23 Nov 2025, 10:16 [ UTC - 5; DST ]
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Post subject: Re: Cirrus convert Posted: 10 Jun 2014, 15:01 |
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Joined: 11/29/13 Posts: 1084 Post Likes: +405 Location: KRMN
Aircraft: Baron 58P
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Username Protected wrote: You found an Archer with Full Avidyne glass and dual 430s?----I did not know they made such an animal----I thought the new Archers were G1000 equipped----hmmmm If you like the 20, that is an awesome deal---enjoy!! matt Matt It's a 2004 year Archer III. Avidyne PFD, MFD, twin 430W, STEC55X.
Had no idea---the Archer I learned in was steam and some of those did not work most of the time
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Post subject: Re: Cirrus convert Posted: 10 Jun 2014, 19:37 |
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Joined: 11/06/10 Posts: 12191 Post Likes: +3075 Company: Looking Location: Outside Boston, or some hotel somewhere
Aircraft: None
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Username Protected wrote: So Allen, you might buy one then? Only in my wildest dreams! Sundowner was right at the limits of my budget. Granted, with a newer plane, I would hope the maintenance would be more of a routine nature than what I went through with my Sundowner (engine overhaul, upgrade avionics, refresh interior, replaced aged engine parts, corrosion issues and the like). The problem for me getting a new plane of any type would be affording insurance, hangaring the plane (no way I would have it tied down outside). i don't know the cost of a normal annual on a Cirrus but I do suspect it would be higher then my "routine" $2K annual my sundowner had set me back every year. If my wallet would be fatter, I'd get back in airplane ownership in a heartbeat. After having sole ownership of a plane, partnership just not an option. That freedom of flying without scheduling, coordinating with others was priceless.
I had a 2004 SR20 G2 for just under two years (Dec 2009 through Nov 2011). I flew it 350 hours and followed a 100 inspection program since the flight school used it some (about 50 hours a year). My 100 hr inspections cost $2,000 and the annual as $2,200. The difference was explained the 100hr did not require the log/AD search which takes a few hours. Otherwise my annuals were really straight forward.
Tim
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Post subject: Re: Cirrus convert Posted: 10 Jun 2014, 20:17 |
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Joined: 08/01/11 Posts: 6917 Post Likes: +6192 Location: In between the opioid and marijuana epidemics
Aircraft: 182, A36TC
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Neither airplane is hard to land. The bonanza is less picky on airspeed. The Cirrus is a sleek airplane. The typical prop strike starts with too fast of airspeed, the flair is usually then too high. The offending pilot then levels out in a flat or slighly nose low attitude. The airplane stays in this attitude until the airspeed decreases and the the airplane hits with the nose flat or even nose first. This starts some skipping or a bounce if you hit too hard.
They are now teaching full stall landings at the Cirrus factory. Wow that is a brand new idea. The idea that you can land an airplane "flat" is fine as long as you arrest the vertical speed first. Neither airplane is hard to land.
An A36 bonanza can be flown fast down to the runway. Pull the power back and ease back on the yoke. Eckalbars book talks about how the wing rapidly gives up lift at low airspeeds. Combine the loss of lift with the amount of drag and you get an airplane which quickly works it's way through ground effect and touches down.
Someone else said the 22 burns too much gas. This is BS. IMO 12.5-13 gal/hr LOP amounts to 160 knots. That is efficient in my book.
_________________ Fly High,
Ryan Holt CFI
"Paranoia and PTSD are requirements not diseases"
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Post subject: Re: Cirrus convert Posted: 10 Jun 2014, 20:57 |
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Joined: 02/13/10 Posts: 20360 Post Likes: +25485 Location: Castle Rock, Colorado
Aircraft: Prior C310,BE33,SR22
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Username Protected wrote: Neither airplane is hard to land. ....................... ................... ...................Someone else said the 22 burns too much gas. This is BS. IMO 12.5-13 gal/hr LOP amounts to 160 knots. That is efficient in my book. My 2004 SR22 G2 easily did 168 KTAS on 12.5 gallons in the 7000-10000 foot range.
_________________ Arlen Get your motor runnin' Head out on the highway - Mars Bonfire
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Post subject: Re: Cirrus convert Posted: 10 Jun 2014, 21:27 |
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Joined: 11/10/13 Posts: 882 Post Likes: +518 Location: Kcir
Aircraft: C90
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Username Protected wrote: I've owned both SR22 and G36. I never felt one was harder to fly or land than the other. Just different and that's mostly due to sight picture. Jason, Which one did you prefer and why? Mark
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Post subject: Re: Cirrus convert Posted: 10 Jun 2014, 22:46 |
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Joined: 01/27/13 Posts: 485 Post Likes: +187
Aircraft: SR22
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Wow, just read the thread. Many items have been well covered.
Chute repack on a G2 or later Cirrus is well under $10K.
Crosswinds are fine in a Cirrus.
The only nose heavy Cirrus is a G2, TN with A/C that hasn't had the tail weight SB done.
Because of the fat prop on the turbo, a turbo Cirrus lands differently than a NA one. The composite prop on the TN acts as a speed brake. In fact the glide ratio is lower on planes with the composite prop.
No way can I scream in and slow down in my SR22 the way my friend can in his BE35.
The small wheels with tight pants on the Cirrus are no where near as grass friendly as the retractable gear on the Bo.
I would take an older SR22 over a newer SR20. The extra power is transformational. The difference in cruise is minor compared to climb rate. In the mountains or during the summer in the south (high to avoid clouds) the ability to climb is great.
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Post subject: Re: Cirrus convert Posted: 11 Jun 2014, 02:19 |
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Joined: 01/29/08 Posts: 26338 Post Likes: +13085 Location: Walterboro, SC. KRBW
Aircraft: PC12NG
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Username Protected wrote: Jason,
Which one did you prefer and why?
Mark
I kinda already said in previous posts in this thread. I prefer the 36TN. It's bigger and tougher and holds it's value much more.
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Post subject: Re: Cirrus convert Posted: 11 Jun 2014, 10:10 |
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Joined: 12/17/10 Posts: 1626 Post Likes: +276 Location: Valparaiso, IN
Aircraft: Lancair Evolution
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Username Protected wrote: Just wait until the Cirrus fleet ages... I've an A&P IA friend with an airworthy straight 35. Another set of 3 friends are in partnership in a C35 (circa 1953) that gets the heck flown out of it thanks to the newest partner finding himself in a cherry E-225 engined Bonanza with a virtually new engine and prop. Between the Garmin glass panels (when will Garmin refuse to repair them?), the Cirrus glass wings and fuselage and the certification life limitations (are there any?), I don't know if a single Cirrus will ever make it to age 70. "Glass wing"?? I'm not sure if you were being non specific but there is nothing glass about it. I'm no fan of the Cirrus, but I have little doubt that the Carbon structure planes will far outlast the aluminum counterparts. As long as you don't do something silly like flying into harsh weather and breaking the structure, they will last darn near infinitely. Aluminum fatigues over time. The carbon fiber structures do not.
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Post subject: Re: Cirrus convert Posted: 11 Jun 2014, 10:18 |
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Joined: 12/17/10 Posts: 1626 Post Likes: +276 Location: Valparaiso, IN
Aircraft: Lancair Evolution
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Username Protected wrote: You know that they are not age limited right? Wouldn't they be if age was the driving factor behind safety of flight? Either way, you are assuming a problem that doesn't yet exist and for which there is no data to support in, what, 15 years of airframe life. I'm not arguing they will last 70 or 100 years. Maybe they will, maybe they won't. But if you are concerned the airframe will last as long as you want to own it, the only number you have to worry about, right now, is 12,000 hours. Anything else is presumption/assumption/unfounded fear.
Ever seen an old fiberglass ski boat?
Fiberglass is a totally different animal than Carbon Fiber. For one, fiberglass is constructed with a polyester resin that has 0 UV protection in it. The reason why is because that is a cheap form of resin. Carbon fiber not only is much much stronger, but uses an Epoxy resin that has UV protection and is much better than a polyester resin. Besides that fact, Carbon Fiber is darn near not effected by heat at all. Anyone that tries to compare fiberglass to carbon fiber does not understand the differences between the two products.
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Post subject: Re: Cirrus convert Posted: 11 Jun 2014, 11:12 |
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Joined: 11/06/10 Posts: 12191 Post Likes: +3075 Company: Looking Location: Outside Boston, or some hotel somewhere
Aircraft: None
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Username Protected wrote: Fiberglass is a totally different animal than Carbon Fiber. For one, fiberglass is constructed with a polyester resin that has 0 UV protection in it. The reason why is because that is a cheap form of resin. Carbon fiber not only is much much stronger, but uses an Epoxy resin that has UV protection and is much better than a polyester resin. Besides that fact, Carbon Fiber is darn near not effected by heat at all. Anyone that tries to compare fiberglass to carbon fiber does not understand the differences between the two products. Gerry, You have lots of assumptions and generalizations in there. However, you can use an epoxy resin with fiberglass that is UV resistant or UV proof (this is actually starting to be more common in boating per a friend of mine). You can also use an epoxy resin with carbon fiber that is susceptible to UV. It really comes down to price and goals. Carbon Fiber is more expensive then Fiber glass, as a general rule people will use the more expensive resin with Carbon Fiber as a result. The more expensive the resin the greater the chance it will resist UV, cure better.... Assuming I recall it correctly, the G1 model was all fiber glass. The G2 model introduced the carbon fiber wing spar which reduced the BEW by 100 lbs. Tim
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Post subject: Re: Cirrus convert Posted: 11 Jun 2014, 11:28 |
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Joined: 12/17/10 Posts: 1626 Post Likes: +276 Location: Valparaiso, IN
Aircraft: Lancair Evolution
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Username Protected wrote: Fiberglass is a totally different animal than Carbon Fiber. For one, fiberglass is constructed with a polyester resin that has 0 UV protection in it. The reason why is because that is a cheap form of resin. Carbon fiber not only is much much stronger, but uses an Epoxy resin that has UV protection and is much better than a polyester resin. Besides that fact, Carbon Fiber is darn near not effected by heat at all. Anyone that tries to compare fiberglass to carbon fiber does not understand the differences between the two products. Gerry, You have lots of assumptions and generalizations in there. However, you can use an epoxy resin with fiberglass that is UV resistant or UV proof (this is actually starting to be more common in boating per a friend of mine). You can also use an epoxy resin with carbon fiber that is susceptible to UV. It really comes down to price and goals. Carbon Fiber is more expensive then Fiber glass, as a general rule people will use the more expensive resin with Carbon Fiber as a result. The more expensive the resin the greater the chance it will resist UV, cure better.... Assuming I recall it correctly, the G1 model was all fiber glass. The G2 model introduced the carbon fiber wing spar which reduced the BEW by 100 lbs. Tim
Sure, I didn't want to get too complicated with it, but explain general differences. From what I understand, the resin used for CF is UV protective. The main premise of my post was to get the point across that CF and Fiberglass are completely different products and CF is far superior of a product than anything we have today to build something like an airplane out of.
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Post subject: Re: Cirrus convert Posted: 11 Jun 2014, 11:42 |
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Joined: 11/06/10 Posts: 12191 Post Likes: +3075 Company: Looking Location: Outside Boston, or some hotel somewhere
Aircraft: None
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Username Protected wrote: Sure, I didn't want to get too complicated with it, but explain general differences. From what I understand, the resin used for CF is UV protective. The main premise of my post was to get the point across that CF and Fiberglass are completely different products and CF is far superior of a product than anything we have today to build something like an airplane out of. Ok, I agree they are different products. But if you are gonna go there you really should include the multiple variations, a few examples: - Fiber Glass
- Carbon Fiber
- Kevlar Strands
- Basalt Fiber
- Aramid Fibers
And all the possible combinations of the items above.  Tim (could not resist)
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Post subject: Re: Cirrus convert Posted: 11 Jun 2014, 11:48 |
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Joined: 07/27/10 Posts: 2155 Post Likes: +533
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Nate that really is beautiful machine, and if/when I get back to TX I hope you'll give me a demo. And for your flying it probably is the best all around machine, especially when evaluated dollar for dollar against twins or Turbo Props that would equal it's mission capabilities.
Best wishes,
Burns
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Post subject: Re: Cirrus convert Posted: 11 Jun 2014, 11:51 |
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Joined: 01/29/08 Posts: 26338 Post Likes: +13085 Location: Walterboro, SC. KRBW
Aircraft: PC12NG
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Username Protected wrote: Fiberglass is a totally different animal than Carbon Fiber. For one, fiberglass is constructed with a polyester resin that has 0 UV protection in it. The reason why is because that is a cheap form of resin. Carbon fiber not only is much much stronger, but uses an Epoxy resin that has UV protection and is much better than a polyester resin. Besides that fact, Carbon Fiber is darn near not effected by heat at all. Anyone that tries to compare fiberglass to carbon fiber does not understand the differences between the two products. What's made of "carbon fiber"? Cirrus? I don't think so. A 30 year old Bonanza is a nice machine. My 2004 Cirrus was showing serious wear and rattle when I got out of it. I disagree that fiberglass will hold up better to the elements and time than aluminum.
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