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		mrspudandcompany(at)veriz Guest
 
 
 
 
 
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				 Posted: Fri Feb 11, 2011 8:44 am    Post subject: AOA indicator | 
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				What effect does icing have on the accuracy of an AOA indicator?  Will it
 give you an accurate indication of an impending stall if you have
 accumulated ice on the wing leading edge?
 
 Roger
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Fri Feb 11, 2011 9:24 am    Post subject: AOA indicator | 
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				At 11:24 AM 2/11/2011, you wrote:
  	  | Quote: | 	 		  
 <mrspudandcompany(at)verizon.net>
 
 What effect does icing have on the accuracy of an AOA indicator?  Will it
 give you an accurate indication of an impending stall if you have
 accumulated ice on the wing leading edge?
 
 | 	  
     No . . . . Most AOA displays don't  give you
     an 'angle' display. They generally display bands
     of relative goodness/badness shaded in legacy red, yellow
     and green. The display will probably be fitted with a
     'sweet spot' . . . which represents an AOA value
     optimized by much flight testing.
 
     The problem is that the any sweet spot assumes that
     the wing is clean and stall breaks at xx.x degrees.
     Just lowering flaps can give you a new sweet spot at
     yy.y degrees. The more sophisticated AOA display
     systems will have inputs for flap position so that
     the sweet spot is automatically moved to a new value
     confirmed by careful flight testing.
 
     Once you add ice shapes on top of those super whippy,
     laminar flow, high efficiency, low drag, etc etc
     air foils, the stall break moves to zz.z degrees.
 
     Unless iced over, the AOA sensor will continue to
     give you an accurate AOA display. The problem is
     that any knowledge the AOA possesses with respect
     to airplane performance is now suspect.
 
     It's not a loss of display integrity that bites.
     It's a departure from performance conditions under which
     IAS or AOA sweet spots were deduced.
    Bob . . .
 
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		email(at)jaredyates.com Guest
 
 
 
 
 
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				 Posted: Fri Feb 11, 2011 9:27 am    Post subject: AOA indicator | 
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				Generally, no, it will not give accurate information.  A wing that used to stall at 13 degrees might stall at 10 or 8 with ice (for instance, these aren't necessarily accurate numbers).  In fact, this has been a source of at least a few crashes of transport category airplanes that stalled on takeoff without activation of the stall protection systems.  Ice accumulation combined with an aggressive rotation rate and the ground effect were sufficient to push the stall AOA below the thresholds for the stick shaker and pusher, so in some cases the crews didn't even get any indication that the airplane was stalled, other than the sudden 90 degree bank angle.  An AOA indicator might or might not indicate degrees AOA correctly, but even if it does, it's information doesn't mean anything, since you don't know what the stall AOA is of your "new" experimental airfoil shape. 
 On Fri, Feb 11, 2011 at 11:24 AM, ROGER &  JEAN CURTIS <mrspudandcompany(at)verizon.net (mrspudandcompany(at)verizon.net)> wrote:
  [quote]--> AeroElectric-List message posted by: "ROGER &  JEAN CURTIS" <mrspudandcompany(at)verizon.net (mrspudandcompany(at)verizon.net)>
   
  What effect does icing have on the accuracy of an AOA indicator?  Will it
  give you an accurate indication of an impending stall if you have
  accumulated ice on the wing leading edge?
  
  Roger
  
  
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  le, List Admin.
  ="_blank">http://www.matronics.com/contribution
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  [b]
 
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		dee.whittington(at)gmail. Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 5:55 am    Post subject: AOA indicator | 
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				Even though what Bob says about the critical angle of attack changing with the accretion of ice is, of course, correct, it would be good to have an AOA indicator which was not killed by ice.  I just remembered that our new Grand Rapids HX (and in fact all new Grand Rapids EFIS units) now have a "AOA Indexer" built in. They display angle of attack on the left side of the screen derived from, I think, AHARS data, not from unheated pin holes in the wing. 
 
  Unfortunately, the GRT web site currently does not explain, or even mention this new feature. I've just brought this to the attention of Carlos Fernandez at GRT and he promised to update the web site.
 
  Dee
 
  At 11:19 AM 2/11/2011, you wrote:
   	  | Quote: | 	 		  --> AeroElectric-List message posted by: "Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
 
  At 11:24 AM 2/11/2011, you wrote:
   	  | Quote: | 	 		  --> AeroElectric-List message posted by: "ROGER &  JEAN CURTIS" <mrspudandcompany(at)verizon.net>
 
  What effect does icing have on the accuracy of an AOA indicator?  Will it
  give you an accurate indication of an impending stall if you have
  accumulated ice on the wing leading edge? | 	  
     No . . . . Most AOA displays don't  give you
     an 'angle' display. They generally display bands
     of relative goodness/badness shaded in legacy red, yellow
     and green. The display will probably be fitted with a
     'sweet spot' . . . which represents an AOA value
     optimized by much flight testing.
 
     The problem is that the any sweet spot assumes that
     the wing is clean and stall breaks at xx.x degrees.
     Just lowering flaps can give you a new sweet spot at
     yy.y degrees. The more sophisticated AOA display
     systems will have inputs for flap position so that
     the sweet spot is automatically moved to a new value
     confirmed by careful flight testing.
 
     Once you add ice shapes on top of those super whippy,
     laminar flow, high efficiency, low drag, etc etc
     air foils, the stall break moves to zz.z degrees.
 
     Unless iced over, the AOA sensor will continue to
     give you an accurate AOA display. The problem is
     that any knowledge the AOA possesses with respect
     to airplane performance is now suspect.
 
     It's not a loss of display integrity that bites.
     It's a departure from performance conditions under which
     IAS or AOA sweet spots were deduced.
 
  
    Bob . . . 
 
  AeroElectric-List Email Forum -
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  - MATRONICS WEB FORUMS -
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   | 	   
  DeWitt (Dee) Whittington
  406 N Mulberry St
  Richmond, VA 23220-3320
  (804) 358-4333 phone and fax
  SKYPE: hilltopkid
  dee.whittington(at)gmail.com     [quote][b]
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 7:59 am    Post subject: AOA indicator | 
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				 	  | Quote: | 	 		  They display angle of attack on the left side of the screen derived 
 from, I think, AHARS data, not from unheated pin holes in the wing.
 
 Unfortunately, the GRT web site currently does not explain, or even 
 mention this new feature. I've just brought this to the attention of 
 Carlos Fernandez at GRT and he promised to update the web site.
 
 | 	  
     How does it matter where and how some AOA value is
     measured or synthesized once the wing is iced?
 
     I was once enamored of the delta-p AOA sensor
     designs. There have been a number of articles
     published on the technique. I've posted a collection
     of my archived articles at:
 
 http://www.aeroelectric.com/articles/Angle_of_Attack/
 
     There was an article in a Sport Aviation issue in
     2005 for a DIY AOA sensor/display package. Anyone
     got a copy in their library? I'd sure like to
     read a copy.
 
     The common thread that runs through these articles
     is an absence of discussion as to when the readings
     so carefully calibrated and displayed are not
     to be trusted.
 
    Bob . . .
 
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		pwmac(at)sisna.com Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 9:08 am    Post subject: AOA indicator | 
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				Interestinb, but production units are out there.
 Lets not ignore what Elbie said about the AOA in icing contitions.
 For sure he is the guru on these devices for all kinds of airplanes
 http://www.riteangle.com/
 PaulW
 =========
 
 At 06:55 AM 2/12/2011, you wrote:
  	  | Quote: | 	 		  
 <nuckolls.bob(at)aeroelectric.com>
 >They display angle of attack on the left side of the screen derived 
 >from, I think, AHARS data, not from unheated pin holes in the wing.
 >
 >Unfortunately, the GRT web site currently does not explain, or even 
 >mention this new feature. I've just brought this to the attention 
 >of Carlos Fernandez at GRT and he promised to update the web site.
 
     How does it matter where and how some AOA value is
     measured or synthesized once the wing is iced?
 
     I was once enamored of the delta-p AOA sensor
     designs. There have been a number of articles
     published on the technique. I've posted a collection
     of my archived articles at:
 
 http://www.aeroelectric.com/articles/Angle_of_Attack/
 
     There was an article in a Sport Aviation issue in
     2005 for a DIY AOA sensor/display package. Anyone
     got a copy in their library? I'd sure like to
     read a copy.
 
     The common thread that runs through these articles
     is an absence of discussion as to when the readings
     so carefully calibrated and displayed are not
     to be trusted.
 
    Bob . . .
 
 
 | 	 
 
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 10:31 am    Post subject: AOA indicator | 
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				At 11:57 AM 2/12/2011, you wrote:
  	  | Quote: | 	 		  
 
 Interestinb, but production units are out there.
 
 | 	  
     Yup, lots of them . . .
 
  	  | Quote: | 	 		  Lets not ignore what Elbie said about the AOA in icing contitions.
 For sure he is the guru on these devices for all kinds of airplanes
 
 | 	  
     But what do YOU understand and are willing to pass
     along to the less informed as to the value of
     and AOA sensor and display system? What statements
     have been made by myself or anyone else that you
     find in error? Is it your understanding that Elbie
     claims that the "sweet spot" on his or any other
     AOA display is golden under all challenges that
     a pilot might face for comfortable arrival with
     the earth?
 
    Bob . . .
 
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		retasker(at)optonline.net Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 12:42 pm    Post subject: AOA indicator | 
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				If you are an EAA member you can see ALL back issues of Sport Aviation 
 on http://www.oshkosh365.org
 
 If that doesn't do it for you I do have the 2005 issues but I would have 
 to see what issue it was in.  Do you remember what month?
 
 Dick Tasker
 
 Robert L. Nuckolls, III wrote:
  	  | Quote: | 	 		      There was an article in a Sport Aviation issue in
     2005 for a DIY AOA sensor/display package. Anyone
     got a copy in their library? I'd sure like to
     read a copy.
 
 | 	  
 -- 
 Please Note:
 No trees were destroyed in the sending of this message.  We do concede, however,
 that a significant number of electrons may have been temporarily inconvenienced.
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		pwmac(at)sisna.com Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 2:05 pm    Post subject: AOA indicator | 
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				I do noy have his message, but it went like any chance of icing 
 forget about the aoa As the readings will be bad..
 PaulW
 ==
 At 09:27 AM 2/12/2011, you wrote:
  	  | Quote: | 	 		  
 <nuckolls.bob(at)aeroelectric.com>
 
 At 11:57 AM 2/12/2011, you wrote:
 >
 >
 >Interestinb, but production units are out there.
 
     Yup, lots of them . . .
 
 >Lets not ignore what Elbie said about the AOA in icing contitions.
 >For sure he is the guru on these devices for all kinds of airplanes
 
     But what do YOU understand and are willing to pass
     along to the less informed as to the value of
     and AOA sensor and display system? What statements
     have been made by myself or anyone else that you
     find in error? Is it your understanding that Elbie
     claims that the "sweet spot" on his or any other
     AOA display is golden under all challenges that
     a pilot might face for comfortable arrival with
     the earth?
 
    Bob . . .
 
 
 | 	 
 
 
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		kuffel(at)cyberport.net Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 5:09 pm    Post subject: AOA indicator | 
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				<< How does it matter where and how some AOA value is measured or 
 synthesized once the wing is iced? >>
 
 The Dynon AOA sensor is a single heated probe with two holes which replaces 
 the standard pitot sensor.  It has temperature control so you just leave it 
 on all the time.  Thus is it relatively immune to icing.  This means I will 
 have one less distracter when I follow Bob's (and others) great advice to 
 get the heck out of wherever I am if ice is encountered.
 Tom Kuffel
 
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		retasker(at)optonline.net Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 6:05 pm    Post subject: AOA indicator | 
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				While the AOA is relatively immune to icing, and it's output is accurate 
 for your clean wings, it doesn't have any way to know the wings are iced 
 up or how to take into consideration the degradation in performance when 
 the wings have ice on them.  Therefore, if you pay attention to it's 
 readings you could end up stalling.
 
 That is what the original poster was referring to.  Even though the AOA 
 is working perfectly, it is giving you false information.
 
 Dick Tasker
 
 The Kuffels wrote:
  	  | Quote: | 	 		   
  <kuffel(at)cyberport.net>
 
  << How does it matter where and how some AOA value is measured or 
  synthesized once the wing is iced? >>
 
  The Dynon AOA sensor is a single heated probe with two holes which 
  replaces the standard pitot sensor.  It has temperature control so you 
  just leave it on all the time.  Thus is it relatively immune to 
  icing.  This means I will have one less distracter when I follow Bob's 
  (and others) great advice to get the heck out of wherever I am if ice 
  is encountered.
  Tom Kuffel
 
 
 | 	  
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 that a significant number of electrons may have been temporarily inconvenienced.
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		kuffel(at)cyberport.net Guest
 
 
 
 
 
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				 Posted: Sat Feb 12, 2011 9:13 pm    Post subject: AOA indicator | 
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				Hi Dick,
 
 <<  That is what the original poster was referring to.  Even though the AOA
 is working perfectly, it is giving you false information. >>
 
 And what I'm referring to is if I take avoidance action, as I should, the 
 instant ice is encountered I don't have to worry about my Dynon giving me 
 "false information".  It will still tell me accurately if my angle of attack 
 is well above stall with clean wings.  While I don't know what my stall 
 margin actually is at the moment I'm certainly better off than with no or 
 incorrect AOA  information.
 
 In other words, as compared to some other AOA systems the Dynon is giving me 
 true information.  My job is to apply judgement to take actions which 
 prevent the stall margin at normal cruise AOA from narrowing to zero.  And I 
 get whatever benefit/insurance, however minor, of a heated pitot.
 
 Tom Kuffel
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Sun Feb 13, 2011 7:08 am    Post subject: AOA indicator | 
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				At 08:01 PM 2/12/2011, you wrote:
  	  | Quote: | 	 		  
 <retasker(at)optonline.net>
 
 That is what the original poster was referring to.  Even though the 
 AOA is working perfectly, it is giving you false information.
 
 | 	  
     I think this is the 'nut' of what has
     yanked some folk's chains. Heated AOA
     or IAS will indeed continue to MEASURE and
     display the rudimentary stimulus that
     the sensor watches. IAS measures
     the DIFFERENCE of two pressures that
     is translated into a CALIBRATED IAS
     reading (complete with sweet-spots
      . . . or sweet-bands)
 
     AOA can be a vane that actually weather-
     cocks to align with relative wind -or-
     the system can measure pressure differentials.
     Both of those phenomenon are calculated upon
     interpreted, CALIBRATED data are displayed
     along with sweet-spots intended to be
     a guide for operation of the airplane.
 
     The concept often missed is that these
     sweet-spots are DERIVED numbers confirmed
     by repeated flight tests. In no case does
     either IAS or AOA directly measure the
     the conditions (shape) that set flying qualities
     of particular wing under  conditions that
     exist right now.
 
     So while the heated instrument is indeed
     performing as advertised in spite of icing
     elsewhere on the airplane, prior CALIBRATIONS
     for the sweet-spot are no longer valid. It's
     perfectly GOOD information. IAS is correct.
     AOA is correct. But the rules of application
     have changed in ways that are difficult to scale
     without taking off our GA pilot's hat and
     putting on the engineering test pilot's hat.
 
     Here the debate becomes purely personal.
     Do you understand what's necessary to re-
     interpret this data before you attempt a
     landing? If so, it's your choice. But if
     not so sure, then what behaviors (plan-b)
     are most likely to produce a happy outcome
     while ignoring previous calibrations of
     compromised sweet-spots.
 
     Bob . . .
 
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		Mark Sletten
 
 
  Joined: 10 Jan 2006 Posts: 43 Location: St. Jacob, IL (Near St. Louis, MO)
  | 
		
			
				 Posted: Sun Feb 13, 2011 7:44 am    Post subject: Re: AOA indicator | 
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				 	  | kuffel(at)cyberport.net wrote: | 	 		  | It will still tell me accurately if my angle of attack is well above stall with clean wings.  While I don't know what my stall margin actually is at the moment I'm certainly better off than with no or incorrect AOA  information.  | 	  
 
 That depends on how you interpret and use the data it provides. If you are flying with an iced wing, the only data even the most accurate AOA indication provides is that the wing is not stalling at the current AOA.
 
 An AOA indicator is only that; an indicator. It tells you the current angle of attack. Its only value lies in knowing a second crucial piece of data: at what AOA the wing will stall. If your wing is iced you no longer have the second crucial piece of data.
 
 Given that you have not stalled, the AOA indicator is not providing data you don't already have, that you have, in fact, not stalled. How does an accurate AOA indication help in this scenario?
 
 Mark Sletten
 
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		pwmac(at)sisna.com Guest
 
 
 
 
 
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				 Posted: Sun Feb 13, 2011 8:14 am    Post subject: AOA indicator | 
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  | 
			 
			
				Bingo
 Bob, Thanks for the summary
 PaulW
 =========
 At 07:04 AM 2/13/2011, you wrote:
  	  | Quote: | 	 		  
 <nuckolls.bob(at)aeroelectric.com>
 
 At 08:01 PM 2/12/2011, you wrote:
 >
 ><retasker(at)optonline.net>
 >
 >That is what the original poster was referring to.  Even though the 
 >AOA is working perfectly, it is giving you false information.
 
     I think this is the 'nut' of what has
     yanked some folk's chains. Heated AOA
     or IAS will indeed continue to MEASURE and
     display the rudimentary stimulus that
     the sensor watches. IAS measures
     the DIFFERENCE of two pressures that
     is translated into a CALIBRATED IAS
     reading (complete with sweet-spots
      . . . or sweet-bands)
 
     AOA can be a vane that actually weather-
     cocks to align with relative wind -or-
     the system can measure pressure differentials.
     Both of those phenomenon are calculated upon
     interpreted, CALIBRATED data are displayed
     along with sweet-spots intended to be
     a guide for operation of the airplane.
 
     The concept often missed is that these
     sweet-spots are DERIVED numbers confirmed
     by repeated flight tests. In no case does
     either IAS or AOA directly measure the
     the conditions (shape) that set flying qualities
     of particular wing under  conditions that
     exist right now.
 
     So while the heated instrument is indeed
     performing as advertised in spite of icing
     elsewhere on the airplane, prior CALIBRATIONS
     for the sweet-spot are no longer valid. It's
     perfectly GOOD information. IAS is correct.
     AOA is correct. But the rules of application
     have changed in ways that are difficult to scale
     without taking off our GA pilot's hat and
     putting on the engineering test pilot's hat.
 
     Here the debate becomes purely personal.
     Do you understand what's necessary to re-
     interpret this data before you attempt a
     landing? If so, it's your choice. But if
     not so sure, then what behaviors (plan-b)
     are most likely to produce a happy outcome
     while ignoring previous calibrations of
     compromised sweet-spots.
 
     Bob . . .
 
 
 
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		raymondj(at)frontiernet.n Guest
 
 
 
 
 
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				 Posted: Sun Feb 13, 2011 8:45 am    Post subject: AOA indicator | 
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				do not archive
 
 ***Disclaimer: I've never had an icing encounter in an airplane. The 
 following is pure speculation based on several icing encounters I have 
 had in cars.***
 I think the value that a working AOA or AI has after an icing encounter 
 is to allow you to return to a known AOA or airspeed.  The knowledge 
 that your airplane will fly at a particular AS/AOA even with the ice 
 load that has accumulated, has value if you deviate from the point while 
 distracted by other tasks. It allows you to return to a point where you 
 know the aircraft will fly.  During any change in attitude it would give 
 a known AOA/AS value that can be adhered to to assure continued flight. 
   Clearly ANY deviation from that know AOA/AS carries additional risk.
 
 I'm guessing that some of the intuitive clues that help seat of the 
 pants flying might be altered by an ice accumulation. The specific one 
 I'm thinking of is the sounds. I know this to be true in cars. I believe 
 this is another reason to take steps to avoid having to fly the aircraft 
 without an AOA/AS.
 
 Raymond Julian
 Kettle River, MN
 
 On 02/13/2011 09:44 AM, Mark Sletten wrote:
  	  | Quote: | 	 		   
  kuffel(at)cyberport.net wrote:
 > It will still tell me accurately if my angle of attack is well above stall with clean wings.  While I don't know what my stall margin actually is at the moment I'm certainly better off than with no or incorrect AOA  information.
  That depends on how you interpret and use the data it provides. If you are flying with an iced wing, the only data even the most accurate AOA indication provides is that the wing is not stalling at the current AOA.
 
  An AOA indicator is only that; an indicator. It tells you the current angle of attack. Its only value lies in knowing a second crucial piece of data: at what AOA the wing will stall. If your wing is iced you no longer have the second crucial piece of data.
 
  Given that you have not stalled, the AOA indicator is not providing data you don't already have, that you have, in fact, not stalled. How does an accurate AOA indication help in this scenario?
 
  Mark Sletten
 
 
  Read this topic online here:
 
  http://forums.matronics.com/viewtopic.php?p=330881#330881
 
 
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Tue Feb 15, 2011 4:33 pm    Post subject: AOA indicator | 
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				At 03:39 PM 2/12/2011, you wrote:
  	  | Quote: | 	 		  
 <retasker(at)optonline.net>
 
 If you are an EAA member you can see ALL back issues of Sport 
 Aviation on http://www.oshkosh365.org
 
 If that doesn't do it for you I do have the 2005 issues but I would 
 have to see what issue it was in.  Do you remember what month?
 
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    Sorry, no. It was mentioned on another forum.
    Had an EAA membership for 20+ years but gave it
    up about 10 years ago. So if anyone could find
    and capture the article, I'd sure appreciate it.
    Bob . . .
 
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		user9253
 
 
  Joined: 28 Mar 2008 Posts: 1944 Location: Riley TWP Michigan
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				 Posted: Wed Feb 16, 2011 6:44 am    Post subject: Re: AOA indicator | 
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				Bob,
 I did a search of past EAA articles and found the following pertaining to AOA:
 Better Way to Fly - May 1998
 Carrier Pilots' Secret - July 1999
 Test Pilot: Angle of Attack - April 2001
 Test Pilot: Angle of attack and lift/drag - May 2001
 Test Pilot: Angle of Attack - November 2003
 Shop Talk: Angle of Attack Indicator - December 2008
 I could not find anything in 2005 about AOA.  The December 2008 article by Dave Barker might be the one that you are looking for.  It describes how to build the AOA sensor using a hall effect transducer and LED bar graph display.
 Here is a link to the December 2008 EAA article: http://www.oshkosh365.org/saarchive/eaa_articles/2008_12_21.pdf
 Below are links to the author's website.  Dave Barker's pdf gives more detailed construction details than the EAA magazine article.
 http://www.barkeraircraft.com/files/AOA_rDisplay.pdf
 http://www.barkeraircraft.com/AOA_kit.html
 Although Dave Barker no longer sells AOA kits, he still has some circuit boards available.  There is a link to his email address on his website.
 Joe
 
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		nuckolls.bob(at)aeroelect Guest
 
 
 
 
 
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				 Posted: Wed Feb 16, 2011 9:36 am    Post subject: AOA indicator | 
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				At 09:44 AM 2/16/2011, you wrote:
  	  | Quote: | 	 		  
 
 Bob,
 I did a search of past EAA articles and found the following pertaining to AOA:
 
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    <snip>  thanks to all who responded to my query about S.A.
    articles. I now have several. It's interesting/useful to see
    what kinds of things have been published for the OBAM aviation
    community. I've added all your contributions to my library.
 
    Bob . . .
 
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		raymondj(at)frontiernet.n Guest
 
 
 
 
 
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				 Posted: Wed Feb 16, 2011 2:29 pm    Post subject: AOA indicator | 
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				Are they online somewhere?  Or am I looking in the wrong place?
 
 Raymond Julian
 Kettle River, MN
 
 On 02/16/2011 10:32 AM, Robert L. Nuckolls, III wrote:
  	  | Quote: | 	 		   
  <nuckolls.bob(at)aeroelectric.com>
 
  At 09:44 AM 2/16/2011, you wrote:
 > 
 > <fran4sew(at)banyanol.com>
 >
 > Bob,
 > I did a search of past EAA articles and found the following pertaining
 > to AOA:
 
  <snip> thanks to all who responded to my query about S.A.
  articles. I now have several. It's interesting/useful to see
  what kinds of things have been published for the OBAM aviation
  community. I've added all your contributions to my library.
 
  Bob . . .
 
 
 
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