X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 10 Oct 2007 09:02:17 -0400 Message-ID: X-Original-Return-Path: Received: from smtp134.iad.emailsrvr.com ([207.97.245.134] verified) by logan.com (CommuniGate Pro SMTP 5.1.12) with ESMTP id 2379122 for lml@lancaironline.net; Wed, 10 Oct 2007 08:38:04 -0400 Received-SPF: none receiver=logan.com; client-ip=207.97.245.134; envelope-from=marknlisa@hometel.com Received: from relay3.r3.iad.emailsrvr.com (localhost [127.0.0.1]) by relay3.r3.iad.emailsrvr.com (SMTP Server) with ESMTP id 9B15744C1DD for ; Wed, 10 Oct 2007 08:37:25 -0400 (EDT) Received: from hometel.com (webmail9.r5.iad.mlsrvr.com [192.168.1.102]) by relay3.r3.iad.emailsrvr.com (SMTP Server) with ESMTP id 9658744C03A for ; Wed, 10 Oct 2007 08:37:25 -0400 (EDT) Received: by webmail.hometel.com (Authenticated sender: marknlisa@hometel.com, from: marknlisa@hometel.com) with HTTP; Wed, 10 Oct 2007 07:37:25 -0500 (CDT) X-Original-Date: Wed, 10 Oct 2007 07:37:25 -0500 (CDT) Subject: TruTrak ADI From: marknlisa@hometel.com X-Original-To: "Lancair Mailing List" Reply-To: marknlisa@hometel.com MIME-Version: 1.0 Content-Type: multipart/alternative;boundary="----=_20071010073725_26146" Importance: Normal X-Priority: 3 (Normal) X-Type: 2 X-Original-Message-ID: <37335.192.168.1.70.1192019845.webmail@192.168.1.70> X-Mailer: webmail6.5 ------=_20071010073725_26146 Content-Type: text/plain; charset="UTF-8" Content-Transfer-Encoding: quoted-printable =0AI think you are guys all making a mountain out of a molehill...=0A=0A"Mi= sinterpretation" is possible with ANY kind of instrument, even the tried an= d true gyroscopic attitude indicator. That's why we are all taught NOT to r= ely on any one instrument in IMC to understand what the aircraft is doing.= =0A=0AAssume you are flying straight and level and wish to climb. You set a= n appropriate nose-up attitude on your attitude indicator, but forget to ma= ke a power adjustment. As the speed bleeds off you continue to hold the nos= e up, but the aircraft stops climbing. Now you have a nose-high attitude wh= ich should result in a climb (that's what you expect anyway), but the altim= eter and VSI don't corroborate, and may, in fact, even be showing a descent= Would you pull back farther -- and possibly cause a stall -- or simply lo= ok at the airspeed indicator and engine instruments and realize you are fly= ing too slow with too little power to climb?=0A=0AThe way I learned instrum= ents the attitude indicator was NEVER the primary control instrument for pi= tch -- it was airspeed.=0A=0AI submit knowing the actual attitude (pitch, y= aw, roll) of the aircraft isn't as important as understanding the SITUATION= (attitude, airspeed, VSI, weather, etc.).=0A=0ALetting a situation go far = enough that you don't know exactly what the aircraft is doing might ALWAYS = result in disorientation and ham-handed, knee-jerk reactions. In the exampl= e cited by others to condemn the TruTrak ADI -- nose high in a descent with= the ADI indicating nose low -- a good scan would instantly orient the pilo= t.=0A=0AAdditionally, TruTrak has already considered the above situation an= d accounted for it. Should the pilot allow the aircraft to slow enough such= that pitch indications might not match the actual attitude of the aircraft= , the TruTrak ADI will has a programmable warning indicator that tells the = pilot to check the airspeed.=0A=0AFor myself, I find the TruTrak ADI a fine= alternative to more expensive mechanical gyroscopic instruments.=0A=0AMark= Sletten ------=_20071010073725_26146 Content-Type: text/html; charset="UTF-8" Content-Transfer-Encoding: quoted-printable

I think you are guys all making a mounta= in out of a molehill...

"Misinterpretation" is possible with AN= Y kind of instrument, even the tried and true gyroscopic attitude indicator= That's why we are all taught NOT to rely on any one instrument in IMC to = understand what the aircraft is doing.

Assume you are flying straigh= t and level and wish to climb. You set an appropriate nose-up attitude on y= our attitude indicator, but forget to make a power adjustment. As the speed= bleeds off you continue to hold the nose up, but the aircraft stops climbi= ng. Now you have a nose-high attitude which should result in a climb (that'= s what you expect anyway), but the altimeter and VSI don't corroborate, and= may, in fact, even be showing a descent. Would you pull back farther -- an= d possibly cause a stall -- or simply look at the airspeed indicator and en= gine instruments and realize you are flying too slow with too little power = to climb?

The way I learned instruments the attitude indicator was N= EVER the primary control instrument for pitch -- it was airspeed.

I = submit knowing the actual attitude (pitch, yaw, roll) of the aircraft isn't= as important as understanding the SITUATION (attitude, airspeed, VSI,= weather, etc.).

Letting a situation go far enough that you don't kn= ow exactly what the aircraft is doing might ALWAYS result in disorientation= and ham-handed, knee-jerk reactions. In the example cited by others to con= demn the TruTrak ADI -- nose high in a descent with the ADI indicating nose= low -- a good scan would instantly orient the pilot.

Additionally, = TruTrak has already considered the above situation and accounted for it. Sh= ould the pilot allow the aircraft to slow enough such that pitch indic= ations might not match the actual attitude of the aircraft, the TruTra= k ADI will has a programmable warning indicator that tells the pilot to che= ck the airspeed.

For myself, I find the TruTrak ADI a fine alternati= ve to more expensive mechanical gyroscopic instruments.

Mark Sletten=

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