Re: [Aus-soaring] Stalls,Spins

2014-12-26 Thread Mike Borgelt
The thing that causes a wing to stall (and subsequently perhaps to 
spin) is that it meets the air at greater than the stalling angle.
All subsonic thin wings, flown at speeds where compressibility is not 
an issue(below about 200 knots) stall at around 15 degrees angle of 
attack (the angle at which the wing meets the air) for large aspect 
ratios (glider wings).
The pilot controls this angle with the position of the elevator. The 
elevator is pretty rigidly connected to the control column so what 
you do with that controls whether the wing is stalled or not.

Nothing to do with speed or attitude at all.

However if you fly below a certain speed the maximum lift force 
generated by the wing is less than the force on the glider due to 
gravity and you cannot sustain level flight. This speed is the level 
flight 1 g stall speed.
At angles of attack close to the stalling angle, coarse use of the 
ailerons and/or rudder can cause one wing to exceed its stalling 
angle and it only takes one wing to stall to initiate an incipient spin.
So the lesson really is quite simple: If the glider stalls (usually 
recognisable by the pitch down or the nose slowing its progress 
around the horizon in a thermal) just STOP PULLING THE STICK BACK. 
Most gliders have heavy wings and won't actually snap roll as the 
wing has a high moment of inertia in roll. As Gel Cuming (long time 
RAAF chief test pilot) told me once about stalls and departures from 
controlled flight (a better term possibly): if the aircraft wants to 
go in the opposite direction to your control inputs, move the stick 
in the direction the aircraft wants to go. By the time you get to the 
middle things will usually be under control.
Rules of thumb about speeds are no substitute for proper 
understanding. There's really no need to ever enter a full spin accidently.


Mike





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Re: [Aus-soaring] Stalls

2011-06-08 Thread Mike Borgelt

At 01:01 PM 3/06/2011, you wrote:

Hi;

Another article which expands upon the subject:

http://www.flightglobal.com/articles/2011/02/06/352727/industry-sounds-warnings-on-airline-pilot-skills.html



Interesting that a meeting was held and nobody could remember where 
the new stall recovery technique came from. It isn't used by FAA 
certification test pilots.


Goes to show that every now and again it may pay to check your 
assumptions or operational doctrine and ask why are we doing this, this way?.


Maybe the Euros should ask EASA why they are messing with gliders 
when they can't stop innocent people being killed in airliners with 
known faulty pitot tubes that made it all the way through 
certification and then numerous operational incidents without an 
emergency AD for replacement. That's before anyone questions Airbus 
cockpit design and operation and airline pilot training, all of which 
appear to need attention.


Mike
Borgelt Instruments - manufacturers of quality soaring instruments since 1978
phone Int'l + 61 746 355784
fax   Int'l + 61 746 358796
cellphone Int'l + 61 428 355784

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Re: [Aus-soaring] Stalls

2011-06-02 Thread Peter F Bradshaw
Hi;

Another article which expands upon the subject:

http://www.flightglobal.com/articles/2011/02/06/352727/industry-sounds-warnings-on-airline-pilot-skills.html

On Mon, 30 May 2011, Mike Borgelt wrote:


 WTF

 http://www.flightglobal.com/articles/2011/05/28/357321/revised-stall-procedures-centre-on-angle-of-attack-not.html

 Mike
 Borgelt Instruments - manufacturers of quality soaring instruments since 1978
 phone Int'l + 61 746 355784
 fax   Int'l + 61 746 358796
 cellphone Int'l + 61 428 355784

 email:   mborg...@borgeltinstruments.com
 website: www.borgeltinstruments.com


Cheers

-- 
Peter F Bradshaw: http://www.exadios.com (public keys avaliable there).
Personal site: http://personal.exadios.com
I love truth, and the way the government still uses it occasionally to
 keep us guessing. - Sam Kekovich.
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Re: [Aus-soaring] Stalls

2011-05-31 Thread tom claffey
Backup is ISIS as D Conway says.
It is solid state for attitude and should last for 5 hours on battery power.
Airbus and Boeing have recently changed stall procedure to include REDUCING 
power due to possibility of pitch up from underslung engines overpowering full 
forward elevator at low speed.
Tom

- Original Message -
From: Mike Borgelt mborg...@borgeltinstruments.com
To: Discussion of issues relating to Soaring in Australia. 
aus-soaring@lists.internode.on.net
Cc: 
Sent: Monday, 30 May 2011 7:43 PM
Subject: Re: [Aus-soaring] Stalls

At 07:37 PM 30/05/2011, you wrote:



Airbus PFDs are driven by the air data computers.  The flight data
recorder indicates that all three air data computers tripped offline --
which would have removed the PFD's data feed, which would have
rendered the entirety of both pilots' PFDs inoperative.

Any Airbus drivers care to tell us if this is correct? No backup 
attitude indication at all?

Mike
Borgelt Instruments - manufacturers of quality soaring instruments since 1978
phone Int'l + 61 746 355784
fax  Int'l + 61 746 358796
cellphone Int'l + 61 428 355784

email:  mborg...@borgeltinstruments.com
website: www.borgeltinstruments.com 

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Re: [Aus-soaring] Stalls

2011-05-30 Thread anthony . smith
  
 
The artificial horizon (AH) will only tell you if you are climbing or 
descending. It works on the direction you are travelling in.  
 
Most larger aircraft will have an angle of attack device, either a 
vane or probe, mounted on either side of the nose. This can be used in 
a stall warning system.  
 
Stall angle is not as simple on high speed / high altitude aircraft 
as it is to low speed / low altitude aircraft like gliders. Unlike 
gliders where the stall angle is a constant, an airliner cruising at 
~Mach 0.8 (give or take a bit) stall angle is a complex variable. At 
those mach numbers it doesn't take too much accelleration of the air 
flow over (and under) the wing to exceed Mach 1. The presence of 
strong shock waves on the surface of the wing can greatly alter the 
lift. The typical affect is that the stall angle is greatly reduced. 
(Note that the lift that the wing produces per degree of angle of 
attack increases with Mach number up to a certain point which can 
compensate a bit.) Note also that when the airliner is low and slow, 
the stall angle returns to a relative constant as per what we are used 
to as glider pilots.  
 
Stall angle gets really complicated and modern airliners will have a 
computer to work it all out and provide warning to the crew. Most of 
the time this takes the form of a 'stick shaker' - a system which 
mechanically shakes the control column to alert the crew.  
 
it is not the first time that this has happened in recent history. I 
read in an Air Safety magazine relatively recently that an airliner 
pilot on approach into Alice Springs encountered stall warning twice. 
The first time he tried to power out of it as allegded with the Air 
France crew. the second time he remembered to lower the nose as well. 
 
 On Mon 30/05/11 12:26 PM , DMcD slutsw...@gmail.com sent: 
  I know nothing about nothing which is probably apparent from my 
 postings, but can someone tell me, do instruments like an artificial 
 horizon give these pilots any indication of nose angle or angle of 
 incidence? 
 
 I was attempting to explain a stall like this to #2 wife and had 
 difficulty understanding why they did not put the nose down or look 
at 
 an instrument to tell them their AOA since they would have had some 
 minutes to think about this during what appears to have been a tail 
 down plunge. 
 
 At least if the SOPs have changed, I can persuade her to get on 
another plane. 
 
 D 
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Re: [Aus-soaring] Stalls

2011-05-30 Thread Mark Newton

On 30/05/2011, at 12:26 PM, DMcD wrote:

 I was attempting to explain a stall like this to #2 wife and had
 difficulty understanding why they did not put the nose down or look at
 an instrument to tell them their AOA since they would have had some
 minutes to think about this during what appears to have been a tail
 down plunge.

They were at high altitude and flying heavy.

Thus Vs and Vmo would have been rather close together.

It isn't entirely unusual for an airliner at altitude to only have
a 10 - 15 KIAS range between maximum speed and stall speed.

Indications from the flight data recorder released so far are
that something happened which made all of the flight computers
trip offline at the same time (possibly all three pitot/static probes
icing over at the same time - speculation)

In very short order, that'd have disengaged the autopilot, placed
the aircraft into alternate law (where overspeed and stalling protections
are disabled), and killed almost all of the instruments.  The screens
would have been full of cautions and warnings from the tripped systems,
and audible alarms would have been blaring through the cockpit.

At high altitude, when Vs and Vmo are close together, and the 
autopilot/autothrottles are offline, virtually any disturbance in the
outside air or applied to the sidestick would have either made the
aircraft stall or overspeed.

The aircraft was in a thunderstorm, so there's your disturbance in the
outside air.

No vertical speed indication, no altimeter, no horizon reference
at night in a thunderstorm, no ASI.  So probably no way of recovering
from the stall.

  - mark


I tried an internal modem,new...@atdot.dotat.org
 but it hurt when I walked.  Mark Newton
- Voice: +61-4-1620-2223 - Fax: +61-8-82231777 -



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Re: [Aus-soaring] Stalls

2011-05-30 Thread Mark Newton

On 30/05/2011, at 5:07 PM, anthony.sm...@adelaide.on.net wrote:

 Stall angle gets really complicated and modern airliners will have a computer 
 to work it all out and provide warning to the crew.  Most of the time this 
 takes the form of a 'stick shaker' - a system which mechanically shakes the 
 control column to alert the crew.
 
 

Airbus aircraft don't have stickshakers, because Normal Law is supposed to
make stalls impossible (the aircraft will override the pilot by adjusting power,
pitch and height as the stall approaches)

There's an audible alarm instead (sounds like a chirping of crickets).

 it is not the first time that this has happened in recent history.  I read in 
 an Air Safety magazine relatively recently that an airliner pilot on approach 
 into Alice Springs encountered stall warning twice. 
 

That's one of the catalysts for Sen. Xenophon's current Senate inquiry into 
air safety.

Another was sparked by a different crew in a Q400 approaching Mascot last
year, which experienced a stick shaker warning and initiated a go-around,
then had another stick-shaker warning on the second landing attempt and
continued the approach regardless.

(and the bodgied-up go-around procedures. and the microburst takeoff. and
the near-miss north of Tullamarine... :)


  - mark



I tried an internal modem,new...@atdot.dotat.org
 but it hurt when I walked.  Mark Newton
- Voice: +61-4-1620-2223 - Fax: +61-8-82231777 -



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Re: [Aus-soaring] Stalls

2011-05-30 Thread David Conway
As Mark says stall angle is complicated but they manage to present a lot of
it on the primary flight display alongside the airspeed strip:

 

cid:image001.gif@01CC1EFA.198ADD10

 

 

From: aus-soaring-boun...@lists.internode.on.net
[mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Mark Newton
Sent: Monday, 30 May 2011 6:32 PM
To: anthony.sm...@adelaide.on.net; Discussion of issues relating to Soaring
in Australia.
Cc: DMcD
Subject: Re: [Aus-soaring] Stalls

 

 

On 30/05/2011, at 5:07 PM, anthony.sm...@adelaide.on.net wrote:





Stall angle gets really complicated and modern airliners will have a
computer to work it all out and provide warning to the crew.  Most of the
time this takes the form of a 'stick shaker' - a system which mechanically
shakes the control column to alert the crew.

 

 

Airbus aircraft don't have stickshakers, because Normal Law is supposed to

make stalls impossible (the aircraft will override the pilot by adjusting
power,

pitch and height as the stall approaches)

 

There's an audible alarm instead (sounds like a chirping of crickets).

 

it is not the first time that this has happened in recent history.  I read
in an Air Safety magazine relatively recently that an airliner pilot on
approach into Alice Springs encountered stall warning twice. 

 

That's one of the catalysts for Sen. Xenophon's current Senate inquiry into 

air safety.

 

Another was sparked by a different crew in a Q400 approaching Mascot last

year, which experienced a stick shaker warning and initiated a go-around,

then had another stick-shaker warning on the second landing attempt and

continued the approach regardless.

 

(and the bodgied-up go-around procedures. and the microburst takeoff. and

the near-miss north of Tullamarine... :)

 

 

  - mark

 




I tried an internal modem,new...@atdot.dotat.org

 but it hurt when I walked.  Mark Newton

- Voice: +61-4-1620-2223 - Fax: +61-8-82231777 -

 

 

 

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Re: [Aus-soaring] Stalls

2011-05-30 Thread Mike Borgelt

At 12:56 PM 30/05/2011, you wrote:

I know nothing about nothing which is probably apparent from my
postings, but can someone tell me, do instruments like an artificial
horizon give these pilots any indication of nose angle or angle of
incidence?

I was attempting to explain a stall like this to #2 wife and had
difficulty understanding why they did not put the nose down or look at
an instrument to tell them their AOA since they would have had some
minutes to think about this during what appears to have been a tail
down plunge.

At least if the SOPs have changed, I can persuade her to get on another plane.

D
___


Angle of incidence is an engineering term to denote the angle  which 
the wing chord line (or tailplane chord line) meets the fuselage datum.


The attitude indicator shows where the nose is pointed. In Head Up 
Displays this known as the waterline. It can be a W shape with wings 
each side.


The velocity vector is the direction in which the aircraft is moving. 
On a HUD this is usually a little diamond shape. The velocity vector 
can also show sideslip.


The angle of attack is the angle of the wing chord line to the relative wind.

I don't know what the Airbus philosophy on the main attitude display 
is. Maybe Adam can enlighten us. I suspect AoA may be a number 
somewhere on the display. I hope at least that.


I think I can see one scenario for the AF447 case. At 35degrees AoA 
the descent angle would be very steep and  the attitude may even have 
been shown to be slightly nose down relative to the horizon. The crew 
may have been trying to pull the nose up but to no avail.


Mike


.
Borgelt Instruments - manufacturers of quality soaring instruments since 1978
phone Int'l + 61 746 355784
fax   Int'l + 61 746 358796
cellphone Int'l + 61 428 355784

email:   mborg...@borgeltinstruments.com
website: www.borgeltinstruments.com 


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Re: [Aus-soaring] Stalls

2011-05-30 Thread Mark Newton

On 30/05/2011, at 6:51 PM, David Conway wrote:

 As Mark says stall angle is complicated but they manage to present a lot of 
 it on the primary flight display alongside the airspeed strip:

Yep, although on AF-744 the PFD would have been inoperative.

(one of the alerts very early in the piece was an underspeed warning
showing 65 kts)

Airbus PFDs are driven by the air data computers.  The flight data
recorder indicates that all three air data computers tripped offline --
which would have removed the PFD's data feed, which would have
rendered the entirety of both pilots' PFDs inoperative.

They were flying blind, at Mach 0.8 at night in a thunderstorm with
no instruments.  The only real mystery is why it took five entire
minutes for them to hit the water.

  - mark


I tried an internal modem,new...@atdot.dotat.org
 but it hurt when I walked.  Mark Newton
- Voice: +61-4-1620-2223 - Fax: +61-8-82231777 -



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Re: [Aus-soaring] Stalls

2011-05-30 Thread Mike Borgelt

At 07:37 PM 30/05/2011, you wrote:




Airbus PFDs are driven by the air data computers.  The flight data
recorder indicates that all three air data computers tripped offline --
which would have removed the PFD's data feed, which would have
rendered the entirety of both pilots' PFDs inoperative.


Any Airbus drivers care to tell us if this is correct? No backup 
attitude indication at all?


Mike
Borgelt Instruments - manufacturers of quality soaring instruments since 1978
phone Int'l + 61 746 355784
fax   Int'l + 61 746 358796
cellphone Int'l + 61 428 355784

email:   mborg...@borgeltinstruments.com
website: www.borgeltinstruments.com 


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Re: [Aus-soaring] Stalls

2011-05-30 Thread David Conway
There is a backup system and separate display to the PFD's (ISIS)

 

 

 

 

cid:image001.gif@01CC1EF9.2FFEA7D0

 

 -Original Message-

 From: aus-soaring-boun...@lists.internode.on.net [mailto:aus-soaring-

 boun...@lists.internode.on.net] On Behalf Of Mike Borgelt

 Sent: Monday, 30 May 2011 7:13 PM

 To: Discussion of issues relating to Soaring in Australia.

 Subject: Re: [Aus-soaring] Stalls

 

 At 07:37 PM 30/05/2011, you wrote:

 

 

 

 Airbus PFDs are driven by the air data computers.  The flight data

 recorder indicates that all three air data computers tripped offline -

 -

 which would have removed the PFD's data feed, which would have

 rendered the entirety of both pilots' PFDs inoperative.

 

 Any Airbus drivers care to tell us if this is correct? No backup

 attitude indication at all?

 

 Mike

 Borgelt Instruments - manufacturers of quality soaring instruments

 since 1978

 phone Int'l + 61 746 355784

 fax   Int'l + 61 746 358796

 cellphone Int'l + 61 428 355784

 

 email:   mborg...@borgeltinstruments.com

 website: www.borgeltinstruments.com

 

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Re: [Aus-soaring] Stalls

2011-05-30 Thread JR
So when they are talking about recovering from stalls, they dont mean the
cheap seats, its something those big things with the whatcha callits out the
sides do.
JR

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Re: [Aus-soaring] Stalls

2011-05-30 Thread Peter F Bradshaw
Hi;

Here is the release from BEA which may answer some questions (and raise
others):

http://www.bea.aero/fr/enquetes/vol.af.447/point.enquete.af447.27mai2011.en.pdf

On Mon, 30 May 2011, Mike Borgelt wrote:

 At 12:56 PM 30/05/2011, you wrote:
 I know nothing about nothing which is probably apparent from my
 postings, but can someone tell me, do instruments like an artificial
 horizon give these pilots any indication of nose angle or angle of
 incidence?
 
 I was attempting to explain a stall like this to #2 wife and had
 difficulty understanding why they did not put the nose down or look at
 an instrument to tell them their AOA since they would have had some
 minutes to think about this during what appears to have been a tail
 down plunge.
 
 At least if the SOPs have changed, I can persuade her to get on another 
 plane.
 
 D
 ___

 Angle of incidence is an engineering term to denote the angle  which
 the wing chord line (or tailplane chord line) meets the fuselage datum.

 The attitude indicator shows where the nose is pointed. In Head Up
 Displays this known as the waterline. It can be a W shape with wings
 each side.

 The velocity vector is the direction in which the aircraft is moving.
 On a HUD this is usually a little diamond shape. The velocity vector
 can also show sideslip.

 The angle of attack is the angle of the wing chord line to the relative wind.

 I don't know what the Airbus philosophy on the main attitude display
 is. Maybe Adam can enlighten us. I suspect AoA may be a number
 somewhere on the display. I hope at least that.

 I think I can see one scenario for the AF447 case. At 35degrees AoA
 the descent angle would be very steep and  the attitude may even have
 been shown to be slightly nose down relative to the horizon. The crew
 may have been trying to pull the nose up but to no avail.

 Mike


Cheers

-- 
Peter F Bradshaw: http://www.exadios.com (public keys avaliable there).
Personal site: http://personal.exadios.com
I love truth, and the way the government still uses it occasionally to
 keep us guessing. - Sam Kekovich.
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Re: [Aus-soaring] Stalls

2011-05-30 Thread Peter F Bradshaw
Hi;

On Mon, 30 May 2011, Mark Newton wrote:


 On 30/05/2011, at 12:26 PM, DMcD wrote:

  I was attempting to explain a stall like this to #2 wife and had
  difficulty understanding why they did not put the nose down or look at
  an instrument to tell them their AOA since they would have had some
  minutes to think about this during what appears to have been a tail
  down plunge.

 They were at high altitude and flying heavy.

 Thus Vs and Vmo would have been rather close together.

 It isn't entirely unusual for an airliner at altitude to only have
 a 10 - 15 KIAS range between maximum speed and stall speed.

 Indications from the flight data recorder released so far are
 that something happened which made all of the flight computers
 trip offline at the same time (possibly all three pitot/static probes
 icing over at the same time - speculation)

 In very short order, that'd have disengaged the autopilot, placed
 the aircraft into alternate law (where overspeed and stalling protections
 are disabled), and killed almost all of the instruments.  The screens
 would have been full of cautions and warnings from the tripped systems,
 and audible alarms would have been blaring through the cockpit.

 At high altitude, when Vs and Vmo are close together, and the
 autopilot/autothrottles are offline, virtually any disturbance in the
 outside air or applied to the sidestick would have either made the
 aircraft stall or overspeed.

 The aircraft was in a thunderstorm, so there's your disturbance in the
 outside air.

 No vertical speed indication, no altimeter, no horizon reference
 at night in a thunderstorm, no ASI.  So probably no way of recovering
 from the stall.

   - mark

I don't understand why they would not have had artificial horizon or
vertical speed indicator. They certainly had an altimeter becase they
called 10,000' as it went by.

Cheers

-- 
Peter F Bradshaw: http://www.exadios.com (public keys avaliable there).
Personal site: http://personal.exadios.com
I love truth, and the way the government still uses it occasionally to
 keep us guessing. - Sam Kekovich.
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Re: [Aus-soaring] Stalls - specifically AF 447

2011-05-30 Thread Terry Neumann
Quite a lot of further information (mixed in with varying amounts of 
falsehood) on this specific accident can be found here:


http://www.pprune.org/tech-log/452836-af447-thread-no-3-a.html

Filter as required - after a while you will work out which contributors 
know what they are talking about.


CAUTION:   You can while away quite a bit if time on this one, and your 
confidence in some aspects of some airline operations may suffer.


Terry

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Re: [Aus-soaring] Stalls

2011-05-30 Thread Mike Borgelt

At 07:55 PM 30/05/2011, you wrote:

Content-Type: multipart/related;
boundary==_NextPart_000_0096_01CC1EFF.5B554370
Content-Language: en-au

There is a backup system and separate display to the PFD's (ISIS)



So hopefully when the computers went off line the back up display 
worked from the gyros and accelerometers? With the quality of the 
gyros and accelerometers they would be using the attitude display at 
least ought to work usefully for some minutes at least, without air 
data inputs.


Mike






cid:image001.gif@01CC1EF9.2FFEA7D0


inline: 2d1dba7.gif
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phone Int'l + 61 746 355784
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Re: [Aus-soaring] Stalls

2011-05-30 Thread Mark Newton

On 30/05/2011, at 8:18 PM, Mike Borgelt wrote:

 So hopefully when the computers went off line the back up display worked from 
 the gyros and accelerometers? With the quality of the gyros and 
 accelerometers they would be using the attitude display at least ought to 
 work usefully for some minutes at least, without air data inputs.



The ISIS is another electronic system, not a gyro-based steam-gauge
system.

It takes data from the third set of pitot/static probes.

If they're iced over, then the ISIS doesn't work.

  - mark



I tried an internal modem,new...@atdot.dotat.org
 but it hurt when I walked.  Mark Newton
- Voice: +61-4-1620-2223 - Fax: +61-8-82231777 -



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Re: [Aus-soaring] Stalls

2011-05-30 Thread Mike Borgelt

At 08:58 PM 30/05/2011, you wrote:


On 30/05/2011, at 8:18 PM, Mike Borgelt wrote:

So hopefully when the computers went off line the back up display 
worked from the gyros and accelerometers? With the quality of the 
gyros and accelerometers they would be using the attitude display 
at least ought to work usefully for some minutes at least, without 
air data inputs.



The ISIS is another electronic system, not a gyro-based steam-gauge
system.

It takes data from the third set of pitot/static probes.

If they're iced over, then the ISIS doesn't work.



Go back and look at David's diagram. See the box marked ISIS? See the 
little legends in it that say accelerometers, gyrometers?


The gyros are probably solid state laser ring or fiber optic rate 
gyros, not mechanical ones. They may even be MEMS gyros but given the 
age of the design I doubt it. MEMS gyros are in things like the Dynon 
instruments etc found in Experimental homebuilts.



Mike
Borgelt Instruments - manufacturers of quality soaring instruments since 1978
phone Int'l + 61 746 355784
fax   Int'l + 61 746 358796
cellphone Int'l + 61 428 355784

email:   mborg...@borgeltinstruments.com
website: www.borgeltinstruments.com 


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Re: [Aus-soaring] Stalls

2011-05-29 Thread Mike Borgelt


WTF

http://www.flightglobal.com/articles/2011/05/28/357321/revised-stall-procedures-centre-on-angle-of-attack-not.html

Mike
Borgelt Instruments - manufacturers of quality soaring instruments since 1978
phone Int'l + 61 746 355784
fax   Int'l + 61 746 358796
cellphone Int'l + 61 428 355784

email:   mborg...@borgeltinstruments.com
website: www.borgeltinstruments.com 


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Re: [Aus-soaring] Stalls

2011-05-29 Thread Mike Timbrell
Scary, isn't it?


-Original Message-
From: aus-soaring-boun...@lists.internode.on.net
[mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Mike
Borgelt
Sent: Monday, 30 May 2011 11:27 AM
To: Discussion of issues relating to Soaring in Australia.
Subject: Re: [Aus-soaring] Stalls


WTF

http://www.flightglobal.com/articles/2011/05/28/357321/revised-stall-procedu
res-centre-on-angle-of-attack-not.html

Mike
Borgelt Instruments - manufacturers of quality soaring instruments since
1978 phone Int'l + 61 746 355784
fax   Int'l + 61 746 358796
cellphone Int'l + 61 428 355784

email:   mborg...@borgeltinstruments.com
website: www.borgeltinstruments.com 

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Re: [Aus-soaring] Stalls

2011-05-29 Thread Terry Neumann

On 30/05/2011 10:57 AM, Mike Borgelt wrote:


WTF

http://www.flightglobal.com/articles/2011/05/28/357321/revised-stall-procedures-centre-on-angle-of-attack-not.html 



Exactly.   I've been reading the PPRuNe threads on this sad business 
since day one.  (OK I know some people will claim that PPRuNe is full of 
BS etc, but I see it as any other group of pages on the internet - of 
which much the same can and must be said - this group excepted of course).


Only in the last few days has this astonishing SOP been revealed.   
There are reasons behind it of course, and they are interesting and 
partly logical, but the basic concept remains completely foreign to what 
most of us would expect, and on this occasion it failed everyone on 
board with tragic results.


This policy and others will be dissected extensively in extensive 
meeting rooms and courts of law over the next few years.  It's not over yet.


Terry
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Re: [Aus-soaring] Stalls

2011-05-29 Thread DMcD
I know nothing about nothing which is probably apparent from my
postings, but can someone tell me, do instruments like an artificial
horizon give these pilots any indication of nose angle or angle of
incidence?

I was attempting to explain a stall like this to #2 wife and had
difficulty understanding why they did not put the nose down or look at
an instrument to tell them their AOA since they would have had some
minutes to think about this during what appears to have been a tail
down plunge.

At least if the SOPs have changed, I can persuade her to get on another plane.

D
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Re: [Aus-soaring] Stalls

2011-05-29 Thread Ruth Patching
Oh god ! one of those is enough. those who go back for more need a jolly good 
talking to.
 Patch 
- Original Message -
From: Christopher Mc Donnell wommamuku...@bigpond.com
To: Discussion of issues relating to Soaring in Australia. 
aus-soaring@lists.internode.on.net
Sent: Monday, 30 May, 2011 1:54:59 PM GMT +10:00 Canberra / Melbourne / Sydney
Subject: Re: [Aus-soaring] Stalls

I was attempting to explain ... this to #2 wife.

No! no! D bin D. You get the senior #1 wife to explain things to the junior 
wives. :-)

C bin D


- Original Message - 
From: DMcD slutsw...@gmail.com
To: Discussion of issues relating to Soaring in Australia. 
aus-soaring@lists.internode.on.net
Sent: Monday, May 30, 2011 12:26 PM
Subject: Re: [Aus-soaring] Stalls


I know nothing about nothing which is probably apparent from my
 postings, but can someone tell me, do instruments like an artificial
 horizon give these pilots any indication of nose angle or angle of
 incidence?

 I was attempting to explain a stall like this to #2 wife and had
 difficulty understanding why they did not put the nose down or look at
 an instrument to tell them their AOA since they would have had some
 minutes to think about this during what appears to have been a tail
 down plunge.

 At least if the SOPs have changed, I can persuade her to get on another 
 plane.

 D
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