08 May 2025, 15:02 [ UTC - 5; DST ]
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 24 Jun 2020, 16:25 |
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Joined: 02/22/10 Posts: 61 Post Likes: +32
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Username Protected wrote: When you say that there is "no option" but to repack the chute, what happens if you don't? Do little Cirrus faeries come out and chop the wings off your airplane? Its not like they can't void the warranty, it would be long expired at that point. I suppose that your insurance provider could cancel coverage. Basically it is required for airworthiness. It is the same as flying without a current annual. It isn't just about insurance, it is a violation of the regs.
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 24 Jun 2020, 16:25 |
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Joined: 11/30/18 Posts: 2465 Post Likes: +2158 Location: NH
Aircraft: F33A, 757/767
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Username Protected wrote: When you say that there is "no option" but to repack the chute, what happens if you don't? Do little Cirrus faeries come out and chop the wings off your airplane? Its not like they can't void the warranty, it would be long expired at that point. I suppose that your insurance provider could cancel coverage. It is a required item because it is an airworthiness limitation. Mandatory to comply, no ifs, ands, buts, even for part 91 operations.
OK, makes sense.
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 25 Jun 2020, 00:09 |
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Joined: 08/01/11 Posts: 6711 Post Likes: +5747 Location: In between the opioid and marijuana epidemics
Aircraft: 182, A36TC
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If I remember correctly BRS wanted the repack business but Cirrus told them “no way!”
A little competition would be nice. Still waiting for the parachute on my airplane.
I would really like to see a push for the chute on here once again.
_________________ Fly High,
Ryan Holt CFI
"Paranoia and PTSD are requirements not diseases"
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 25 Jun 2020, 14:40 |
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Joined: 01/22/19 Posts: 1084 Post Likes: +844 Location: KPMP
Aircraft: PA23-250
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Username Protected wrote: Does Cirrus have limitations on maintenance, or annual, work that can be done by IA's that are not Cirrus authorized service centers? No. The only things held captive to a Cirrus Authorized Service Center are the parachute reefing line cutter replacement, and a chute repack. And only because those aren't covered in an A&P's privileges under current FAA regs. So even a properly trained CASC tech cannot do those outside of the CASC if he leaves the facility.
_________________ A&P/IA/CFI/avionics tech KPMP Cirrus aircraft expert
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 26 Jun 2020, 15:53 |
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Joined: 04/02/18 Posts: 276 Post Likes: +134 Location: KALM
Aircraft: RV-4
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Username Protected wrote: This isn't a swipe, but an honest question, isn't the chute required because of unfavorable stall characteristics? IIRC it was just because Cirrus didn’t want to spend the time/money to demonstrate the recovery and used the chute as an alternate method of compliance. I read somewhere that EASA made them demonstrate stall/spin recoveries anyway and the design did fine.
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 26 Jun 2020, 15:55 |
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Joined: 12/19/11 Posts: 3307 Post Likes: +1434 Company: Bottom Line Experts Location: KTOL - Toledo, OH
Aircraft: 2004 SR22 G2
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Username Protected wrote: This isn't a swipe, but an honest question, isn't the chute required because of unfavorable stall characteristics? Not in the least bit Chip. I've flown many different types and among them all the Cirrus has some of the most benign stall characteristics. The cuffed outer wing panel is the primary feature that's responsible for such a docile stall. The outer wing panels remain fully attached in the stall and aileron control is also maintained. I've done many stalls in the SR's and have yet to be able to get a wing to drop. There's some explanation in the article below about stall and spin characteristics and certification history of both the SR's and Cessna 350/400: http://whycirrus.com/engineering/stall-spin.aspx
_________________ Don Coburn Corporate Expense Reduction Specialist 2004 SR22 G2
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 28 Jun 2020, 21:47 |
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Joined: 01/22/19 Posts: 1084 Post Likes: +844 Location: KPMP
Aircraft: PA23-250
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Username Protected wrote: This isn't a swipe, but an honest question, isn't the chute required because of unfavorable stall characteristics? The chute was required by Cirrus founder Alan Klapmeier, due to his previous experience of a mid air collision and the desire to have an option other than death.
_________________ A&P/IA/CFI/avionics tech KPMP Cirrus aircraft expert
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 28 Jun 2020, 22:57 |
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Joined: 01/23/13 Posts: 9115 Post Likes: +6876 Company: Kokotele Guitar Works Location: Albany, NY
Aircraft: C-182RG, C-172, PA28
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Username Protected wrote: Will be interesting to see what happens when some airframes hit repack #3. Suspect a number get scrapped at that point. Why would they get scrapped when they get to their third repack?
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 28 Jun 2020, 23:45 |
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Joined: 07/17/13 Posts: 2128 Post Likes: +3077 Location: Covington, LA (KHDC)
Aircraft: 1966 C55 Baron
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Username Protected wrote: Why would they get scrapped when they get to their third repack? Because they didn't get scrapped after the 2nd repack and it's gotta happen sometime, right? 3rd repack is the next best chance. Well, until the 4th repack. Or the 5th....
_________________ Flying - Because baseball, football, basketball, soccer, bowling & golf only take one ball.
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Post subject: Re: TTx vs SR22T - why didn't the TTx succeed? Posted: 29 Jun 2020, 00:46 |
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Joined: 01/30/09 Posts: 3617 Post Likes: +2267 Location: $ilicon Vall€y
Aircraft: Columbia 400
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Username Protected wrote: Will be interesting to see what happens when some airframes hit repack #3. Suspect a number get scrapped at that point. Why would they get scrapped when they get to their third repack?
Not cost effective, or components no longer available.
Then again, the airframe has a 12,500 hour life limit too.
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