50.png.