A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Piloting
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?



 
 
Thread Tools Display Modes
  #21  
Old January 22nd 07, 11:24 PM posted to rec.aviation.piloting,rec.aviation.student
Robert M. Gary
external usenet poster
 
Posts: 2,767
Default Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?


BDS wrote:
"Jim Logajan" wrote

"Question: Has any spin testing been conducted in the CIRRUS airplanes?

CIRRUS Engineer: Yes, CIRRUS has done spin testing in both the SR20 and

the
SR22, and we've done a variety of spins in both models.


That's interesting. I wonder who the "test pilot(s)" were that thought that
it was "virtually unrecoverable", and why they made that comment.


I spoke with the Mooney test pilot who did spin testing in the 201. He
said it was not a fun day, and he didn't look forward to it. The manual
says that spins beyond one turn may not be recoverable (the test pilot
only had the guts to do one turn ). However, even at that it passed
the FAA's spin test requirements for normal category. Makes you wonder
what's up with the Cirrus that that wasn't even desirable.

-Robert

  #22  
Old January 23rd 07, 12:06 AM posted to rec.aviation.piloting
JGalban[_8_]
external usenet poster
 
Posts: 1
Default Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?


Robert wrote :
The manual
says that spins beyond one turn may not be recoverable (the test

pilot
only had the guts to do one turn ).


That sounds fishy. One turn is all that the FAA requires, but I
doubt the pilot was scared to do more. When spin testing a design,
aircraft are normally equipped with spin chutes that deploy from the
tail and arrest the spin. They can then be jettisoned for a normal
approach and landing. They are pretty common in GA spin testing. My
bet is that the test pilot was instructed by Mooney to do the one
required turn and call it a day.

John Galban=====N4BQ (PA28-180)


--
JGalban
Posted at www.flight.org

  #23  
Old January 23rd 07, 02:28 AM posted to rec.aviation.piloting,rec.aviation.student
Matt Barrow
external usenet poster
 
Posts: 603
Default Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?

"BDS" wrote in message
et...

I found this on the Grumman Yankee which I recalled had a nasty reputation
for spins and yet was being used as a primary trainer:

"The original American Aviation AA-1 Yankee developed a poor reputation
for
safety in its first years of production (1969-71). The aircraft was
designed
purely to fill the role of a personal transportation and touring aircraft
and not a trainer, but many of the early production models were purchased
by
flying schools. The appeal of the AA-1 to schools was obvious - compared
to
the competition, the AA-1 was faster, cost less to purchase and maintain
and, most importantly, had more student-appeal with its sliding canopy and
fighter-like looks.

Many of the early school accidents were related to spin-training. Once the
AA-1 entered a fully developed spin and exceeded three turns, it was
usually
not recoverable. The AA-1 had been spin-tested as part of its
certification,
but in 1973 the FAA issued Airworthiness Directive 73-13-07 ordering the
aircraft placarded against spins."


Analysis and comparison of aircraft spin characteristics and the records:
http://www.aopa.org/asf/asfarticles/2003/sp0302.html


  #24  
Old January 23rd 07, 03:05 AM posted to rec.aviation.piloting,rec.aviation.student
Jim Logajan
external usenet poster
 
Posts: 1,958
Default Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?

"Matt Barrow" wrote:
Analysis and comparison of aircraft spin characteristics and the
records: http://www.aopa.org/asf/asfarticles/2003/sp0302.html


An interesting article, thanks.
  #25  
Old January 23rd 07, 09:04 AM posted to rec.aviation.piloting,rec.aviation.student
Thomas Borchert
external usenet poster
 
Posts: 1,749
Default Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?

Bds,

Would this stop me from buying one - no. Would it stop me from spinning one
on purpose knowing that I might have to trash it to recover - yes.


I'm with you. Now let my find that stash of cash...

--
Thomas Borchert (EDDH)

  #26  
Old January 23rd 07, 09:04 AM posted to rec.aviation.piloting,rec.aviation.student
Thomas Borchert
external usenet poster
 
Posts: 1,749
Default Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?

George,

If the aircraft cannot be recovered from a spin who would buy such a
beast ?


If that were the case, who'd certify it?

--
Thomas Borchert (EDDH)

  #27  
Old January 23rd 07, 04:40 PM posted to rec.aviation.piloting,rec.aviation.student
john smith
external usenet poster
 
Posts: 1,446
Default Cirrus spin recovery was tested. Was: Why does airspeed changewhen I adjust the prop?



Peter Dohm wrote:
I never understood Calculus I until I took Calculus II.

I would have gained far more useful knowledge if they had allowed my

to
skip Calc II and Calc III and just take Calc I three times.


Calc was NASTY. But that @##$%^&* Matrix Algebra was WORSE.


Calc I was easier than Theory of Caclulus (graduate level course that
involved proofs of the theory of limits)
  #28  
Old January 23rd 07, 06:41 PM posted to rec.aviation.piloting,rec.aviation.student
Jim Logajan
external usenet poster
 
Posts: 1,958
Default Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?

john smith wrote:
Peter Dohm wrote:
I never understood Calculus I until I took Calculus II.
I would have gained far more useful knowledge if they had
allowed my

to
skip Calc II and Calc III and just take Calc I three times.


Calc was NASTY. But that @##$%^&* Matrix Algebra was WORSE.


Calc I was easier than Theory of Caclulus (graduate level course that
involved proofs of the theory of limits)


In my day we had to solve non-linear differential equations while walking
from home uphill to class in a snowstorm. And then solve systems of
nonlinear second order differential equations while walking uphill from
class to home in a sandstorm! Those M. C. Escher topology landscapes were
tough on our three-year-old legs.

;-)
  #29  
Old January 24th 07, 05:40 PM posted to rec.aviation.piloting,rec.aviation.student
john smith
external usenet poster
 
Posts: 1,446
Default Cirrus spin recovery was tested. Was: Why does airspeed changewhen I adjust the prop?

The only/best thing I got out of Theory of Calculus was my wife.

Jim Logajan wrote:
john smith wrote:
Peter Dohm wrote:
I never understood Calculus I until I took Calculus II.
I would have gained far more useful knowledge if they had
allowed my
to
skip Calc II and Calc III and just take Calc I three times.
Calc was NASTY. But that @##$%^&* Matrix Algebra was WORSE.

Calc I was easier than Theory of Caclulus (graduate level course that
involved proofs of the theory of limits)


In my day we had to solve non-linear differential equations while walking
from home uphill to class in a snowstorm. And then solve systems of
nonlinear second order differential equations while walking uphill from
class to home in a sandstorm! Those M. C. Escher topology landscapes were
tough on our three-year-old legs.

;-)

  #30  
Old January 25th 07, 12:59 AM posted to rec.aviation.piloting,rec.aviation.student
Matt Barrow
external usenet poster
 
Posts: 603
Default Cirrus spin recovery was tested. Was: Why does airspeed change when I adjust the prop?


"john smith" wrote in message
...
The only/best thing I got out of Theory of Calculus was my wife.


Hmmm...me too. I married the professors daughter.


 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) Rich Stowell Aerobatics 28 January 2nd 09 02:26 PM
SR22 Spin Recovery gwengler Piloting 9 September 24th 04 07:31 AM
Spin Training Captain Wubba Piloting 25 April 12th 04 02:11 PM
Cessna 150 Price Outlook Charles Talleyrand Owning 80 October 16th 03 02:18 PM
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) Rich Stowell Piloting 25 September 11th 03 01:27 PM


All times are GMT +1. The time now is 07:06 PM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.